WO1992016147A1 - Intravascular imaging apparatus and method - Google Patents

Intravascular imaging apparatus and method Download PDF

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Publication number
WO1992016147A1
WO1992016147A1 PCT/US1992/002117 US9202117W WO9216147A1 WO 1992016147 A1 WO1992016147 A1 WO 1992016147A1 US 9202117 W US9202117 W US 9202117W WO 9216147 A1 WO9216147 A1 WO 9216147A1
Authority
WO
WIPO (PCT)
Prior art keywords
transducer
imaging
guide wire
drive cable
sheath
Prior art date
Application number
PCT/US1992/002117
Other languages
French (fr)
Inventor
Wayne Sieben
Mark J. Whalen
Original Assignee
Scimed Life Systems, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US07/840,917 external-priority patent/US5353798A/en
Application filed by Scimed Life Systems, Inc. filed Critical Scimed Life Systems, Inc.
Priority to JP92510598A priority Critical patent/JPH05508099A/en
Priority to CA002082161A priority patent/CA2082161A1/en
Publication of WO1992016147A1 publication Critical patent/WO1992016147A1/en

Links

Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B8/00Diagnosis using ultrasonic, sonic or infrasonic waves
    • A61B8/12Diagnosis using ultrasonic, sonic or infrasonic waves in body cavities or body tracts, e.g. by using catheters
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B8/00Diagnosis using ultrasonic, sonic or infrasonic waves
    • A61B8/44Constructional features of the ultrasonic, sonic or infrasonic diagnostic device
    • A61B8/4444Constructional features of the ultrasonic, sonic or infrasonic diagnostic device related to the probe
    • A61B8/4461Features of the scanning mechanism, e.g. for moving the transducer within the housing of the probe
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S15/00Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
    • G01S15/88Sonar systems specially adapted for specific applications
    • G01S15/89Sonar systems specially adapted for specific applications for mapping or imaging
    • G01S15/8906Short-range imaging systems; Acoustic microscope systems using pulse-echo techniques
    • G01S15/8934Short-range imaging systems; Acoustic microscope systems using pulse-echo techniques using a dynamic transducer configuration
    • G01S15/8938Short-range imaging systems; Acoustic microscope systems using pulse-echo techniques using a dynamic transducer configuration using transducers mounted for mechanical movement in two dimensions
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S15/00Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
    • G01S15/88Sonar systems specially adapted for specific applications
    • G01S15/89Sonar systems specially adapted for specific applications for mapping or imaging
    • G01S15/8906Short-range imaging systems; Acoustic microscope systems using pulse-echo techniques
    • G01S15/899Combination of imaging systems with ancillary equipment
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/52Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S15/00
    • G01S7/52017Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S15/00 particularly adapted to short-range imaging
    • G01S7/52023Details of receivers
    • G01S7/52034Data rate converters
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B8/00Diagnosis using ultrasonic, sonic or infrasonic waves
    • A61B8/44Constructional features of the ultrasonic, sonic or infrasonic diagnostic device
    • A61B8/4444Constructional features of the ultrasonic, sonic or infrasonic diagnostic device related to the probe
    • A61B8/445Details of catheter construction
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B8/00Diagnosis using ultrasonic, sonic or infrasonic waves
    • A61B8/44Constructional features of the ultrasonic, sonic or infrasonic diagnostic device
    • A61B8/4483Constructional features of the ultrasonic, sonic or infrasonic diagnostic device characterised by features of the ultrasound transducer
    • A61B8/4488Constructional features of the ultrasonic, sonic or infrasonic diagnostic device characterised by features of the ultrasound transducer the transducer being a phased array

Definitions

  • This invention relates to an ultrasonic imaging device and methods for use and manufacture thereof, and particularly to an ultrasonic imaging device positionable in coronary vessels to obtain images thereof.
  • Ultrasonic imaging of portions of a patient's body provides a useful tool in various areas of medical practice for determining the best type and course of treatment.
  • Imaging of the coronary vessels of a patient by ultrasonic techniques could provide physicians with valuable information about the extent of a stenosis in the patient and help in determining whether procedures such as angioplasty or atherectomy are indicated or whether more invasive procedures may be warranted.
  • obtaining ultrasonic images of the distal coronary vessels with sufficiently high resolution to be valuable for making medical decisions, such as described above requires overcoming several significant obstacles one of the most significant of which relates to the size of the ultrasonic sensing device.
  • ultrasonic imaging of organs deep within the body that are surrounded by other, relatively dense organs and tissues requires connecting a sensor on a probe and positioning the sensor and the probe near or even into the organ.
  • the heart and the vessels connected to it are organs of this type.
  • the vessels in the distal regions of the vascular tract that would be useful to image include the coronary arteries, branch vessels stemming from the external carotid artery such as the occipital and the arteries leading to the vessels of the head and brain, splenic, and the inferior mesenteric and renal arteries leading to the organs of the thorax.
  • the size of an ultrasonic sensor and probe must be relatively small not just to traverse the arterial vessel but also to avoid occluding the vessel lumen.
  • a device such as a catheter, probe, or sensor
  • the blood flow through the vessel is restricted to an annular region
  • the probe should be sufficiently small in dimension so as not only to be positioned in these small, possibly partially occluded arteries, but also to be sufficiently small so as not to totally or almost totally occlude the lumen of the vessel into which it is positioned. Accordingly, for an ultrasonic sensor device to be used for distal coronary applications, it must be small enough to be suitably positioned in the coronary vessels and to permit a sufficient blood flow therearound. For use in the distal coronary vasculature, the exterior dimension for a sensor device should be approximately 0.040 inches (1 mm) in diameter to provide an annular region of flow in even the most distal vessels.
  • Ultrasonic imaging devices intended to be placed in the vascular system have been disclosed in prior patents (e.g. U.S. Pat. No. 4,794,931). However, these prior devices have had numerous drawbacks that limited their utility for the most part to uses in only the peripheral vasculature and not in deep coronary arteries. Prior devices, having diameters ranging from 3.5 French (1.2 mm) and up, would be limited by their size to only very proximal coronary arteries. Prior devices, having diameters ranging from 4.5 French (1.5 mm) and up, would be limited by their size to only very proximal locations of coronary arteries, peri ⁇ pheral vessels, or very proximal organ vessels. Furthermore, in addition to these limitations, prior ultrasonic probe devices have produced images lacking in sufficiently high detail and resolution to provide useful information.
  • the probe device in order to position a probe device in a deep coronary vessel from a remote percutaneous site such as via the femoral artery, the probe device should possess a high degree of longitudinal flexibility over its length.
  • an ultrasonic probe device may have to transverse several curvatures of radius of 3/16 of an inch (4.7 mm) or less.
  • the probe device should possess a high degree of flexibility longitudinally over its length to enable it to transverse virtually any curvature of the vascular tract.
  • the device is to include a rotating ultrasonic sensor at a distal end to make radial scans of the entire cross section of the coronary artery, it should not only be flexible longitudinally, but should also be stiff torsionally. Rotation of the ultrasonic device should be achieved so that a drive shaft extending to the sensor does not experience angular deflection which might cause image distortion. Due to the continuous angular motion which dictates the location at which an ultrasound sensor scans, if angular deflection occurs at the distal end of sensor drive shaft, it can result in an artifact of angular distortion that becomes apparent on the ultrasound displayed image. This arti ⁇ fact can occur if the rotating sensor drive shaft experiences "whip".
  • Wood may be defined as the angular deceleration and acceleration of the sensor drive shaft as a result in shaft angular deflections during rotation. As the transducer drive shaft is rotating it may undergo angular deflection if the drive shaft's torsional stiffness is low enough to make the drive shaft susceptible to dynamic changes in torsional load. It may also undergo angular deflection if the • dynamic torsional loads are high and varying.
  • Image quality and accuracy is dependent on constant sensor angular velocity.
  • Image construction assumes a constant sensor velocity, therefore relative acceleration or deceleration between the expected and actual sensor angular velocity will cause image distortion.
  • the value of the device depends upon the quality of the ultrasonic image which in turn is a direct function of both the acoustic pulse signal and the electrical signal trans ⁇ mission. Therefore, in addition to the mechanical properties necessary for locating and rotating a sensor, the device should also provide a high quality electrical and acoustic signal. This may include several specific properties, such as a high signal to noise ratio of the electronic signal, impedance match ⁇ ing of the overall system without the need for internal electronic matching components, and minimization of voltage requirements to attain a signal of sufficient quality to provide an image.
  • the present invention provides a device for intravascular ultrasonic imaging, and methods for the use an manufacture thereof, comprising an elongate member with a distal end that can be positioned within a vessel of a patient's body while a proximal end is positionable outside the body.
  • the device also in ⁇ cludes a transducer located at a distal end of the elongate member and a signal processor connected to a proximal end of the elongate member for generating pulses to and receiving from said transducer.
  • the device preferably includes a motor for rotating the transducer and a drive cable for connecting the transducer to the motor and the signal processor.
  • the drive cable is operable to transmit electrical signals to and from the transducer.
  • Figure 1 is a schematic representation of a presently preferred embodiment of the ultrasonic imaging apparatus.
  • Figure 2 is a longitudinal vertical sectional view of a distal portion of the ultrasonic imaging apparatus depicted in Figure 1.
  • Figure 3 is a sectional view of the -aistal portion of the ultrasonic imaging apparatus along lines 3 - 3' in Figure 2.
  • Figure 4 is a sectional view of the -distal portion of the ultrasonic imaging apparatus along lines 4 - 4' in Figure 2.
  • Figure 5 is a plan view of a portion, parti ⁇ ally disassembled, of the drive cable.
  • Figure 6 is a sectional view of an embodiment of the elongate member of the system depicted in Figure 1.
  • Figure 7a a sectional view alone lines 7 - 7' of the embodiment of the elongate member depicted in Figure 6 illustrating a first alternative indexing function construction.
  • Figure 7b a sectional view alone lines 7 - 7' of the embodiment of the elongate member depicted in Figure 6 illustrating a second alternative indexing function construction.
  • Figures 8a and 8b are block diagrams of processing steps related to acoustical indexing.
  • Figure 9 is a sectional view of the alterna ⁇ tive embodiment of the elongate member shown in Figure 6 illustrating a first flushing method.
  • Figure 10 is a sectional view of a second alternative embodiment of the elongate member illus ⁇ trating a second flushing method.
  • Figure 11 is a sectional view along lines 10 - 10' of the embodiment in Figure 9.
  • Figure 12 is a sectional view of a portion of a third alternative embodiment of the elongate member illustrating a third flushing method.
  • Figure 13 is a plan view of the uncoupling member shown in Figure 1.
  • Figure 14 is a longitudinal vertical sec- tional view of the transducer pin assembly shown in Figure 13.
  • Figure 15 is a longitudinal vertical sec ⁇ tional view of the slip ring assembly shown in Figure 13.
  • Figure 16 is a plan view with a partial sec ⁇ tional view of the proximal drive cable shown in Figure 1.
  • Figure 17 is a diagram of signal amplitude versus time for the pulser in a first embodiment of the present invention.
  • Figure 18 is a diagram of signal intensity versus radial distance from the sensor perpendicular to drive direction.
  • Figure 19 is a diagram of signal intensity versus radial distance from the sensor perpendicular to drive direction.
  • Figure 20 is a diagram of signal intensity versus the position along the cross section A - A' of Figure 18.
  • Figure 21 is a diagram of signal intensity versus the position along the cross section B - B' of Figure 18.
  • Figure 22 is a block diagram of the calibrated waveform of the pulser.
  • Figure 23 is a perspective view of another embodiment of the transducer sensor.
  • Figure 24 is a plan view of the distal end of an imaging guide wire which is another embodiment of the present invention.
  • Figure 25 is plan view of yet another embodi ⁇ ment of the sensor housing of the present invention.
  • Figure 26 is plan view of still another embodiment of the sensor housing of the present invention.
  • Figure 27 is plan view of another embodiment of the present invention for 3-D imaging.
  • Figure 28 is a view of a distal section of an alternative embodiment of the elongate member with variations represented for 3-D indexing.
  • Figure 29 is a cross sectional view of the embodiment shown in Figure 28 along lines A - A'.
  • Figure 30 is a top view of a the distal end of yet another embodiment of the present invention that utilizes an alternative drive mechanism.
  • Figure 31 is an alternative embodiment of that shown in Figure 30.
  • Figure 32 is a block diagram of the data and graphics pipeline of an alternative embodiment of the present invention.
  • Figure 33 is a diagram illustrating horrina tion of a neural network architecture in an alternative embodiment of the present invention.
  • Figure 35 is a side elevational view of a first preferred embodiment of an imaging guide wire.
  • Figure 36 is a side elevational view of a preferred embodiment of a sliced transducer sensor for use in the imaging guide wire of Figure 35.
  • Figure 36a is a cross sectional view of the sliced transducer sensor of Figure 36.
  • Figure 37 is a top view of the sliced transducer sensor of Figures 36 and 36a.
  • Figures 36, 38, and 39 each show a top view of alternative constructions of the sliced transducer sensor of Figures 36 and 36a.
  • Figure 40 is a side elevational view of the preferred embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating a sheath over the transducer sensor.
  • Figure 40a is a cross sectional view along line A - A' of the transducer sensor of Figure 40.
  • Figure 41 is a side elevational view of an alternative embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating an exponential matching layer.
  • Figure 41a is a cross sectional view along line A - A' of the transducer sensor of Figure 41.
  • Figure 42 is a side elevational view of a preferred embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating a formed sheath matching layer.
  • Figure 42a is a cross sectional view along line A - A' of the transducer sensor of Figure 42.
  • Figure 43 is a side elevational view of an embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating a splined attenuation backing support.
  • Figure 43a is a cross sectional view along line A - A' of the transducer sensor of Figure 43.
  • Figure 44 is a side elevational view of an embodiment of a wedge transducer sensor for use in the imaging guide wire of Figure 35.
  • Figure 44a is a cross sectional view along line A - A' of the transducer sensor of Figure 44.
  • Figure 45 is a side elevational view of an embodiment of a multiple transducer sensor for use in the imaging guide wire of Figure 35.
  • Figure 45a is a cross sectional view along line A - A' of the transducer sensor of Figure 45.
  • Figure 46 is a side elevational view of an embodiment of the distal tip construction of the imaging guide wire of Figure 35.
  • Figure 47 is a side elevational view of an alternative embodiment of the distal tip construction of the imaging guide wire of Figure 35 incorporating a locking tip feature.
  • Figure 48 is a perspective view, partially disassembled, of an embodiment of the drive cable construction of the imaging guide wire of Figure 35.
  • Figures 49, 50, and 51 each show a perspective view of alternative embodiments of the proximal end section of the imaging guide wire of
  • Figure 52 is a side elevational view of an extension wire for use with the imaging guide wire of Figure 35.
  • Figure 53 is a side sectional view of a drive interface for making the electrical an mechanical connections for driving the imaging guide wire of
  • Figures 54a and 54b each show alternative embodiments of supporting means for the proximal end section of the imaging guide wire of Figure 35.
  • Figure 55 is a side sectional view of a holder apparatus for the imaging guide wire of Figure 35.
  • Figure 56 is a flow chart representing an embodiment of the pipeline architecture for the imager of Figures 1 or 35.
  • Figure 57 is a side sectional view of an alternative embodiment of the slip ring assembly of
  • Figure 15 incorporating a capacitive non-contacting slip ring assembly.
  • Figure 58 is a side sectional view of an alternative embodiment of the slip ring assembly of Figure 15 incorporating a magnetic non-contacting slip ring assembly.
  • Figure 59 is a side sectional view of an alternative embodiment of the imager of Figures 1 or 35 incorporating an EEPROM into the imager to store essential product information.
  • Figure 60 is a perspective view of an embodiment of a cath lab patient table and accessories for use with the imager of Figures 1 or 35.
  • the system comprises a sensor assembly 24 located at a distal end of the system 20 at a distal end of an elongate member 26.
  • the elongate member 26 can be percutaneously positioned in the cardiovascular system of a patient via a remote site such as the femoral artery so the distal end of the elongate member is located in or close to the remote site while a proximal end extends out the body of the patient.
  • the elongate member 26 includes at a distal end thereof the sensor assembly 24.
  • the elongate member 26 further includes means for transmitting an electrical signal between the sensor assembly 24 located at the distal end thereof and the proximal end extending out of the body of the patient.
  • the elongate member 26 further includes means for operating the sensor assembly to make scans of the remote vessel site.
  • the means for operating the sensor assembly 24 and the means for transmitting a electrical signal to and from it are provided by a distal drive cable 28 located inside the elongate member 26.
  • the sensor assembly 24 is connected to a distal end of the distal drive cable 28.
  • the distal drive cable 28 is connected at its proximal end to a coupling member 30 which connects to components located at a proximal end of the sy tem 20.
  • the coupling member 30 serves to releas- ably couple the distal drive cable 28 to, and uncouple the distal drive cable 28 from, a proximal drive cable 32.
  • the proximal drive cable 32 includes a first leg 33 that connects to a signal processing unit 34 and a second leg 35 that connects to a motor 36.
  • a control unit 38 Connected to both the signal processing unit 34 and the motor 36 is a control unit 38 that serves to operate the motor 36 and the signal processing unit 34.
  • the present embodiment is adapted for use in deep organ vessels where the residual diameter of the vessel may be 1.5 mm or less.
  • the overall maximum diameter of the distal portion of the ultrasound imaging system is preferably not more than approximately 3.2 French (1.07 mm or 0.42 inch) and preferably the distal portion of the system has an overall diameter of less than 3.0 French (1.0 mm).
  • the signal processing unit 34 In operation, the signal processing unit 34 generates electrical pulses that are transmitted to the sensor assembly 24 via a proximal electrical transmis ⁇ sion cable inside the proximal drive cable 32 (as further described below) and the distal drive cable 28. The signal processing unit 34 also receives electrical pulses back from the sensor assembly 24 via these cables.
  • the motor 36 operates to rotate a proximal drive shaft located inside the proximal drive cable 32 (as described below) which in turn rotates the sensor assembly 24 to which it is coupled via the distal drive cable 28. Rotation of the sensor assembly 24 while pulsing and receiving the reflections effects an radial ultrasonic scan of the area proximate to the sensor assembly 24.
  • the motor 36 operates to rotate the transducer assembly 24 at speeds ranging from 500 to 1800 RPM, with a preferred rotational speed of approximately 1000 RPM.
  • the design and construction of the various components of the system are preferably computer modeled and iterated to provide optimum overall system performance. For example, for optimum performance, impedance throughout the overall system from the signal processing unit 34 to the sensor assembly 24 is carefully matched to eliminate reflections at all interfaces caused by impedance mismatch. By eliminating reflections in the system, there is a faster settling of the pulses since reflections can cause ringing of the pulse thus reducing the radial resolution. Because there is limited potential for adjustment of the impedance at the sensor assembly 24 end of the system, consistent with other requirements, the rest of the system components proximal from the sensor assembly 24 are matched to it. In this embodiment, a system impedance of 50 ohms is selected.
  • the coupling member 30 is not specifically matched to that of the rest of the system.
  • the coupling member has a low resistance, e.g. less than 0.5 ohm. However, the length of the unmatched impedance portion of the coupling member is made to be only approximately 0.75 inch.
  • the signal processing unit 34 (including the pulser) , at signal voltage levels, is also selected with impedance matched to the system impedance, i.e. 50 ohms, to eliminate reflections. With a matched termination at the signal processing end of the system, the signal is insensitive to the length of the cable members. This provides the advantage that the motor 36 and signal processing unit can be positioned out of the way of the physician, e.g. under a table or other convenient place.
  • FIG. 2 there is depicted a vertical longitudinal sectional view of a distal portion of the imaging system 20 including the sensor assembly 24 of a first presently preferred embodiment.
  • the sensor assembly 24 is located inside the elongate member 26.
  • the sensor assembly 24 is connected at a proximal end thereof to the drive cable 28.
  • the sensor assembly 24 includes a sensor housing 40 in which is mounted a transducer sensor 42.
  • the transducer housing 40 is a hollow, generally tubular member having a cylindrical wall and open ends.
  • the housing 40 has dimensions that provide for posi ⁇ tioning and rotating inside of a lumen 43 of the elongate tubular member 26.
  • the housing 40 has an outside diameter of 0.030 inches. This may be equal to the diameter of the drive cable 28.
  • the housing 40 is a metallic tube of 304 stainless steel.
  • the transducer sensor operates in alternating pulsing and sensing modes. In the pulsing mode, when excited electrically, the transducer sensor 42 creates a pressure wave pulse which travels through the elongate member into the arterial environment.
  • the transducer sensor 42 In the sensing mode, the transducer sensor 42 produces an electrical signal as a result of receiving pressure waves reflected back to the transducer. These reflections are generated by the pressure waves traveling through changes in density in the arterial environment being imaged. The electrical signals produced by the transducer sensor 42 are transmitted back to the signal processing unit 34 for generation of images of the arterial environment by methods known in the art and as further described below.
  • the transducer sensor 42 is constructed from several distinct layers including a transducer core material 44 having a first and a second metallized electrically conductive surface layers, 45a and 45b, bonded thereto, a matching layer 46, a backing layer 47 bonded to the metallized sur ⁇ faces, and one or more adhesive layers.
  • This con ⁇ struction provides a transducer sensor with an active area of approximately 1.0 x 0.5 mm.
  • the impedance of the transducer is a linear function of the active area so for a device having an active surface area of about 1.0 x 0.5 mm, the impedance is approximately 50 ohm.
  • the transducer core 44 of the tranducer sensor 42 is a flat rect- angular piece of PZT (Lead Zirconate Titarate) type ceramic material.
  • PZT material has an acoustic impedance of mid 20's and a speed of sound of about 5000 m/s. At this speed, the thickness for a 30 MHz sensor is about 0.003 inch. At this thickness, PZT materials should be selected with small grain sizes so that shorts are not generated during processing.
  • the PZT material is cut to a rectangular shape of 0.5 x 1.25 mm.
  • the active area after wires and a matching layer are attached is approximately 0.5 x 1.0 mm.
  • the first and second conductive layers, 45a and 45b are positioned respectively on each face of the transducer core 44.
  • the conductive layers 45a and 45b may be composed of a number of electrically conduc ⁇ tive materials, such as gold, silver, copper, or nickel. However, a number of other materials, elements or alloys are suitable. Additional layers may be needed under each conductive layer to provide for adhesion to the core material, e.g. , using chromium under gold. For good performance, the resistance of the conductive layers should be less than 1 ohm from one end thereof to the other.
  • the matching layer 46 provides an impedance transformation between the transducer sensor 42 and the fluid therearound to allow a better coupling of energy into the fluid. This transformation is frequency dependent.
  • a matching layer may be used where a dif- ference exists between the transducer and the medium adjacent thereto. Use of a matching layer provides for a stronger and sharper pulse and thus a better image.
  • the optimized value range for the matching layer is from 3.8 to 4.2 (x 10 6 kg/m 2 sec).
  • the material that is used for the matching layer may be PVDF (Kynar) at a thickness of 0.95 x (quarter wavelength thickness) .
  • the matching layer 46 is bonded to the first conductive layer 45a by means of a thin glue layer.
  • the matching layer 46 conforms approximately in surface dimension to the active size of the transducer, i.e. 0.5 x 1.0 mm.
  • the backing layer 47 serves to absorb acoustical energy generated off the non- imaging side of the transducer and also helps minimize energy reflections coming back to the transducer.
  • the amount of energy traveling from the transducer core to the backing is a function of the acoustic impedance of the core and the backing material. The energy that is generated and enters the backing material should be attenuated sufficiently before it is reflected back into the core where it can distort the signal.
  • the backing layer 47 impedance is selected to provide optimum damping so that the transducer sensor 42 vibrates for only a short duration after electrical excitation is stopped and prevents energy from being reflected to or from the artery wall to the back side of the transducer. This enables the transducer sensor 42 to be ready to receive pressure waves reflected from the arterial environment with no or minimal interfer ⁇ ence from ringing from the pulse.
  • the impedance of the backing layer may be determined by computer modeling and in this embodiment is selected in the range from 5 to 7 (x 10 6 kg/m 2 sec).
  • the composition used for the backing is preferably a tungsten and silicon rubber mixture. The acoustical impedance of the mixture can be varied by mixing various sized tungsten powder particles into the silicon rubber.
  • the backing layer 47 may be bonded to the conductive surface 45b by means of a thin glue layer applied on backing type material.
  • the backing layer 47 conforms in surface dimension to the size of the active area, i.e. approximately 0.5 x 1.0 mm.
  • the backing layer 47 is preferably provided with a maximum thickness, or depth dimension, consistent with the dimensions of the sensor housing 40, drive cable, elongate member, etc.
  • the backing layer 47 may be made to a dimension equal to the cross-section of the drive cable 28 and/or housing 40. This allows for a backing layer of a maximum size to provide for sensor ringdown time and yet is small enough to fit deep into the coronary arterial environ ⁇ ment.
  • the backing layer may be approximately 0.012 inches in thickness.
  • the transducer sensor 42 is connected by the sides 48 and 49 thereof to the interior of wall 50 of the housing 40.
  • the transducer sensor 42 is mounted so that the central axis of the sensor assembly 24 passes through or is close to the plane defined by the flat surface of the transducer sensor 42.
  • the flat surface of the transducer faces perpendicular to its axis of rotation. This permits maximizing the dimensions of the matching layer and backing layer.
  • This construction also allows for secure mounting of the sensor assembly 24 to the drive cable 28 by inserting and connecting the housing 40 to the distal end of the drive cable 28.
  • the housing 40 has a first acoustic window (or aperture) 52 and a second window 53 oppositely located from each other in the cylindrical wall of the housing 40.
  • These windows are preferably approximately rectangular in shape having parallel sides in the longitudinal direction of the housing 40 and rounded sides in the chordal direction. These windows may be formed by removing portions of the material of the cylindrical wall of the housing but leaving narrow bands 54 and 55 of the wall 50 of the housing 40 onto which the transducer sides 48 and 49 may be bonded. In a preferred embodiment, both windows 52 and 53 are approximately 0.6 x 2.0 mm.
  • the transducer sensor 42 is mounted and located in the housing 40 directly facing the first window 52 so that the ultrasonic signal is emitted from the transducer sensor 42 through the first window 52.
  • the size and geometry of the windows are related to the pulse generating characteristics and the advantages of the disclosed window geometry are de ⁇ scribed below in conjunction with the description of the operation of the pulser.
  • the sensor assembly 24 can be constructed and tested before mounting to the drive cable 28 by connecting the wires between the tested sensor and the tested cable inside the window. This ability to screen sensor assemblies prior to attachment to the drive cable increases transducer drive shaft assembly yield dramatically.
  • the housing design also allows alignment of the transducer in the elongate member during rotation by the smooth rounded end and fit between elongate member 26 and the housing 40. Referring to Figure 4, the sensor assembly 24 is connected at its proximal end to the distal end of the drive cable 28. Specifically, the first conductive layer 45a of the transducer sensor 42 is connected to the distal end of an internal conductor 58 of the drive cable core wire 60.
  • a distal end of an external layered coil portion 62 of the drive cable 28 is con ⁇ nected to the housing 40. These connections may be made by means of an epoxy adhesive.
  • An external conductor 63 (also referred to as the reference plane conductor) of the core wire 60 is sealed by means of an epoxy.
  • the reference plane conductor 63 of the core wire 60 is connected electrically to the housing 40 via the external layered coil portion 62 of the drive cable 28.
  • a single trans ⁇ ducer is mounted in a single transducer housing which is connected at the distal end of a drive cable.
  • more than one transducer with one or more housings may be connected serially at the end of a drive cable in order to make scans of a length of a vessel.
  • an appropriate switching device may be utilized in conjunction with the signal process ⁇ ing unit and the transducers to coordinate pulsing and receiving data.
  • the drive cable 28 is positioned inside the elongate member 26 and is con- nected to the sensor assembly 24, as described above.
  • the drive cable 28 serves as both the mechanical and electrical link to the sensor assembly 24.
  • the drive cable 28 conducts the electrical signal from the proximally located signal processing unit 34 (via the proximal drive cable 32) to the sensor assembly 24 and conveys the sensed signal from the sensor assembly 24 back to the signal processing unit 34.
  • the electrical components of the drive cable provide for mechanical motion transmittance as well.
  • the drive cable 28 connects the sensor assembly 24 to the proximally located motor 36, via a drive shaft located in the proximal drive cable 32, in order to rotate the sensor assembly 24 to scan -the coronary vasculature with an ultrasonic signal.
  • the drive cable 28 In order to provide high quality electrical signal transmission, the drive cable 28 possesses a controlled matched impedance, a low signal loss, and high shielding and conductivity at high frequencies.
  • the need for a matched impedance in the drive cable 28 follows from the requirement for matching impedances at interfaces of the overall imag- ing system from the signal processing unit 34 to the sensor assembly 24 in order to eliminate reflections.
  • the rest of the system components, including the drive cable 28 are matched to that of the impedance of the transducer sensor 42. Accordingly, the impedance of the drive cable 28 is matched to that of the sensor assembly 24 and in this embodiment is established to be 50 ohms.
  • the drive cable 28 possesses high torsional stiffness (i.e. minimal angular deflec ⁇ tion under operating torsional load) yet possess longi ⁇ tudinal (axial) flexibility to allow percutaneous posi ⁇ tioning in the coronary vessels.
  • the drive cable 28 also possesses dimensional properties suitable for positioning in a patient's coronary vasculature, specifically the drive cable 28 has a low profile diameter to navigate torturous coronary arteries.
  • a present embodiment provides these features in part by a coaxial multi ⁇ layer drive cable construction.
  • the drive cable 28 includes a core wire 60 located inside of an outer layered coil assembly 62, as explained below.
  • the core wire 60 is located at the center of the drive cable 28.
  • the core wire 60 includes an insulated internal conductor 58.
  • the core wire 60 has a diameter of 0.014 inch and its internal conductor 58 is 38 AWG (7 strands of 46 AWG) copper wire.
  • the internal conductor 58 is surrounded by a teflon coating that forms an insulator layer 66. Teflon is used as an insulator for the internal conductor 58 of the core wire 60 because of the relatively low dielectric constant which allows for a smaller cable, less loss, and higher speed of electrical transmission for a given impedance.
  • Around the insulated internal conductor 58 is an external conductor 63 in the form of a braided shield which forms the exterior electrical shield of the core wire 60.
  • the braided shield is preferably composed of eight silver-plated, rectangular copper strands 70, four in each direction of rotation. Spe ⁇ cifically, each strand is 0.001 x 0.007 inch oxygen free highly conductive (OFHC) copper with 50 micro- inches of silver plating.
  • OFHC oxygen free highly conductive
  • the silver plating provides a high qual- ity environmental seal from corrosion.
  • the silver plating on the flat copper wires of the braided shield of the external conductive wire 63 also advantageously reduces the shield's electrical resistance at the high electrical frequencies due to "skin effect". Electrical transmission through a con ⁇ ductor wire at high frequencies exhibits a "skin effect" which is a phenomena wherein the electrical current tends to increasingly travel in the outer periphery of a conductor as the signal frequency is increased. At the frequencies of operation of the imaging system, most of the current would be carried in the conductor within less than 0.0005 inch of the sur ⁇ face of the conductor. This is one of the reasons that the external conductor wire 63 is made with silver plating because silver has a lower resistivity than copper. For a given thickness more current will be carried in a silver layer than in the copper base.
  • a further reason for using silver plating is its property of non-corrosiveness which helps maintain low electrical resistance at the overlapping joints of the braided shield of the external conductor 63.
  • the application of the silver plated, braided shield to the insulated internal wire thus forms a high quality miniature 50 ohm coaxial cable with a total diameter less than 0.030 inch (0.75 mm).
  • the layered coil assembly 62 comprises a multi-layer, multi-strand coil for optimum torque transmittance.
  • the layered coil assembly 62 of the present embodiment is comprised of three layers 74, 76, and 78. Each coil layer is composed of three separate wires strands, e.g. coil layer 78 is comprised of strands 80, 82, and 84. Each strand may be com ⁇ prised of a 50 micro-inch silver plated, oxygen free highly conductive (OFHC) copper ribbon wire having dimensions of 0.001 x 0.007 inch.
  • This construction of the layered coil assembly provides for suitable torque transmission (or stiffness) by reducing the torsional load per strand.
  • coil layer 74 is wound in an opposite helical direction from that of coil layer 76
  • coil layer 76 is wound in an opposite helical direction from that of coil layer 78 (but coil layer 78 would be wound in the same helical direction as coil layer 74)
  • the coil winding direction is determined so as to be consistent with the direction of drive cable rotation so that during operation of the system, the layered coil assembly will tend to tighten upon itself thereby providing additional torsional stiffening effects to the drive cable during operation without decreasing the cable's longitudinal flexibility during positioning. Increasing the torque stiffness reduces the angular deflection per coil layer.
  • flat wire for the layered coil assembly has several advantages. Using flat wire helps in maintaining the low profile of the drive cable, e.g only approximately 0.028 inch. This is significantly smaller than would be possible if a round wire of equivalent inertial moment were used. In addition, the use of multiple flat wire coils provides a significant amount of shaft flexibility due to the inherent slip planes between coils and strands which facilitates placement of the drive cable in the coronary arteries.
  • the utilization of silver plated OFHC copper for the layered coil assembly 62 advantageously bene- fits the drive cable's electrical properties as well.
  • the use of the silver plated OFHC copper provides shielding effectiveness and lower resistance than other conductors (both DC resistance and high frequency resistance due to "skin effect" in conductors) . These properties reduce the electrical signal attenuation through the drive cable 28 and aid in producing the cable's matched impedance.
  • These electrical character ⁇ istics improve the overall system performance by improving the signal to noise ratio and eliminating the need for impedance matching components.
  • the drive cable 28 may be constructed accord ⁇ ing to the following procedure.
  • the core wire 60 is constructed.
  • the braided shield for the reference plane conductor is constructed over a 0.014 inch diameter teflon insulated core wire using a Kokubun braiding machine.
  • the Kokubun braider utilizes 16 bobbins containing braid wire moving in a inter-twining planetary action to create an interlaced braid.
  • Bobbin movement, in terms of orbiting speed, and feed rate of the central core wire through the braiding area are controlled by two speed regulated motors, such as 2 1/4 H.P. Emerson Motors, P/N 3120-406.
  • Motor speed of the core wire take up pulley and the bobbin rotation are closely regulated to predetermined values to ensure finished shaft's mechanical and electrical properties. This may be done with a Focus 1 Speed Controller.
  • the following process is followed to set up the Kokubun braiding machine.
  • the teflon insulated internal wire 58 is routed through the center guide of the braider's bobbin carriage. Due to the fragility of the internal wire and the ribbon wire to be braided over it, an additional core wire guiding apparatus providing wire support, back tension, and braid wire entrance angle guiding is added to the Kokubun braiding machine. Also, the back tension provided at the bobbins for the braid flat wire has been reduced to approximately 35% of its original value. A modified upper guide has been added to control the small diameter braided wire's movement during the braiding process.
  • the Kokubun braider provides positions for 16 bobbins from which to create a 16 strand braid. Eight of these bobbins are removed to generate a coarser braid. The eight bobbins removed consist of 4 in each direction in an alternating fashion such that the remaining interleaved braid consists of four strands in each direction.
  • the braiding machine is started and bobbin carriage and braid take up wheel motor speed are adjusted.
  • the bobbin carriage speed is set to 395 +/- 5 RPM.
  • the braid take up wheel speed is set to 530 +/- 5 RPM.
  • the braider configuration is modified such that the bobbin carriage motor has been fitted with a 5:1 gear reducer and similarly, the braid take up wheel motor utilizes a 30:1 gear reducer to provide the appropriate carriage and take up speeds.
  • the internal wire is routed through the braider's main guide and the upper broad guide and attached securely to the take up wheel.
  • Bobbins containing the 0.001 inch x 0.007 inch silver plated OFHC copper ribbon wire are threaded through the upper guide and attached to the braider's take up wheel, one strand at a time. Using the manual carriage crank, the bobbin carriage is rotated through 5 full rotations in order to initiate the braid on the internal wire.
  • the braid After initiation of the braid onto the internal wire, the braid is bonded to the core wire using a cyanoacrylate adhesive over the entire existing braid length.
  • the braiding machine is started by simultane ⁇ ously switching on both the carriage motor and the take up wheel motor. The motor speeds are verified with respect to their preset values. The braider is then allowed to operate for sufficient time to produce the required length of braided core cable based on the braider's approximate production of 0.33 feet/min.
  • the braid Upon completion of the braided length, the braid is bonded using a cyanoacrylate adhesive over 0.5 inch bond length. The braid is cut at the bond area and removed from the braiding machine. The core wire portion is completed.
  • the layered coil portion 63 is added to the core wire 60.
  • a length of core wire of 66 inches is provided.
  • the core wire 60 is prepared for the addition of the layered coil portion 62 by bonding the braided wire ends of the external conductor 63 using cyanoacrylate adhesive over a 0.5 inch length to prevent unravel of the braid.
  • the application of layered coil portion 62 to the core wire 60 is performed using an Accuwinder Model CW-16A.
  • the core wire is loaded in to the coil winder head and tail stock chucks. Three spools of 0.001 inch x 0.007 inch silver plated, OFHC copper ribbon wire are loaded on the coil winder's spool carriage.
  • the wires are individually threaded through the coil winder's two guides and two tensioning clamps and finally through the three wire, lead angle guide. Wires must be routed under the three wire guide wheel and over the lead angle guide.
  • the tensioning clamps are set to light tension.
  • the spool carriage is moved into its initial coiling position; it is located such that the lead angle wire guide is approximately 0.25 inches (axially) from and head stock, and approximately 0.005 inches (radially) from the core wire. Guide adjustments are made by loosening their retaining screws.
  • the first multistrand coil 74 is wound with the coil winder's rotation direction switch in the clockwise (CW) position. This coil winding rotation direction requires the three coil strands to be routed beneath the core wire and secured to the head stock spindle.
  • Axial tension is slowly added to the core wire until a value of.3 to .5 pounds-force is reached.
  • the operating lever is lowered.
  • the coil winding speed is slowly increased to a maximum value of 60%.
  • Core wire tension is continuously monitored during the coil winding process to maintain a wire tension of .3-.5 pounds- force.
  • Coil winding is continued until the lead angle guide is within 1 inch, axially, of the tail stock chuck.
  • the coiling process is halted by raising the operating lever and reducing the speed control to 0%.
  • the coils are bonded to the core wire at the head and tail stock location over a 0.5 inch bond length.
  • the three strands used to form the coil 74 are cut at the core wire 60 and care is taken to prevent damage to the core wire 60.
  • the spool carriage is returned to the head stock location in preparation for applying the second, opposing, coil 76.
  • the tail stock pulley is loosened such that it can move independently of the coil winder drive shaft.
  • the tail stock spindle is rotated 5 full revolutions in the CCW direction (when viewing the front of the tail stock chuck) in order to preload the first coil.
  • the tail stock pulley is tightened.
  • the three ribbon wires to be coiled are routed under the three wire guide, over the lead angle guide, and placed over the core wire; the wires are temporarily secured to the head stock spindle.
  • the coil winder's rotation direction switch is moved to the Counter Clock Wise (CCW) position.
  • the operating lever is lowered and the speed control is increased gradually to 60%.
  • the core wire tension is maintained at .3-.5 pounds-force.
  • Coiling is continued until the lead angle guide is within 1 foot, axially, of the tail stock chuck.
  • the coiling process is halted by raising the operating lever and reducing the speed control to 0%.
  • the coils in this layer 76 are bonded to the core wire 60 at the head and tail stock locations over a 0.5 inch bond length.
  • the three strands used to form the coil 76 are cut at the core wire 60 and care is taken to prevent damage to the core wire 60.
  • the spool carriage is returned to the head stock location in preparation for applying the third coil 78.
  • the tail stock pulley is loosened such that it can move independently of the coil winder drive shaft.
  • the tail stock spindle is rotated 5 full revolutions in the CW direction (when viewing the front of the tail stock chuck) in order to preload the second coil.
  • the tail stock pulley is tightened.
  • Ribbon wires to be coiled are routed under the three wire guide, over the lead guide, and placed under the core wire; the wires are temporarily secured to the head stock spindle.
  • the coil winder's rotation direction switch is moved to the Clock Wise (CW) position.
  • the operating lever is lowered and the speed control is increased gradually to 60%.
  • the core wire tension is maintained at .3-.5 pounds-force. Coiling is continued until the lead angle guide is within 1 foot, axially, of the tail stock chuck.
  • the coiling process is halted by raising the operating lever and reducing the speed control to 0%.
  • the coils are bonded to the core wire at the head and tail stock locations over a 0.5 inch bond length.
  • the three strands used to form the coil 78 are cut at the core wire 60 and again care is taken to prevent damage to the core wire 60.
  • the spool carriage is returned to the head stock location. Exiting the coil winding computer control program is accomplished by pressing the escape key (esc) at the computer keyboard, lowering the operating lever, and gradually raising the speed control above 0%. This sequence will create a user prompt to continue or exit to the main menu. A "M" is keyed to return the user to the main menu.
  • the completed drive cable 28 is removed from the coil winder.
  • the remaining coil strands at the head stock are removed by trimming.
  • a preferred embodiment of the drive cable 28 is provided having an impedance of 50 ohms, a low electrical signal loss of 10-12%, and high shield and signal conductivity at high frequencies in the range of 10 - 50 MHz (which includes the preferred operating frequency of 30 Mhz) .
  • a cable constructed according to the above described method can possess a relatively low loss, from 0.9 to 1.4 Db loss over the required frequency range.
  • the drive cable 28 has a diameter of 0.028 inch which is suitable for use inside a lumen of the elongate member 26 having an internal diameter of approximately 0.035 inches.
  • the drive cable 28 and sensor assembly 24 rotate at an angular speed while the transducer sensor 42 is excited and monitored.
  • the drive cable 28 and sensor assembly 24 are located in the flexible elongate member 26.
  • the elongate member 26 is composed of a non-rotating, bio-compatible sheath that not only encloses both the drive cable 28 and sensor assembly 24 but also serves to position the transducer sensor 42 at a desired location in the coronary vasculature.
  • the elongate member 26 comprises a tubular sheath 80 having a distal portion 82 that can be positioned in a coronary artery and a proximal portion 84 that extends out of the body of the patient.
  • the proximal portion 84 of the sheath 80 is fixed to a stationary (non-rotating) component, specifically to a catheter manifold 85 which in turn is connected to the housing of the uncoupling member 30 (as described below and as depicted in Figure 14) .
  • the sensor assembly 24 is located in a lumen of the elongate member 26 and specifically in a lumen 86 of the sheath 80 in a distal portion thereof.
  • the sheath 80 In order to permit the transmission of the ultrasonic signal from the transducer sensor 42 which is inside of the sheath 80 into the body of the patient (and the reflections back again) , the sheath 80, or at least a distal portion thereof, is made of a material that is transparent to the ultrasonic signal.
  • the sheath 80 or the distal portion thereof is made of a TPX material, specifically a methylpentene copolymer plastic.
  • the TPX material has an acoustic impedance close to water, a low coefficient of friction, and good mechanical properties. Because the acoustic impedance of the TPX material is close to water, very minimal signal reflections are created at the sheath/blood interface. This characteristic allows the TPX material to appear transparent to the trans ⁇ ducer.
  • the sheath 80 is formed of a polyurethane material.
  • the transducer sensor 43 is mounted in the housing 40 at a slight forward tilting angle, e.g. 10 degrees. This allows for the passage of the ultrasonic waves through the sheath 80 without reflections.
  • the sheath 80 is formed having a low profile suitable for positioning in the coronary vasculature.
  • the sheath has 80 an external diameter of 0.040 inch.
  • the TPX material lends itself easily to the extrusion process and can be readily drawn to very thin wall diameters.
  • the wall diameter of the sheath is 0.0025 and the diameter of inner lumen is 0.035.
  • the sheath 80 furnishes other features. Because the TPX material has a low coeffi ⁇ cient of friction, it provides a low frictional resistance bearing surface between the internal drive cable 28 and the wall of the lumen 86 of the sheath 80. In addition, the sheath 80 provides mechanical support to the drive cable 28 in order to develop good "pushability" for cable manipulation. The TPX material possesses good mechanical properties for an extruded copolymer. The mechanical strength of the TPX material coupled with the axial stiffness of the drive cable 28 generates a sufficient degree of "pushability", i.e. structural support in the sheath assembly, for positioning the sensor assembly 24 in coronary arteries.
  • an inner lumen seal 87 Located in the lumen 86 of the sheath 80 near the distal end is an inner lumen seal 87.
  • This inner lumen seal 87 serves to establish a barrier between the interior of the sheath 80 and the patient's blood vessel. This shields the blood vessel from the turbulence caused by the rotation of the drive cable 28 and sensor assembly 24.
  • the distal end of the sensor assembly 24 is approximately 0.050 inches from the inner lumen seal 87.
  • the guiding tip 88 may be located in the lumen 86 of the sheath 80 distally from the inner lumen seal 87.
  • the guiding tip 88 may be comprised of a radiopaque material, such as a coil of thin platinum wire. Platinum, with its inherent radiopacity, wound in a coil configuration produces a soft, flexible, radio-opaque, crush resistant tip. Mounting the coil inside the lumen 86 of the sheath 80 permits retaining the smooth outer surface of the sheath 80 thereby facilitating maneuvering the sheath 80 through a guiding catheter and eventually into a coronary artery.
  • the catheter manifold 85 As mentioned above, at a proximal end of the sheath 80 is located the catheter manifold 85.
  • the catheter manifold 85 has a first or main port 89 gener ⁇ ally aligned and communicating with the lumen 86 of the sheath 80 and a second port 90 also communicating with the lumen 86 of the sheath 80.
  • a strain relief coil 91 is located around the outside of the proximal end of the sheath 80 and extends into and is bonded between the sheath 80 and the catheter manifold 85.
  • the catheter manifold 85 is utilized to connect the sheath 80 to the uncoupling member 30, as described below.
  • the drive cable 28 is installed into the sheath 80 via the main port 89.
  • the second port 90 may be used for flushing of the sheath 80, as described below.
  • the sheath 80 may also provide for a means of rotational compensation in order to continuously calibrate the transducer's angular orientation during operation.
  • One of the drawbacks associated with rotat ⁇ ing ultrasonic imaging devices is angular distortion between the encoders at the proximal end and the sensor at the distal tip of the catheter.
  • the fixed distortion is caused by friction or stiffness that causes a repeatable torque variation with each cycle. This can be found in almost every rotating element to some degree.
  • the distortion that changes in time causes the image to rotate periodically.
  • the major source of this is the heart moving, which flexes the elongate member causing a frictional torque variation synchronous with the heart beat.
  • An acoustical indexer is a locational marking that is put on, or built into the sheath to provide a rotational registration. This registration is constructed in the manner so that it can be readily identified in the signal processing.
  • rotational compensation markers 92 can be incorporated circumfer- entially in the wall of sheath 80 in a distal portion thereof.
  • the markers 92 may be splines or patterns incorporated on the interior surface of the sheath 80, as depicted in Figure 7a, or on the exterior surface of the sheath, as depicted in Figure 7b.
  • the markers 92 are located at periodic positions 45 degree from each other around the circumference of the sheath wall.
  • the markers 92 can be made from a variable thickness in the sheath material, but could be made from two different materials.
  • markers 92 may be formed in the extruding process for the sheath and may be made just in the region of the sensor or may extend over the entire length of the sheath.
  • Each wall thickness change may be recognized by the signal processing unit 34 and can be used to verify the transducer's angular position during operation. The thickness steps could be made at various ramp rates.
  • the signal process ⁇ ing unit can follow the image variation in distance. By following and holding steady one edge or feature, the time variable distortion is corrected. This com- pensation ability removes any discrepancy in a image due to an angular speed change of the transducer.
  • FIG. 8a and 8b A block diagram of the indexing data -process ⁇ ing is shown in Figures 8a and 8b.
  • a real time con- figuration tracks an edge in real time and adjusts the pulse pattern very quickly, as represented in «fig- ure 8a.
  • the data is intercepted from the raw data pipeline, processed and transferred to the pulser com ⁇ puter.
  • the EKG signal would be useful for calibrating the image to the heartbeat and removing the time-motion effect.
  • a non-real time configuration could be used almost as effectively, as represented in Figure 8b.
  • the data is processed and transferred periodically as needed.
  • the data is captured and processed by the main processor and the result sent to a pulser computer that would pulse the excitation at the proper times.
  • a variation of this method but yielding basically the same result would apply a pulse to the sensor every increment of a motor encoder and determine the position of each vector in the pipeline processing.
  • a sheath 80 may be made by irst bonding a tubular portion into the catheter manifold 85 using an epoxy or other suitable adhesive.
  • the sheath 80 should extend to a distal side of the entrance of the flush ports into the manifold 85. Care should be taken to ensure that adhesive does not flow into the lumen 86 of the sheath.
  • the strain relief coil 91 may be installed into the manifold hub. The hub is then filled with adhesive. This assembly is then allowed to cure.
  • the adhesive lumen seal 87 is installed in the distal end of the sheath 80.
  • the seal 87 is preferably located 0.5 inch from distal tip of sheath 80.
  • the seal 87 should be 0.100 inch in total length.
  • the distal marker coil is installed. Using a syringe, adhesive is applied to 0.05 inch of the distal end of the marker prior to installation. The distal marker is installed in the distal end of sheath 80. The marker coil is allowed to interfere with the sheath's seal 87 by 0.05 inch. Then the assembly is allowed to cure at 140°F for 4 hours.
  • the sheath 80 includes a means for flushing the sensor assembly 24 and sheath lumen 86. Any pres ⁇ ence of entrapped gas or contaminants in around the sensor assembly 24 reduces the performance of the imag ⁇ ing system. Any gas or contaminants on the surface of the transducer sensor 42 may generate severe reflec- tions and essentially blind the transducer in that region. The flushing process assures that all gas and contaminants are removed.
  • a first embodiment of the flushing system utilizes a flushing lumen 93 which may be a flexible tubular member having a diameter less than the diameter of the lumen 86 of the sheath 80.
  • the flushing lumen 93 may be fed through the catheter manifold's second port 90 proximal to the distal seal 87 of the lumen 86.
  • the flushing lumen 93 is then pressurized with a flushing medium.
  • the flushing lumen 93 is slowly withdrawn from the sheath 80 while press ⁇ ure is maintained on the flushing medium. The process is continued until the flushing medium flows from the proximal end of the manifold's main port 89 and the flushing lumen is removed.
  • the second flushing embodiment uses a sheath 94 having dual lumens, a main lumen 95 and an outer lumen 96.
  • the outer lumen 96 provides a flushing channel to the distal end of the sheath 94 where it communicates with the distal end of the main lumen 94 through a opening 97 between the lumens 95 and 96.
  • a flushing medium is depicted.
  • a proximal catheter manifold's flush port 98 through the flushing lumen 96 from the proximal end to the distal end, through the opening 97 into the main lumen 95, and back through the main lumen 95 from the distal end to the proximal end until the medium flows from the manifold's main port.
  • a third embodiment of the flushing system is depicted.
  • This embodiment in- eludes a sheath 99 having an air permeable seal 100 in the sheath's distal tip to allow entrapped gases to diffuse out during flushing pressurization.
  • the seal 100 has a permeability which allows the air mass in the sheath lumen to be dissipated through the distal tip area in a reasonably short amount of time.
  • the seal's porosity is low enough to restrict water mass transfer, i.e. the surface tension of the water coupled to the porosity of the seal prohibits mass transfer.
  • the seal may be made with materials with permeabilities in the range of: 2 to 2,000,000 ng/(s-m-Pa) .
  • This permeability range covers both flushing pressure variations of 6.895 kPa to 689.5 kPa and flushing times of 1 second to 1200 seconds.
  • permeability for sheath flushing in 20 seconds at a 202.7 kPa flushing pressure through a 2.54 mm long seal is 1290.1 ng/(s-m- Pa).
  • the elongate - em- ber 26 (with the distal drive cable inside thereof) is connected at its proximal end to the coupling member 30 by means of the manifold 85.
  • the coupling (and un ⁇ coupling) member 30 connects the distal drive cable 28 to the proximal drive cable 32 which in turn connects to the proximally located components, i.e. the signal processing unit 34 and the motor 36.
  • the imaging system 20 provides a means of coupling and uncoupling the distal transducer side of the system from the proximal components at a point outside the body of the patient.
  • This coupling member 30 provides several advantages for the imaging system 20. Providing for coupling and uncoupling of the distal sensor facili ⁇ tates loading and handling of the drive cable 28 and the sensor assembly 24 into the elongate member 26.
  • the imaging system 20 can utilize larger size, less expensive components for electrical and mechanical transmission proximally from the coupling location where the dimensions of the components are not limited by the constraints of positioning in the coronary vasculature.
  • critical electrical information can be transferred from the rotating drive cable 28 to a less expensive, commercially available, stationary, 50 ohm coaxial cable while maintaining a mechanical link between the motor 36 and the sensor assembly 24.
  • transfer of electrical information by the coupling member 30 is preferably maintained in a controlled impedance environment matched to the transducer.
  • the transmission of mechanical torque can also be transferred proximally to larger, commercially available components that are less expensive to manufacture.
  • a mechanical 'fuse' may be pro ⁇ vided to prevent torsional overload to the drive cable in the body.
  • the electrical and mechanical functions which are united in the same com- ponents in the distal drive cable 28 are split into separate, adjacent cables one for the mechanical trans ⁇ mission and another for the electrical transmission inside the proximal drive cable 32.
  • the electrical signal transmission which in the distal drive cable 28 is conducted by the core wire that is rotating at operating speed, is transferred to a non-rotating coaxial cable connected to the proximal signal processing unit 34.
  • the coupling member 30 may be located approximately 60 inches proximal of the sensor assem ⁇ bly 24 so that it is outside of the patient's body.
  • the coupling member 30 is comprised of a sleeve 101 inside of which is contained a matable coaxial con- nector pair.
  • the coupling member 30 in this embodiment of the imaging system is provided by two assemblies that are mechanically coupled together: a transducer pin assembly 102 that connects to the components on the distal side of the system, such as the sensor assembly 24 and the elongate member 26, and a slip ring assembly 104 that connects to the components on the proximal end of the system, such as the signal processing unit 34 and the motor 36.
  • the coupling member sleeve 101 is formed by a first or distal sleeve portion 106 that is part of the transducer pin assembly 102 and a second or proximal sleeve portion 108 that is part of the slip ring assem ⁇ bly 104.
  • These sleeve portions 106 and 108 may be made of a metal, such as aluminum.
  • the sleeve portions 106 and 108 are held together through the use of a coupling nut 110.
  • the coupling nut 110 provides the means for securing the distally located transducer pin assembly 102 to the proximally located slip ring assembly 104 and their respective coaxial connector halves located therewithin together, as described below, during system operation. This nut 110 may be removed or tightened to disconnect or connect the distal components from the proximally located com ⁇ ponents.
  • the coupling nut 110 slidably fits over the sleeve portion 106 and abuts against a shoulder 112 on the proximal end of the sleeve portion 106.
  • the coupling nut 110 has threads 114 internal thereto oriented in a proximal direction to engage corresponding external threads 115 on the exterior of the slip ring sleeve portion 108, as shown in Figure 15.
  • each of the sleeve portions 106 and 108 there is provided one half of the matable coaxial con ⁇ nector pair.
  • a male component 116 of the matable coaxial connector pair is located in the transducer pin assembly 102 and a female component 117 of the matable coaxial connector pair is located in the slip ring assembly 104.
  • This coaxial connector mated pair 116 and 117 provides for both the electrical and mechanical separation point between the transducer pin assembly 102 and slip ring assembly 104.
  • Mechanical coupling between the mated connector halves is controlled by the spring force exerted by interfer ⁇ ence between the male coaxial connector shield spring contacts 118 and the female coaxial connector shell
  • This spring force generated between the male and female components of the matable coaxial pain allows for torque to be transmitted across the coupling mem ⁇ ber 30.
  • This matable coaxial pair may be a commerci- ally available coaxial connector pair, such as made by Amphenol Corp., modified to be connected in the coupling member 30.
  • This internal coaxial connection is made with a controlled impedance matched to the drive cable 28 and the transducer sensor 42, i.e. with an impedance of 50 ohms. Matching the impedance in the coupling member 30 with these components avoids mismatch signal reflec ⁇ tions, as described above.
  • the transducer pin assembly 102 is connected to the proximal end of the drive cable 28 so as to allow rotation of the drive cable 28 inside the transducer pin assembly 102.
  • a sleeve cap 120 Located at and covering the distal end of the sleeve portion 106 of the transducer pin assembly 102 is a sleeve cap 120 having a passage 121 therethrough.
  • the sleeve cap 120 is secured to the sleeve portion 106 by stamping or a compression fit or other means.
  • the sleeve cap 120 includes a nipple portion 122 which extends distally and in which is located the distal portion of the passage 121.
  • the nipple portion 122 is connected to or may be formed of the sleeve cap 120.
  • a compression 0-ring 129 may be provided between the distal end of the nipple 122 and the manifold 85 to ensure a secure fit.
  • a coaxial connector bearing 130 and a bearing retaining ring 131 Located inside and connected to the sleeve 106 proximally from the end cap 120 is a coaxial connector bearing 130 and a bearing retaining ring 131.
  • the bearing 130 and end cap 120 define an interior portion 132 of the transducer pin assembly 102.
  • the bearing 130 may be made of bronze and oil-impregnated to provide for free rotation inside the pin assembly's outer shell.
  • a drive cable clamp 134 is secured to the drive cable 28 so as to be located in the interior portion 132 of the transducer pin assembly 102.
  • the clamp 134 may be secured to the drive cable 28 by an adhesive or other means.
  • a strain relief sleeve 136 may be connected to or formed on the distal surface of the clamp 134 and extend distally on the drive cable 28 to a location through the nipple 122 (e.g. 0.75 inches) .
  • the strain relief sleeve 136 may be made of teflon.
  • the shell 138 is comprised of a first shell half 139 and a second shell half 140 that can be secured together such as by means of threads. When the shell halves 139 and 140 are secured together, they also secure by compression the clamp 134 between them.
  • the shell 138 include a distal opening 141 and a proximal opening 142, both aligned with the passage 121 so as to receive the drive cable 28.
  • the opening 141 may also receive a portion of the strain relief sleeve 136.
  • a bushing 143 may be located in the proximal opening 142.
  • the bushing 143 may be made of teflon. Connected to the distal side of the shell 138 is the male portion 116 of the coaxial connector pair.
  • the drive cable 28 is thus rotatably secured within the transducer pin assembly 102.
  • the drive cable 28, the clamp 134, the strain relief sleeve 136, the shell halves 139 and 140, the bushing 143 and the male coaxial connector 116 are rotatable.
  • the slip ring assembly 104 which forms the proximal half of the coupling member 30.
  • the electrical signal is transferred from rotatable distal components to non-rotatable proximal components, i.e. the electrical signal transmission which is carried by rotating components distally is transferred to non-rotating components proximally.
  • the electrical signal which is carried by the same components that transmit the mechanical torque distally, is carried proximally by components separate from those that transmit the mechanical torque.
  • a slip ring end cap 158 connects to and covers the proximal end of the slip ring sleeve 108.
  • the slip ring end cap 158 includes a first opening 160 aligned centrally therein and a second opening 162 offset from the first opening 160.
  • Located in and extending through the first opening 160 is a slip ring drive shaft 164.
  • a proximal bushing 166 is positioned in the first opening 160 around the slip ring drive shaft 164.
  • An outer slip ring 167 and an inner slip ring 168 are connected to the distal end of the slip ring drive shaft 164.
  • the outer and inner slip rings 167 and 168 are connected distally to a modified coaxial connector
  • the lead 172 connects to the signal conductor and the lead 174 connects to the reference plane conductor of a coaxial cable in the proximal drive cable 32, as explained below.
  • the distal end of the lead 172 connects to an inner brush ring 176 and the distal end of the lead 174 connects to an outer brush ring 178.
  • the inner and outer brush rings 176 and 178 may be made of brass and may be approximately 0.063 inch wide.
  • An inner spring 180 is located between the inner brush ring 176 and the end cap 158 and an outer spring 182 is located between the outer brush ring 178 and the end cap 158.
  • the inner and outer springs 180 and 182 bias the inner and outer brush rings 176 and 178, respectively, in a distal direction away from the end cap 158.
  • each set of brushes 184 and 186 includes three brushes, (only two brushes of each set are shown in Figure 15) . Each brush is located at 120 degree intervals to the other two brushes in its respective set.
  • the inner set of brushes 184 and the outer set of brushes 186 are slidably held by a brush guide 188.
  • the brush guide 188 is mounted into the inside of the slip ring sleeve 108.
  • the brush guide 188 is a cylindrical plug having two sets of three slots each located at 120 degrees from each other (i.e. for a total of six slots) therethrough for retaining the two sets 184 and 186 of three brushes each.
  • the brush guide 188 also includes a large central opening 189 through which passes the slip ring drive shaft 164.
  • the set of inner brushes 184 bears against and rides on the inner ring 168.
  • the inner ring 168 is used to conduct the signal and is attached to the internal conductor of the coaxial connector 117.
  • the set of outer brushes 186 bears against and rides on the outer ring 167.
  • the outer ring 167 is used for connection to the reference plane signal and is attached to the reference plane conductor in the coaxial connector 117 and/or the sleeve 108.
  • the brushes provide the path for transferring the electrical signal information between the station ⁇ ary inner and outer brush rings 176 and 178 and the rotating inner and outer slip rings 168 and 167.
  • the brushes are made of silver graphite.
  • Silver graphite provides for a brush ma ⁇ terial that is highly conductive and self-lubricating.
  • Relatively large brass slip rings are util ⁇ ized to increase the conductive contact area available between both the slip rings and coaxial connector 117, and the slip ring and brushes. The use of large contact areas reduces electrical resistance and signal loss through the slip ring assembly 104.
  • the slip ring assembly 104 also furnishes the mechanical torque transmission across the coupling member 30.
  • the springs 180 and 182 in the slip ring assembly 104 develop the friction force which supports the torsional load created by the transducer drive cable 28.
  • Mechanical coupling between the mated con ⁇ nector halves 104 and 106 is provided by the spring force generated by the interference between the male coaxial connector shield contacts 116 and the female coaxial connector shell 117. This spring force creates a friction fit between the mated connector pair 116 and 117 and allows torque to be transmitted across the coupling member 30.
  • the torque transmittance in the slip ring assembly 104 is tuned by adjusting the spring force to provide a maximum torque of 3 inch-ounces before relative slip ⁇ page between connector halves 116 and 117 occurs. This provides for a mechanical 'fuse' feature in the system that ensures torque transmittance to the drive shaft assembly and not the pin assembly shell.
  • the coupling member 30, comprised of the transducer pin assembly 102 and the slip ring assembly 104, is easy to use and eliminates or reduces obstruc ⁇ tions in the area of the patient. This facilitates the placement and manipulation of the elongate member 26 and sensor assembly 24 in the coronary vasculature of the patient without the burden of having bulky com- ponents in close proximity to the patient.
  • the assem ⁇ bled coupling member 30 has a cylindrical shape of approximately 0.75 inch in diameter and approximately 4 inches in length. (The transducer pin assembly 102 is approximately 0.75 inch in diameter and 1.75 inch in length.)
  • slip ring assembly 104 uses controlled impedance components for electrical trans ⁇ mission except for a portion of a length less than 0.5 inches. This feature provides for the reduction of signal reflections from impedance mismatches.
  • the distal end of the proximal drive cable 32 connects to the proximal end of the slip ring sleeve portion 108, as shown in Figure 15.
  • the distal end of the proximal drive cable 32 includes a proximal cable sheath 190 that connects to the slip ring assembly sleeve portion 108.
  • the proximal cable sheath 190 may be formed of a section of heat shrink tubing.
  • Provided in the interior of the cable sheath 190 are the drive shaft 192 that connects proximally to the motor 36 and the proximal coaxial cable 194 that connects proximally to the signal processing unit 34.
  • the drive shaft 192 and the proximal coaxial cable 194 are adjacent to each other with the drive shaft 192 aligned approximately along a central axis of the sheath 190 and the coaxial cable 194 offset therefrom. Proximally from the cable sheath 190, the drive shaft 192 and the proximal coaxial cable 194 are enclosed in a proximal cable covering 195.
  • the drive shaft 192 connects to the slip ring drive shaft 164 inside the sheath 190. This connection is made by means of a shaft coupler 196 which may be a tubular member made of DELRIN®.
  • the slip ring drive shaft 164 extends distally from its connection to the drive shaft 192 into the slip ring assembly 104 through the opening 160 in the slip ring assembly end cap 158.
  • the drive shaft 192 is prefer ⁇ ably longitudinally flexible yet torsionally rigid so that it can rotate through operation of the motor and transmit this rotation to the slip ring assembly on to the drive cable and transducer assembly 24.
  • the drive shaft 192 may be a flexible cable made of high tensile strength steel or stainless steel. A commercially available flexible drive shaft may be used, such as S. S. White Industrial Products, Inc. shaft # 098-9.
  • proximal cable sheath 190 Also inside the proximal cable sheath 190 is the distal end of the proximal coaxial cable 194.
  • the distal end of the reference plane conductor 198 of the proximal coaxial cable 194 connects to the proximal end of the reference plane lead 174 and the distal end of the signal conductor 200 of the proximal coaxial cable 194 connects to the proximal end of the signal lead 172.
  • the coaxial cable 194 is preferably flexible and is stationary, i.e. it does not rotate with the drive shaft 192.
  • a matching capacitor 202 may be connected between the signal and reference plane conductors 200 and 198 of the coaxial cable 194 for impedance matching purposes.
  • the matching capacitor 202 would normally have a heat shrunk cover, which is not shown in Fig- ure 15) .
  • the proximal coaxial cable 194 may be a commercially available 50 ohm coaxial cable, such as RG 178 B/N, available from Belden Corporation.
  • the drive shaft 192 and the proximal coaxial cable 194 extend proximally from the proximal cable sheath 190 adjacent to each other inside the proximal cable cover 195.
  • the proximal coaxial cable 194 may be enclosed in an isolation shield 206 that may be made of tin plated copper braid.
  • the drive shaft 192 in enclosed in a non-rotating metallic sleeve 208.
  • the coaxial cable 194 and the drive shaft 192 separate.
  • the branching member 210 may be made of a heat shrink tubing.
  • the coaxial cable 194 extends proximally inside a coaxial cable jacket 212 to coaxial connector 214 that can be fitted to the signal processing unit 34.
  • the drive shaft 192 extends proximally inside a drive shaft jacket 216 to a coupling connector 218 to provide for connection to the motor 36.
  • the motor may be a 40 watt DC rare earth motor, such as manufactured by Maxon Motor Co., Model No. RE035-071-39EAB200A.
  • the signal processing unit 34 includes a pulser which generates the high energy pulses that are converted by the sensor into an acoustical wave that is used for imaging.
  • a full single cycle pulser is used since it gives twice the energy as a half cycle pulser for the same peak voltage and further it gives better settling.
  • a transformer is used for isolation between the high voltage circuitry and the elongate member. High frequency transformers are easier to design for cyclic waveforms with no DC frequency component, if fast settling is important.
  • a full single cycle pulse of the sensor generates a return signal with almost no increase in ringdown time as compared to an impulse. Any increase in the number of cycles beyond one increases the ringdown time almost directly propor ⁇ tionally. For a good image, signal quality is very important.
  • a pulser technique is utilized that provides for a sharper pulse and better ringdown of the signal.
  • Prior pulsers implement a pulse shape of an integer number of half cycles at a given frequency.
  • a pulser that is capable of gener ⁇ ating a pseudo-random pulse would be able to excite the transducer and settle the reflections out by the sequence of pulses at certain amplitudes and at the right time.
  • the size and shape of the sensor window is directly related to the quality of the ultrasonic image obtained.
  • Ultrasonic imaging in two dimensions, i.e. of a cross section of the arterial wall
  • the objective for a good imaging system is to have a thin sharp rotating beam over the distance of interest, e.g., in a direction, y, radial to the artery wall.
  • the beam of course, propagates in all directions.
  • the performance of the beam in the two lateral directions from the radial direction is termed the acoustical optics of the sensor.
  • the beam shape is a function of the distance from the sensor, sensor focus, physical shape and the operating frequency.
  • the resolution in the radial direction is limited by the number of cycles of propagation of the pulse waveform. This time or distance is determined typically by the - 40 dB amplitude points of the waveform, as illustrated in Figure 17.
  • Using a rectangular transducer sensor is one of the keys to making a very small intravascular ultra- sound device for use deep in the coronaries. There are some tradeoffs with respect to circular apertures, but at the very small sizes the best performance is obtained from a rectangular aperture.
  • the beam shape is a function of the housing aperture size in the respective direction. This function is
  • Z A 2 /L
  • Z the near field distance
  • A the aperture size
  • L the wavelength.
  • Z the near field distance
  • A the aperture size
  • L the wavelength.
  • the near field is 1.1 mm in the x directions and 4.5 mm in the y direction.
  • the significance of the near field is that, for an unfocused sensor, the beam width is nearly the aperture width through the length of the near field.
  • the beam In the near field the beam is rapidly changing in all directions. This is from the constructive and destruc ⁇ tive interference patterns.
  • the beam In the far field the beam is more uniform and diverges. The far field behaves as though the source was a point source. For focused crystals the beam can be focused up to the limit of the near field.
  • a focused beam is narrower in the focused region but diverges faster than unfocused outside this region.
  • intravascular ultrasound in the coronary region it is sought to obtain images out to about 5 mm in radius.
  • an advantage of the rectangular shape is that even though the energy is spreading in the x directions, the energy in the y direction remains relatively constant through the distance of the region of interest, as illustrated in Figures 18 - 21.
  • the beam size is quite usable to gener ⁇ ate good intravascular images throughout the radius of interest.
  • the intensity would decrease very rapidly since the beam is spreading uniformly in all directions.
  • the rectangular aperture has better distance vs. energy dropoff along with a larger surface area. For apertures 0.5 mm and smaller the rectangular shape has some characteristics that are more desirable for apertures than circular shapes.
  • the ringdown of the signal is very important and it would be desirable to have a single cycle response to a impulse excitation.
  • the excitation that is used is either a half cycle type impulse excitation or a integer number of sine wave cycles.
  • the resultant objective of the iterative optimization program is to generate a system transfer function that has a smooth phase and magnitude over the widest frequency range. This is achieved by optimizing the value of peak pulse amplitude squared divided by the integral of time weighted magnitude after the peak.
  • the Fourier transform of the excitation is different so that the frequency spectrum of the excitation is different than an impulse.
  • the ideal impulse has constant magnitude frequency com- ponents.
  • This circuit could be implemented using a high speed Digital to Analog (D/A) converter, where the output could be programmed by a computer to a predeter- mined wave form, (see Figure 22) . This output could be amplified to any required level that is required.
  • the optimized waveform is generated over a few hundred nanoseconds and is settled out before the image data is received.
  • FIG. 23 there is depicted an alternative embodiment for the construction of the transducer sensor.
  • a sensor it is desirable to have a configuration that gives a uniform beam from one device to the next and is easy to produce.
  • a uniform beam is necessary for both good repeatability of system performance as well as for implementing other, more advanced data conditioning algorithms necessary for image enhancement.
  • the transducer sensor in Figure 23 is com- prised of a several separate layers including a trans- ducer core, conductive layers bonded to either side thereof, a backing layer and a matching layer.
  • a matching layer 301 (which may be composed of a PVDF material) is larger in dimension than sensor core 44 and includes a overhang 303 on a proximal end. This overhang 303 allows electrical contact between the conductive surface 45a over the sensor core 44 and the center conductor of the coaxial drive cable (not shown) . This provides for both a superior transducer surface with a very uniform active area.
  • This embodiment also significantly facilitates manufacturing. These features can be fur ⁇ ther enhanced through the use of a conductive backing 305.
  • the conductive backing 305 provides an electrical contact between the sensor back surface and the sensor holder.
  • the sensor holder is electrically connected to the drive cable outer conductor (not shown) .
  • the con ⁇ ductive backing can be composed of a number of differ ⁇ ent materials, such as silver, tungsten, copper, gold or a number of other elements or alloys.
  • the matching layer 301 can be made from PVDF, or other materials.
  • PVDF type material having a conductive layer on both the front and back face of the sensor to carry the signals to their connection. Behind the layer on the back side of the sensor an attenuating layer may be needed to absorb the energy coming off in that direction.
  • the two connections would be terminated at the drive cable coaxial electrical connections.
  • a further alternative is to extend the conductive faced matching layer and the conductive faced backing layer from the sensor core to the proximal portion of the drive cable by integrating the flexible circuits into the construction of the drive cable. In order to electrically insulate the two conductive surfaces, an insulation layer is incorporated between the «__yers. This would require no joints in the electrical sensor construction within the catheter.
  • An alternative embodiment of the present invention may combine the functions of a guide wire with those of an ultrasonic imager.
  • a guide wire function is to navigate to a location of interest in a patient's vasculature and to position a catheter over the guide wire into place for a procedure, such as balloon angioplasty. Because it would be desirable to have a device that would image the artery before, during and after such procedures, it would be advant ⁇ ageous to combine the functions of the guide wire and the imaging device. Most catheters are of a coaxial design so that once the catheter is in place the guide wire could be withdrawn and an imaging guide wire put in its place.
  • the drive cable 28 has a diameter of 0.026 inches and accommodates a transducer sensor having an active area of approximately 0.020 x 0.040 inch.
  • the dimensions of the drive cable would be reduced in size to approximately 0.018 inch in diameter.
  • the transducer sensor would be made with a housing aperture close to 0.017 inch. At that size the image resolution would be substantially the same as in the embodiment described above. With image enhancement techniques described elsewhere in this specification, it would be possible to have an image as good as or better than those currently achieved. A thinner transducer having a higher frequency or a different material could be used for the sensor.
  • a distal end of an imaging guide wire 350 is illustrated in Figure 24.
  • a drive cable 352 can be constructed substantially as described above, except that for reducing the size from 0.026 inch to 0.018 inch, two coils and a double braid would be used instead of three coils and an eight wire braid. This has the result of reducing the outer coils and con ⁇ ductors to 0.008 inch leaving 0.010 inch for a center conductor and insulation.
  • the construction of the imaging guide wire would likely depart from that of the embodiment described above and that is in the mounting of the transducer sensor to the drive cable. In the imaging guide wire, the width of the active area of the sensor would be nearly equal to the diameter of the drive cable.
  • This drive cable 352 has a sensor holder 354 mounted at the distal end thereof. Unlike the sensor housing described above having oppositely located windows, the sensor mount 354 of this embodi ⁇ ment would not include a second window located oppositely from the transducer opening. Instead, the mount 354 would provide physical support under the transducer sensor 356. Also, due to size constraints, there would be little room for backing material on the back side of the transducer sensor. This could be com ⁇ pensated for by several different methods.
  • the senor could be made from a copolymer material which has a low acoustic impedance so that no matching layer would be needed to couple to the fluid and further the impedance difference between the backing support and the sensor material would be large enough so much less energy would enter into the backing compared to PZT directly mounted.
  • the energy that enters into the back support can be some ⁇ what dissipated and scattered by using a material such as a porous sintered type metal for the backing support and canceling out reflections with a calibrated pulse waveform.
  • a major problem with copolymer materials is the lower D33 coefficient. (D33 is the dielectric constant in the thickness direction.) This makes a sensor of the same surface area have a larger impedance. This impedance difference could be com- pensated for by using some of the techniques described elsewhere within this specification or active circuitry could be placed next to the sensor to buffer the signal to a lower impedance.
  • PZT materials can also be used in the imaging guide wire embodiment, but they would likely need a front matching layer and a back decoupling layer.
  • the backing configuration may include a half wave decoupler where its impedance is low with respect to both the sensor and backing support. This backing decoupler would work in the opposite manner from that of the matching layer, i.e. where a quarter wave length aids in coupling, a half wave length thickness helps in decoupling energy transfer between two impedances.
  • the electrical connections would be made through the backing support to the back side of the sensor and to the outer conductors of the drive cable.
  • the front connection would be made the same way as in the embodiment de ⁇ scribed above.
  • con- nections would be made using one of the center drive cable wires and connecting the leads directly to the metallized copolymer surface using conductive epoxy or low temperature solder.
  • the imaging guide wire is an intravascular imaging device having an ultrasonic sensor located at a distal end of an intravascular wire sized and adapted to be located within the guide wire lumen of conventional catheters used for intravascular procedures.
  • the imaging guide wire has several significant advantages.
  • the imaging guide wire can utilize the path provided by the guide wire lumen of a conventional catheter to image at the arterial location to which the catheter is advanced.
  • the imaging guide wire may be provided with conventional guide wire features, e.g. a floppy spring tip, to enable the imaging guide wire to be used as both a conventional guide wire for positioning an intravascular catheter as well as imaging features, e.g. a sensor, to enable imaging the intravascular regions accessible thereby.
  • the imaging guide wire 450 includes a tip section 452, a sensor section 454, a drive cable section 456, and a proximal connector section 458.
  • an essential requirement for the imaging guide wire is that it possess an outer profile of a size that allows it to fit through a guide wire lumen in conventional interventional catheters. In catheters that use 0WPWPCCOMSPECPROMPT ⁇ @ A W A A ⁇ N*Y.
  • the drive cable section 456 should be very straight. Electrically, the drive cable 456 is preferably capable of sending a signal from one end to the other with minimum loss.
  • the electrical impedance of the drive cable 456 is preferably in the range of 20 to 100 ohms.
  • An embodiment of the drive cable 456 is illustrated in Figure 48.
  • the drive cable 456 includes a core wire 564, an insulation layer 566, a shield layer 568, and a coil layer 570.
  • the core wire 564 may possess several alternative constructions.
  • the core wire 564 is formed of a solid wire.
  • the core wire may be formed of multi-strand copper or silver-plated copper wires. The latter embodiment provides good electrical characteristics and allows the drive cable 456 to be relativley floppy. However, a multi-strand construction may not provide sufficient longitudinal stiffness.
  • the core wire may preferably be formed of a material having a high modulus of elasticity thereby increasing the longitudinal stiffness.
  • Materials like stainless steel, tungsten, and beryllium copper are preferred. Of these, tungsten is most preferred since it has the highest yield strength and the highest conductivity.
  • a high conductivity material is applied to the outer surface of the core wire 563.
  • Preferred materials for applying to the outer surface of the core wire 563 include silver or copper. Silver is most preferred since it has the highest conductivity. These materials are easily plated to a thickness suitable for good electrical transmission. At high frequencies, electrical current stays close to the surface of a conductor and therefore a 0.001 inch of conductor plating over the core wire is sufficient. In a preferred embodiment, taking into account both mechanical and electrical requirements, the ideal thickness of the coating is less than 0.001 inch.
  • the insulation layer 566 in the imaging guide wire separates the conductive core layer 564 from the conductive shield layer 568.
  • this layer 566 is nonconductive and preferably has as low of an dielectric constant as possible. If a solid wire is used for the core wire 564, it is preferred that a means be incorporated into the insulative layer 566 to restrict longitudinal motion between the core wire 564 and the outer coil 568. If the insulative layer 564 is made of Teflon, a direct bond may be difficult to make between the layers. In this case, movement between the core wire 564 and the outer layers can be restricted at the joint between the drive cable 456 and the sensor housing 354.
  • This sleeve is made out of glass ceramic or other hard, nonconducting material.
  • holes are formed in the Teflon at various patterns to allow glue or other bonding material to be used to connect the layers together.
  • a material other than Teflon can be used for the insulation layer 566.
  • Such other materials include glass strands or a solid extrusion of glass, kynar strands, or a ceramic extrusion. The extrusions would form a solid, uniform layer over the core wire out to a given diameter. The strands would then be expoxied to form a composite layer much like a fiber glass or other composite structure that uses fiber and binder to generate a unique high strength material.
  • the shield layer 568 is located over the insulating layer 566 to make up the outer layer of a coaxial signal cable.
  • the shield 568 can be made from a braid of wires or a coil of wires. In a preferred embodiment, these wires are rectangular silver-plated copper wires. A single layer of coils may be used to provide the smallest diameter drive cable.
  • a low resistance shield layer provides for RF emission shielding and susceptibility. Cable loss is a function of the core and shield total resistance, and accordingly, it is desirable to provide the shield with as low resistance as possible. For this reason, it is preferred that a braid or double coil is used for the shield layer.
  • the outer coil layers 570 are needed for good torque transmission for performing the functions of both the drive cable and guide wire.
  • the outer coil layers 570 are formed of copper or alternatively other metals like stainless steel.
  • a binder is used to bind all the layers together over a length thereof so as to make that portion of the imaging guide wire straight and stiff.
  • This proximal section is from the proximal connector of the imaging guide wire to a location corresponding the end of the guide catheter with which the imaging guide wire would be used. This distance is typically 130 cm. This allows the distal section of the imaging guide wire to be relatively more flexible where it needs to go through tight bends.
  • Another alternative way to provide additional stiffness in a proximal section of the imaging guide wire drive cable 456 is to provide another layer of material over the metal coil outer layer 570 along a proximal section.
  • This additional layer may be formed of other-than-metal strands of glass, kevlar or other high strength materials.
  • the strands would be used in a coil or braid layer over the core cable 570.
  • the strands could then be epoxied to form a composite layer much like a fiber glass or other composite structure that uses fiber and binder thereby resulting in a unique, high-strength material.
  • this can be a dual section composite in which «ne section is made out of one fiber and binder and the other section the same or different fiber and binder or a combination thereof. 5. Imaging Guide Wire Proximal Section
  • a proximal section 458 of the imaging guide wire provides several functions. These functions include a connection for electrical contacts for signal transmission, torque transmission during imaging, torque and longitudinal moWPWPCCOMSPECPROMPT ⁇ ⁇ ⁇ W A A ⁇ N*Yrovided and used in quadrature, thereby allowing the direction to be determined.
  • gray scale encoding may be preferable. Gray scale coding has the property that only one bit changes in going from one state to the next. This prevents errors compared to binary scale for example, since there is no way of ensuring in binary scaling that all bits will change simultaneously at the boundary between two encoded values for binary or other codes.
  • Patterns for both radial acoustic indexing and 3-D lateral indexing may coexist on the sheath. Both patterns could be formed of the sheath material or could be formed of different materials. One pattern could be formed on the inner side of the sheath while the other on the outer side. Also, these patterns could be formed on the same surface.
  • acoustical rotational indexing allows determination of the sensor angular position inde ⁇ pendent of the proximal angular position of a mechanical drive shaft or cable. With this capability, means other than a mechanical drive shaft can be used to scan the vessel with a rotating acoustic beam.
  • a rotating imaging device 408 for scanning of a vessel of a patient with a rotating acoustic beam that is driven by means other than a mechanical drive cable.
  • a rotatable mirror 410 is driven by a rotating hydraulic source 409.
  • the rotating hydraulic source may be a jet and fin type turbine 412.
  • the turbine 412 would propel the mirror 410 in a rotational direction.
  • the speed of rotation of the mirror 410 could be controlled by varying the fluid flow rate. Using fluid, the rotation of a mirror 410 would be very smooth since there would be little friction from rotating shafts compared to mechanical drive devices. Bearings 414 could be provided to provide for smooth rotation. Feedback to the pulser for pulsing and speed monitoring would be provided using an acoustical indexing pattern 416 on the sheath in the rotational direction as described above.
  • a transducer sensor 418 could be mounted either distally or proximally from the mirror and aimed to direct an acoustic pulse toward the angled face of the rotating mirror 410.
  • This configuration provides advantages for combining other functions into the device. With no moving parts over most of the length of the device, there is available substantial room to add other features. For example, it would be possible to integrate a balloon onto the device. The hydraulic course would already be present, and if the balloon is ported to the same fluid used for driving the mirror, all that would need to be done to inflate the balloon would be to control the input pressure independent of the output flow rate. This could control both the inflation pressure as well as the mirror rotation speed.
  • a rotating sensor 420 could be used instead of a rotating mirror by using a slip ring holder 422 to couple the signals to and from the rotating sensor 420 to a signal cable on a catheter, as shown in Figure 31.
  • a hydraulic turbine 424 would drive this device just as described in the embodiment above with the mirror.
  • an acoustic encoding pattern 426 would be included on the sheath portion of the device.
  • This embodiment has the advantage that the sensor 420 could be designed with a thin backing with a hole there ⁇ through large enough for admitting a guide wire 428 through the center of the device. This would provide for over-the-wire placement of the device.
  • processing can range from all analog to all digital.
  • the conditioned signal is acquired through data acquisition, processed by a computer, and displayed through some graphics hardware. This can be accomplished over a computer buss as long as there is a limited amount of trans- ferring being done.
  • Current systems are very basic in the digital conditioning and image processing, and can utilize this approach.
  • FIG. 32 depicts a pipeline structure that provides this architecture.
  • This architecture includes a dual pipeline: one for raw data and another for graphics data.
  • the analog input from the sensor/conditioning is acquired from a high speed data acquisition circuit.
  • This circuit synchronizes the raw data pipeline and transfers the data down the pipeline at a lower speed.
  • the data is passed from one function to the next in real time or near real time speeds.
  • This pipeline basically processes polar data. Since there would be much less data in the polar domain, it would be preferable to process this data as much as possible.
  • These processing functions may include deconvolutions, fourier transform processing, neurocomputing processing or other techniques to enhance the raw data and do feature extraction.
  • the data is converted to a graphics data stream through a large "look up table" (LUT) .
  • LUT essentially performs a polar to rectangular conversion.
  • the graphics data can then be handled in the graphics pipeline. Processing functions performed here are those that preferably should be done in rectangular instead of polar coordinates. These may include edge detection, area calculations/manipulations, logical pixel edge smooth- ing, other area operations, and image overlays.
  • This architecture is ideal for intravascular imaging applications since the data can be acquired and processed from one function to the next with minimal time delay.
  • the pipeline structure is very flexible for feature enhancements and additions, all that needs to be done is to change a cable between the appropriate location to add a new pipeline function.
  • This struc ⁇ ture can accommodate a variable number of pipeline elements, as needed.
  • Some of these pipeline functions include the provision for recording and playback of raw data.
  • a function may be provided for the buffering of raw data as the catheter is advanced or withdrawn through the guide wire lumen of the interventional catheter. This would provide the physician with information about the entire artery from the incision location to the coronaries. This data would likely not need to be viewed at the time it is obtained, however, it would be available for analysis off line after the procedure.
  • the raw data can be stored on an optical disk, e.g. a WORM, that can store up to 1 Gbyte of data. It is estimated that during the relatively short period of time that the imaging guide wire is being advanced or withdrawn through the guide wire lumen of the catheter, the data is being generated at a rate of approximately 100 Mbytes/minute.
  • a small variation on this architecture would include the addition of parallel pipelines. This could be done for example by taking the raw data acquisition output, branching off to a second LUT, and combining the two at the initial graphics pipeline function. This would allow two displays of the same raw data at the same time in different locations on the screen. This would be desirable if a real time enhanced display is desired while at the same time showing a slower 3-D reconstruction or enhanced feature detection.
  • Figure 56 shows the pipeline structure integrated into one type of system environment.
  • Figure 56 shows how the communication portion of the architecture can be implemented to allow the central system CPU to handle pipeline setup and configuration. This allows user input to effect changes in overlays, images and signal conditioning of data. Not every pipeline function may require a direct interface to a common buss. * *An alternative to common bussing is daisy-chained communications.
  • the common processor would be able to perform the setup and configuration t*sks using a serial or parallel communication link.
  • An external controller may be provided in the overall system configuration. This controller may issue commands to the system or may be directly memory-mapped to the functions on the system.
  • the external controller may be connected in a serial or parallel manner and communicate with the system CPU. As with the keyboard, these commands can be queued and processed, or a handshaking can occur for synchronized command execution and communication.
  • the memory-mapped external system control is performed by having the external system take control of the system common buss and accessing the hardware and memory directly.
  • a major goal in acoustic imaging is high resolution of the image. It is desired to have an image with features as well defined as possible.
  • One of the limitations to the image resolution is the attenuation of the signal with frequency. If there were a much higher signal to noise ratio, a higher frequency could be used, yielding a higher resolution image for a given size aperture device. Alternatively, a smaller device could be produced having the same resolution. Resolution may be defined as the distance at which two points are barely distinguishable. With acoustic beams using traditional imaging techniques, the resolution of the image is a function of the beam width at the points of interest.
  • the beam is of the form of an airy disk for a circular aperture and a mathematical Sine 2 function for a rectangular aperture.
  • convolution is the summing in time of a finite pattern input into a output pattern using a transfer function.
  • Deconvolution is the reverse process where from a given output the input pattern is found.
  • the accuracy of the determined input is a function of the accuracy of the measured output function and the accuracy of the transfer function.
  • a transfer function also exists for acoustical imaging but is in two dimensional space and time as well.
  • the two dimensional space transfer function is proportional to the intensity of the acoustical beam at a given radius. This problem is more difficult than the one above but the same basic principles apply.
  • a knowledge of the beam shape and point intensity as a function of time is the major variable in performing a deconvolution on the acquired information.
  • the beam shape and point intensity values are a function of sensor aperture, surface, uniformity, sensor construction tolerances, and diffraction/reflection of where the beam has come from and gone though. To know the beam values to any great detail is a very time consuming task if they are computed or measured.
  • the beam shape is varying rapidly as distance from the sensor changes.
  • the beam In the focused region and in the far field, the beam is more uniform and predict ⁇ able. In these regions deconvolution will be of some use.
  • this tech- nique In the other areas of the beam as sensor tech ⁇ nology produces more uniform sound beams, this tech- nique will enhance the entire image. For the current system, most of the imaging is done in the far field in the rotationally lateral direction.
  • the resulting benefits from this routine are a sharper apparent resolution and a higher signal to noise ratio.
  • the side lobes magnitude and the main beam size are the main determinates of the resolution of the image. Deconvolution will improve upon the limits set by both of these factors.
  • the noise is reduced if the noise waveform has a small similarity with the acoustic transfer function, which is mostly the case.
  • the standard technique for performing a deconvolution is to use Fourier analysis. This is done by taking the Fourier transform of the output, dividing this by the Fourier transfer function, taking the inverse Fourier transform, and using the result. For a system where the transfer function is varying with time and space, the exact procedure is more complicated than this simple example. This is a very time consuming routine for current conditioning equipment, but a parallel network of processors could be built into the previously mentioned data pipeline in a direct or a parallel manner depending on how fast the process is and how much improvement in image results.
  • Neural Network Feature Detection Feature detection is a very complex problem. The goal is to enable the computer to identify and label various layers of the artery and atheroma. A type of atheroma that is truly identifiable from the pattern displayed is calcific plaque. This is un ⁇ mistakable to the eye as indicated by a bright area with a blocked out region behind. Even though it is easy for a human to learn how to identify this feature of the displayed image of an atherosclerotic diseased artery, it would be very difficult to write a program to identify and mark the region. Image processing and technology for object and feature detection is currently in a very early stage as far a technical sophistication. Most computer object detection is per- formed by performing a sequence of image transformation operations. The correct sequence is usually found iteratively by trying different combinations of the operations from a library of operations. Correct object detection is still a probabilistic event where certain combinations have a higher hit ratio than others.
  • Neural networks are a scalable architecture defined as a number of weighted summing nodes organized in a layered manner.
  • Figure 33 there is depicted a diagram illustrating interconnections of a three layer network. Each layer node feeds its value forward as well as feedback to other layers. They can have any number of layers as well as any number of nodes per layer.
  • the major advantage to neural networks is that the correct weighings on the input nodes can be determined by a learning process. The network is programmed by exposing it to inputs and telling it the correct output.
  • the network can determine what the weighing values need to be to give the most accurate answer. Determining the features in an ultrasound scan of an artery using neural networks is the best approach. After the network has learned the correct responses, a circuit could be developed to process the data in real time. Initially the network would be designed to operate on the data going through the raw data pipeline. Here, the network could work on a limited number of vectors at one time as inputs. This would keep the circuitry down to a practical level of parts. Handling the input raw data from one vector would require handling 500 points. For a number of complete vectors to be processed a large number of inputs result. A more reasonable approach is to use a network that processes a limited number of points from each vector and use more vectors. A circuit handling 25 radial points and 5 to 10 vectors could be developed with presently available hardware and yet contain all the neighborhood information from the acoustic beam that would be useful in reducing the data to an output feature.
  • the transmission of the electrical signal from the imager elongate shaft to the proximal electronics is provided by a mechanical contacting slip ring assembly 104.
  • the slip ring assembly provides excellent transmission, in alternative embodiments, it would be advantageous, and potentially a simplification of the interface, if a non-contacting means were employed to couple electrical signal between the rotating and non- rotating parts.
  • Two alternative means for providing this transmission link are capacitive coupling and magnetic coupling.
  • FIG. 57 A first alternative embodiment of the signal coupling assembly is shown in Figure 57.
  • This embodiment employs capacitive coupling.
  • Capacitive coupling can be used when the capacitance is large enough between the rotating and non-rotating contact rings.
  • the capacitance is a function of the surface area, the gap distance and the effective dielectric constant. For a 30 Mhz signal, 100 pF would be more than enough capacitance to provide suitable coupling. A values greater or less than this would work also.
  • Capacitive contact rings 600 are shown to be longitudinally spaced, although alternatively, the rings 600 could be positioned radially. If positioned radially, one ring would be placed on the inner diameter and the other contact ring on the outer diameter of the assembly. With either capacitive or magnetic non- contacting slip rings, the mechanical energy is transferred by a keyed configuration or a friction fit. There are other means that could be used to transfer the mechanical energy, for example by a magnetic drive. By making the rotating contact rings out of a magnetic material or by placing a permanent magnetic in the assembly, the slip and drive shaft could be rotated without physical contact. A similar principle is used in stepper motors.
  • Figure 58 shows an embodiment of a magnetic non-contacting slip ring assembly 604.
  • This alternative embodiment includes a rotating and a non- rotating transformer coil 608 and 610. The energy is transferred by magnetic fields through the magnetic circuit.
  • a consideration with this embodiment is air gaps reducing the coupling between the two coils. For this reason, the gap area 612 is enlarged to minimize this problem.
  • Imaging device dependant information is entered manually or by shunting contact pins to provide some device type information. These parameters may be as simple as device type, frequency, device serial number, and production information. Other imaging parameters that are sensor dependant include those that would be used for a calibrated waveform pulser or coefficients that describe the acoustic waveform that would be used in image enhancement routines, as described above. This information must be entered into the system before imaging begins. However, it is not very user-friendly to force the user to enter the information manually into the system.
  • a feature that can be incorporated into any of the embodiments discussed herein provides for automatic imager information entry.
  • An embodiment incorporating this feature is shown in Figure 59.
  • the device dependant information is stored in a non ⁇ volatile storage medium 614.
  • a storage medium is an EEPROM.
  • the information is available when the imaging catheter or imaging guide wire is plugged into the driving apparatus and control system 38.
  • the means for connection could be direct wiring or an isolated reading means could be used.
  • a minimum of two wires are typically needed to transfer information.
  • Common serial EEPROM devices are available that operate off three wires and have a wide range of storage capacity. Also potentially available but not as desirable is parallel access non-volatile storage.
  • Another easy method of entering this information is to provide a separate data card or disk. This can be plugged into the system and the computer control can read the information before imaging begins.
  • Figure 60 shows a motor box 620 attached to the edge of a patient table 622.
  • a gooseneck device 624 extends the catheter connector over the table 622 and holds the imaging catheter or guide wire in place. It is important to keep the imaging catheter or guide wire straight while imaging.
  • This gooseneck type device 624 allows movement back and forward easily to follow to doctor as the imaging is performed. Before and after imaging, the gooseneck device 624 and imaging catheter can be pushed back out of the way to eliminate some of the clutter on the patient table 622 as well as to protect the imaging drive shaft from getting bent.
  • This gooseneck device 624 could have cables internal or external to its supporting structure.
  • the goose neck device 624 preferably possesses a physical configuration and structure that can support a weight at a distance and be moved between two three-dimensional points.
  • Ultrasound imaging in catheter labs is currently performed by wheeling an ultrasound imaging system into the cath lab, setting up the system and catheter and then imaging.
  • a direct connection is made between the motor 630 and conditioning unit (MCU) 632.
  • the motor is typically in a cabinet on a cart and the MCU is mounted on the table.
  • the proximal drive cable is laying across the floor and can be tripped on if the system is not next to the doctor.
  • the MCU should have a connector on the floor, the table or hanging from the ceiling.
  • a connector 634 is mounted to the table 622 so the MCU 632 cable follows the table 622 when it is moved.
  • the system also has a plug 636 and could be unplugged for portable configurations.
  • Other system configurations include a rack mount system integrated into existing or modified catheter lab control hardware. In this configuration, the system is already on-line and when the doctor needs to perform an imaging procedure, the MCU 620 is mounted to the table 622 and plugged in. At this time, imaging could begin.
  • the external controller could issue the system commands and the video outputs are multiplexed and displayed at the doctors overhead screen.
  • Another alternative configuration provides for the system to be located within the MCU 620. This could be provided if the system electronics were small enough to fit within a reasonable sized box to place on the table rack.
  • the system electronics were small enough to fit within a reasonable sized box to place on the table rack.
  • a manual interface on the unit and that can be operated remotely from an external controller.
  • a small monitor can be provided internally, but the preferred method of viewing would be externally on the overhead monitor.
  • there is a plug for communications, video signals and power there is a plug for communications, video signals and power.

Abstract

A device for ultrasonic imaging, and methods for the use and manufacture thereof, particularly of small coronary vessels. The device comprises an elongate member (26) with a distal end (28) that can be positioned within a small vessel of a patient's body while a proximal end (32) is located outside the body, a transducer located at a distal end of the elongate member and operable to scan the distal coronary vessels with ultrasonic pulses, and a signal processor (43) connected to a proximal end of the elongate member and to the transducer for generating and receiving pulses to and from the transducer. A motor (36) may also be connected to the proximal end of the elongate member for rotating the transducer. Control unit (38) operates the motor and the signal processor.

Description

Intravascular Imaging Apparatus and Method
BACKGROUND OF THE INVENTION
This invention relates to an ultrasonic imaging device and methods for use and manufacture thereof, and particularly to an ultrasonic imaging device positionable in coronary vessels to obtain images thereof.
Ultrasonic imaging of portions of a patient's body provides a useful tool in various areas of medical practice for determining the best type and course of treatment. Imaging of the coronary vessels of a patient by ultrasonic techniques could provide physicians with valuable information about the extent of a stenosis in the patient and help in determining whether procedures such as angioplasty or atherectomy are indicated or whether more invasive procedures may be warranted. However, obtaining ultrasonic images of the distal coronary vessels with sufficiently high resolution to be valuable for making medical decisions, such as described above, requires overcoming several significant obstacles one of the most significant of which relates to the size of the ultrasonic sensing device.
Obtaining ultrasonic images of high resolution of a body organ generally requires bringing an ultrasonic sensor (i.e. a transmitter/receiver) sufficiently proximate to the organ and scanning the organ with ultrasonic pulses. Ultrasonic imaging of organs deep within the body that are surrounded by other, relatively dense organs and tissues requires connecting a sensor on a probe and positioning the sensor and the probe near or even into the organ. The heart and the vessels connected to it are organs of this type. Because it is a well known technique to insert catheters, guide wires and probes into the coronary vasculature from remote sites via arteries, such as the femoral artery, and further because some of the information of interest to the physician is the extent of stenosis on the inside walls of the coronary vessels, it would be desirable to be able to position an ultrasonic sensor connected to a probe into the distal regions of the coronary vasculature via a remote arterial site, such as the femoral artery, to obtain ultrasonic images of the coronary arterial walls. The vessels in the distal regions of the vascular tract that would be useful to image include the coronary arteries, branch vessels stemming from the external carotid artery such as the occipital and the arteries leading to the vessels of the head and brain, splenic, and the inferior mesenteric and renal arteries leading to the organs of the thorax. To be positioned in these regions, the size of an ultrasonic sensor and probe must be relatively small not just to traverse the arterial vessel but also to avoid occluding the vessel lumen. When a device, such as a catheter, probe, or sensor, is positioned in a blood vessel, it occupies a volume which restricts blood flow within the vessel as well as in vessels proximate thereto. When a device is positioned within an arterial vessel, the blood flow through the vessel is restricted to an annular region
(i.e. the area of "ring-'-shaped cross section) which is effectively created between the outer perimeter of the device and the inner wall of the vessel. This would normally not present a problem in large arteries with large blood flows, such as the femoral arteries of the legs, or the aorta, or in very proximal coronary arteries. In these large arteries, any restriction caused by the device would be relatively small and the blood flow would be relatively large. However, in small arteries in remote locations, such as the occipital that leads to the brain, or the coronary arteries of sizes of 3.0 mm or less that lead to the right and left sides of the heart, any restriction of blood flow must be minimized. The consequences of occluding these small vessels can cause a loss of flow in the coronary arteries of the heart which may have several adverse effects, such as severe chest pains, or physiological changes such as arrythmia, ischemia, and tachycardiac response. These effects may be threatening to the patient and further, once begun, may be difficult to stabilize.
Moreover, not only are these latter vessels very small but these vessels are also those in which there might also be restrictive disorders, such as atherosclerosis. Atherosclerotic disease as well as other thrombus formations which occlude blood flow occurs in these smaller arteries due to the hemodyna ics of the blood tissue interface. Reflecting this fact is that presently angioplasty is primarily performed in vessels of a size range of 2.0 to 3.5 mm in diameter. Such disorders would diminish the cross sectional area of these vessel lumens even more.
Therefore, a significant obstacle to using an intravascular probe device to obtain ultrasonic images of such vessels is that the probe should be sufficiently small in dimension so as not only to be positioned in these small, possibly partially occluded arteries, but also to be sufficiently small so as not to totally or almost totally occlude the lumen of the vessel into which it is positioned. Accordingly, for an ultrasonic sensor device to be used for distal coronary applications, it must be small enough to be suitably positioned in the coronary vessels and to permit a sufficient blood flow therearound. For use in the distal coronary vasculature, the exterior dimension for a sensor device should be approximately 0.040 inches (1 mm) in diameter to provide an annular region of flow in even the most distal vessels.
Ultrasonic imaging devices intended to be placed in the vascular system have been disclosed in prior patents (e.g. U.S. Pat. No. 4,794,931). However, these prior devices have had numerous drawbacks that limited their utility for the most part to uses in only the peripheral vasculature and not in deep coronary arteries. Prior devices, having diameters ranging from 3.5 French (1.2 mm) and up, would be limited by their size to only very proximal coronary arteries. Prior devices, having diameters ranging from 4.5 French (1.5 mm) and up, would be limited by their size to only very proximal locations of coronary arteries, peri¬ pheral vessels, or very proximal organ vessels. Furthermore, in addition to these limitations, prior ultrasonic probe devices have produced images lacking in sufficiently high detail and resolution to provide useful information.
There are significant obstacles to making an ultrasonic probe device with dimensions sufficiently small to fit into distal coronary vessels and yet possessing the necessary mechanical and electrical properties required for high quality ultrasonic images. For example, in order to position a probe device in a deep coronary vessel from a remote percutaneous site such as via the femoral artery, the probe device should possess a high degree of longitudinal flexibility over its length. The vessel paths of access to such deep coronary vessels, as well as the numerous branches which stem from these vessels, may be of an extremely tortuous nature. In some areas within the vascular system, an ultrasonic probe device may have to transverse several curvatures of radius of 3/16 of an inch (4.7 mm) or less. Thus, the probe device should possess a high degree of flexibility longitudinally over its length to enable it to transverse virtually any curvature of the vascular tract.
Another desired mechanical property for the probe device is stable torsional transmittance. If the device is to include a rotating ultrasonic sensor at a distal end to make radial scans of the entire cross section of the coronary artery, it should not only be flexible longitudinally, but should also be stiff torsionally. Rotation of the ultrasonic device should be achieved so that a drive shaft extending to the sensor does not experience angular deflection which might cause image distortion. Due to the continuous angular motion which dictates the location at which an ultrasound sensor scans, if angular deflection occurs at the distal end of sensor drive shaft, it can result in an artifact of angular distortion that becomes apparent on the ultrasound displayed image. This arti¬ fact can occur if the rotating sensor drive shaft experiences "whip". "Whip" may be defined as the angular deceleration and acceleration of the sensor drive shaft as a result in shaft angular deflections during rotation. As the transducer drive shaft is rotating it may undergo angular deflection if the drive shaft's torsional stiffness is low enough to make the drive shaft susceptible to dynamic changes in torsional load. It may also undergo angular deflection if the • dynamic torsional loads are high and varying.
During operation, relative changes in torsional load should be minimal, therefore any induced 'whip' could be attributed to a shaft with a low torsional stiffness. The acceleration and decelera¬ tions associated with shaft whip can be described by the energy change from kinetic to potential under vary¬ ing torsional load conditions. For example, as a sensor drive shaft encounters additional torsional resistance its angular velocity drops causing a deceleration and shaft angular deflection. When the shaft is free of the added resistance, the energy stored in the shaft, in the form of potential energy from the angular deflection and shaft stiffness, is released causing an angular acceleration and increase in the shaft's angular velocity.
Image quality and accuracy is dependent on constant sensor angular velocity. Image construction assumes a constant sensor velocity, therefore relative acceleration or deceleration between the expected and actual sensor angular velocity will cause image distortion.
Even if a sensor possesses the aforementioned minimal size and mechanical properties, the value of the device depends upon the quality of the ultrasonic image which in turn is a direct function of both the acoustic pulse signal and the electrical signal trans¬ mission. Therefore, in addition to the mechanical properties necessary for locating and rotating a sensor, the device should also provide a high quality electrical and acoustic signal. This may include several specific properties, such as a high signal to noise ratio of the electronic signal, impedance match¬ ing of the overall system without the need for internal electronic matching components, and minimization of voltage requirements to attain a signal of sufficient quality to provide an image.
Accordingly, it is an object of the present invention to provide a device that overcomes the limitations of the prior art and which enables the ultrasonic scanning of small diameter body vessels with a transducer probe that can be positioned therein. It is a further object of the invention to provide an apparatus, and methods for use and manufac¬ ture, that enables obtaining ultrasonic image informa¬ tion of high resolution or quality.
SUMMARY OF THE INVENTION
The present invention provides a device for intravascular ultrasonic imaging, and methods for the use an manufacture thereof, comprising an elongate member with a distal end that can be positioned within a vessel of a patient's body while a proximal end is positionable outside the body. The device also in¬ cludes a transducer located at a distal end of the elongate member and a signal processor connected to a proximal end of the elongate member for generating pulses to and receiving from said transducer. The device preferably includes a motor for rotating the transducer and a drive cable for connecting the transducer to the motor and the signal processor. The drive cable is operable to transmit electrical signals to and from the transducer.
BRIEF DESCRIPTION OF THE FIGURES
Figure 1 is a schematic representation of a presently preferred embodiment of the ultrasonic imaging apparatus. Figure 2 is a longitudinal vertical sectional view of a distal portion of the ultrasonic imaging apparatus depicted in Figure 1.
Figure 3 is a sectional view of the -aistal portion of the ultrasonic imaging apparatus along lines 3 - 3' in Figure 2.
Figure 4 is a sectional view of the -distal portion of the ultrasonic imaging apparatus along lines 4 - 4' in Figure 2. Figure 5 is a plan view of a portion, parti¬ ally disassembled, of the drive cable.
Figure 6 is a sectional view of an embodiment of the elongate member of the system depicted in Figure 1.
Figure 7a a sectional view alone lines 7 - 7' of the embodiment of the elongate member depicted in Figure 6 illustrating a first alternative indexing function construction. Figure 7b a sectional view alone lines 7 - 7' of the embodiment of the elongate member depicted in Figure 6 illustrating a second alternative indexing function construction.
Figures 8a and 8b are block diagrams of processing steps related to acoustical indexing.
Figure 9 is a sectional view of the alterna¬ tive embodiment of the elongate member shown in Figure 6 illustrating a first flushing method.
Figure 10 is a sectional view of a second alternative embodiment of the elongate member illus¬ trating a second flushing method.
Figure 11 is a sectional view along lines 10 - 10' of the embodiment in Figure 9.
Figure 12 is a sectional view of a portion of a third alternative embodiment of the elongate member illustrating a third flushing method.
Figure 13 is a plan view of the uncoupling member shown in Figure 1.
Figure 14 is a longitudinal vertical sec- tional view of the transducer pin assembly shown in Figure 13.
Figure 15 is a longitudinal vertical sec¬ tional view of the slip ring assembly shown in Figure 13. Figure 16 is a plan view with a partial sec¬ tional view of the proximal drive cable shown in Figure 1.
Figure 17 is a diagram of signal amplitude versus time for the pulser in a first embodiment of the present invention.
Figure 18 is a diagram of signal intensity versus radial distance from the sensor perpendicular to drive direction. Figure 19 is a diagram of signal intensity versus radial distance from the sensor perpendicular to drive direction.
Figure 20 is a diagram of signal intensity versus the position along the cross section A - A' of Figure 18.
Figure 21 is a diagram of signal intensity versus the position along the cross section B - B' of Figure 18.
Figure 22 is a block diagram of the calibrated waveform of the pulser.
Figure 23 is a perspective view of another embodiment of the transducer sensor.
Figure 24 is a plan view of the distal end of an imaging guide wire which is another embodiment of the present invention.
Figure 25 is plan view of yet another embodi¬ ment of the sensor housing of the present invention.
Figure 26 is plan view of still another embodiment of the sensor housing of the present invention.
Figure 27 is plan view of another embodiment of the present invention for 3-D imaging.
Figure 28 is a view of a distal section of an alternative embodiment of the elongate member with variations represented for 3-D indexing. Figure 29 is a cross sectional view of the embodiment shown in Figure 28 along lines A - A'.
Figure 30 is a top view of a the distal end of yet another embodiment of the present invention that utilizes an alternative drive mechanism.
Figure 31 is an alternative embodiment of that shown in Figure 30.
Figure 32 is a block diagram of the data and graphics pipeline of an alternative embodiment of the present invention.
Figure 33 is a diagram illustrating utiliza¬ tion of a neural network architecture in an alternative embodiment of the present invention.
Figure 35 is a side elevational view of a first preferred embodiment of an imaging guide wire. Figure 36 is a side elevational view of a preferred embodiment of a sliced transducer sensor for use in the imaging guide wire of Figure 35.
Figure 36a is a cross sectional view of the sliced transducer sensor of Figure 36.
Figure 37 is a top view of the sliced transducer sensor of Figures 36 and 36a.
Figures 36, 38, and 39 each show a top view of alternative constructions of the sliced transducer sensor of Figures 36 and 36a.
Figure 40 is a side elevational view of the preferred embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating a sheath over the transducer sensor. Figure 40a is a cross sectional view along line A - A' of the transducer sensor of Figure 40.
Figure 41 is a side elevational view of an alternative embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating an exponential matching layer. Figure 41a is a cross sectional view along line A - A' of the transducer sensor of Figure 41.
Figure 42 is a side elevational view of a preferred embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating a formed sheath matching layer.
Figure 42a is a cross sectional view along line A - A' of the transducer sensor of Figure 42.
Figure 43 is a side elevational view of an embodiment of the transducer sensor for use in the imaging guide wire of Figure 35 incorporating a splined attenuation backing support.
Figure 43a is a cross sectional view along line A - A' of the transducer sensor of Figure 43. Figure 44 is a side elevational view of an embodiment of a wedge transducer sensor for use in the imaging guide wire of Figure 35.
Figure 44a is a cross sectional view along line A - A' of the transducer sensor of Figure 44. Figure 45 is a side elevational view of an embodiment of a multiple transducer sensor for use in the imaging guide wire of Figure 35.
Figure 45a is a cross sectional view along line A - A' of the transducer sensor of Figure 45. Figure 46 is a side elevational view of an embodiment of the distal tip construction of the imaging guide wire of Figure 35.
Figure 47 is a side elevational view of an alternative embodiment of the distal tip construction of the imaging guide wire of Figure 35 incorporating a locking tip feature.
Figure 48 is a perspective view, partially disassembled, of an embodiment of the drive cable construction of the imaging guide wire of Figure 35. Figures 49, 50, and 51 each show a perspective view of alternative embodiments of the proximal end section of the imaging guide wire of
Figure 35.
Figure 52 is a side elevational view of an extension wire for use with the imaging guide wire of Figure 35.
Figure 53 is a side sectional view of a drive interface for making the electrical an mechanical connections for driving the imaging guide wire of
Figure 35. Figures 54a and 54b each show alternative embodiments of supporting means for the proximal end section of the imaging guide wire of Figure 35.
Figure 55 is a side sectional view of a holder apparatus for the imaging guide wire of Figure 35.
Figure 56 is a flow chart representing an embodiment of the pipeline architecture for the imager of Figures 1 or 35.
Figure 57 is a side sectional view of an alternative embodiment of the slip ring assembly of
Figure 15 incorporating a capacitive non-contacting slip ring assembly.
Figure 58 is a side sectional view of an alternative embodiment of the slip ring assembly of Figure 15 incorporating a magnetic non-contacting slip ring assembly.
Figure 59 is a side sectional view of an alternative embodiment of the imager of Figures 1 or 35 incorporating an EEPROM into the imager to store essential product information.
Figure 60 is a perspective view of an embodiment of a cath lab patient table and accessories for use with the imager of Figures 1 or 35.
DETAILED DESCRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS
I. THE SYSTEM Referring to Figure 1, there is depicted a schematic representation an ultrasonic imaging system 20. The system comprises a sensor assembly 24 located at a distal end of the system 20 at a distal end of an elongate member 26. The elongate member 26 can be percutaneously positioned in the cardiovascular system of a patient via a remote site such as the femoral artery so the distal end of the elongate member is located in or close to the remote site while a proximal end extends out the body of the patient. The elongate member 26 includes at a distal end thereof the sensor assembly 24. The elongate member 26 further includes means for transmitting an electrical signal between the sensor assembly 24 located at the distal end thereof and the proximal end extending out of the body of the patient. The elongate member 26 further includes means for operating the sensor assembly to make scans of the remote vessel site. In a preferred embodiment, the means for operating the sensor assembly 24 and the means for transmitting a electrical signal to and from it are provided by a distal drive cable 28 located inside the elongate member 26. The sensor assembly 24 is connected to a distal end of the distal drive cable 28. The distal drive cable 28 is connected at its proximal end to a coupling member 30 which connects to components located at a proximal end of the sy tem 20. Specifically, the coupling member 30 serves to releas- ably couple the distal drive cable 28 to, and uncouple the distal drive cable 28 from, a proximal drive cable 32. The proximal drive cable 32 includes a first leg 33 that connects to a signal processing unit 34 and a second leg 35 that connects to a motor 36. Connected to both the signal processing unit 34 and the motor 36 is a control unit 38 that serves to operate the motor 36 and the signal processing unit 34. These components are described in further detail below. This embodiment of the present invention is particularly adapted for ultrasonic diagnostic imaging in the small, distal vessels of a human patient. These vessels typically have diameters of only up to 4.5 mm diameter. In particular, the present embodiment is adapted for use in deep organ vessels where the residual diameter of the vessel may be 1.5 mm or less. However, it should be understood that embodiments of present invention may be readily adapted for use in vessels having other dimensions with corresponding advantages in these other size vessels as well. In the preferred embodiment for use in vessels having a diameter of approximately 3.5 mm with potential stenosis resulting in diameters of down to 1.2 mm, the overall maximum diameter of the distal portion of the ultrasound imaging system is preferably not more than approximately 3.2 French (1.07 mm or 0.42 inch) and preferably the distal portion of the system has an overall diameter of less than 3.0 French (1.0 mm). In operation, the signal processing unit 34 generates electrical pulses that are transmitted to the sensor assembly 24 via a proximal electrical transmis¬ sion cable inside the proximal drive cable 32 (as further described below) and the distal drive cable 28. The signal processing unit 34 also receives electrical pulses back from the sensor assembly 24 via these cables. At the same time, the motor 36 operates to rotate a proximal drive shaft located inside the proximal drive cable 32 (as described below) which in turn rotates the sensor assembly 24 to which it is coupled via the distal drive cable 28. Rotation of the sensor assembly 24 while pulsing and receiving the reflections effects an radial ultrasonic scan of the area proximate to the sensor assembly 24. In this embodiment, the motor 36 operates to rotate the transducer assembly 24 at speeds ranging from 500 to 1800 RPM, with a preferred rotational speed of approximately 1000 RPM.
The design and construction of the various components of the system are preferably computer modeled and iterated to provide optimum overall system performance. For example, for optimum performance, impedance throughout the overall system from the signal processing unit 34 to the sensor assembly 24 is carefully matched to eliminate reflections at all interfaces caused by impedance mismatch. By eliminating reflections in the system, there is a faster settling of the pulses since reflections can cause ringing of the pulse thus reducing the radial resolution. Because there is limited potential for adjustment of the impedance at the sensor assembly 24 end of the system, consistent with other requirements, the rest of the system components proximal from the sensor assembly 24 are matched to it. In this embodiment, a system impedance of 50 ohms is selected. With a system impedance of 50 ohms, readily available industry standard components, such as coaxial cables may be used for proximal equipment. A suitable sensor can be constructed and used that is matched to this impedance and that has an active surface area of 0.50 mm2. Similarly, the distal drive cable 28 and the proximal drive cable 32 are constructed with an impedance of 50 ohms. The impedance of the coupling member 30 is not specifically matched to that of the rest of the system. The coupling member has a low resistance, e.g. less than 0.5 ohm. However, the length of the unmatched impedance portion of the coupling member is made to be only approximately 0.75 inch. At the preferred operating frequency of 30 Mhz, a segment of this length with an unmatched impedance can be present in the electrical transmission conductor of the system without causing a significant reflection. The signal processing unit 34 (including the pulser) , at signal voltage levels, is also selected with impedance matched to the system impedance, i.e. 50 ohms, to eliminate reflections. With a matched termination at the signal processing end of the system, the signal is insensitive to the length of the cable members. This provides the advantage that the motor 36 and signal processing unit can be positioned out of the way of the physician, e.g. under a table or other convenient place.
II. THE SENSOR ASSEMBLY
Referring to Figure 2, there is depicted a vertical longitudinal sectional view of a distal portion of the imaging system 20 including the sensor assembly 24 of a first presently preferred embodiment. The sensor assembly 24 is located inside the elongate member 26. The sensor assembly 24 is connected at a proximal end thereof to the drive cable 28.
The sensor assembly 24 includes a sensor housing 40 in which is mounted a transducer sensor 42. The transducer housing 40 is a hollow, generally tubular member having a cylindrical wall and open ends. The housing 40 has dimensions that provide for posi¬ tioning and rotating inside of a lumen 43 of the elongate tubular member 26. In a preferred embodiment, the housing 40 has an outside diameter of 0.030 inches. This may be equal to the diameter of the drive cable 28. In a preferred embodiment, the housing 40 is a metallic tube of 304 stainless steel. The transducer sensor operates in alternating pulsing and sensing modes. In the pulsing mode, when excited electrically, the transducer sensor 42 creates a pressure wave pulse which travels through the elongate member into the arterial environment. In the sensing mode, the transducer sensor 42 produces an electrical signal as a result of receiving pressure waves reflected back to the transducer. These reflections are generated by the pressure waves traveling through changes in density in the arterial environment being imaged. The electrical signals produced by the transducer sensor 42 are transmitted back to the signal processing unit 34 for generation of images of the arterial environment by methods known in the art and as further described below. Referring to Figures 2 and 3, the transducer sensor 42 is constructed from several distinct layers including a transducer core material 44 having a first and a second metallized electrically conductive surface layers, 45a and 45b, bonded thereto, a matching layer 46, a backing layer 47 bonded to the metallized sur¬ faces, and one or more adhesive layers. This con¬ struction provides a transducer sensor with an active area of approximately 1.0 x 0.5 mm. The impedance of the transducer is a linear function of the active area so for a device having an active surface area of about 1.0 x 0.5 mm, the impedance is approximately 50 ohm.
Transducer Sensor Core Material:
In a preferred embodiment, the transducer core 44 of the tranducer sensor 42 is a flat rect- angular piece of PZT (Lead Zirconate Titarate) type ceramic material. Such PZT material has an acoustic impedance of mid 20's and a speed of sound of about 5000 m/s. At this speed, the thickness for a 30 MHz sensor is about 0.003 inch. At this thickness, PZT materials should be selected with small grain sizes so that shorts are not generated during processing. The PZT material is cut to a rectangular shape of 0.5 x 1.25 mm. The active area after wires and a matching layer are attached is approximately 0.5 x 1.0 mm. Transducer Sensor Conductive Layers;
The first and second conductive layers, 45a and 45b, are positioned respectively on each face of the transducer core 44. The conductive layers 45a and 45b may be composed of a number of electrically conduc¬ tive materials, such as gold, silver, copper, or nickel. However, a number of other materials, elements or alloys are suitable. Additional layers may be needed under each conductive layer to provide for adhesion to the core material, e.g. , using chromium under gold. For good performance, the resistance of the conductive layers should be less than 1 ohm from one end thereof to the other.
Transducer Sensor Matching Layer: The matching layer 46 provides an impedance transformation between the transducer sensor 42 and the fluid therearound to allow a better coupling of energy into the fluid. This transformation is frequency dependent. A matching layer may be used where a dif- ference exists between the transducer and the medium adjacent thereto. Use of a matching layer provides for a stronger and sharper pulse and thus a better image. The optimized value range for the matching layer is from 3.8 to 4.2 (x 106kg/m2 sec). The material that is used for the matching layer may be PVDF (Kynar) at a thickness of 0.95 x (quarter wavelength thickness) . The matching layer 46 is bonded to the first conductive layer 45a by means of a thin glue layer. The matching layer 46 conforms approximately in surface dimension to the active size of the transducer, i.e. 0.5 x 1.0 mm.
Transducer Sensor Backing Layer:
Bonded to the conductive layer 45b on the opposite surface of the core 44 from the matching layer 46 is the backing layer 47. The backing layer serves to absorb acoustical energy generated off the non- imaging side of the transducer and also helps minimize energy reflections coming back to the transducer. The amount of energy traveling from the transducer core to the backing is a function of the acoustic impedance of the core and the backing material. The energy that is generated and enters the backing material should be attenuated sufficiently before it is reflected back into the core where it can distort the signal. The backing layer 47 impedance is selected to provide optimum damping so that the transducer sensor 42 vibrates for only a short duration after electrical excitation is stopped and prevents energy from being reflected to or from the artery wall to the back side of the transducer. This enables the transducer sensor 42 to be ready to receive pressure waves reflected from the arterial environment with no or minimal interfer¬ ence from ringing from the pulse. The impedance of the backing layer may be determined by computer modeling and in this embodiment is selected in the range from 5 to 7 (x 106kg/m2 sec). The composition used for the backing is preferably a tungsten and silicon rubber mixture. The acoustical impedance of the mixture can be varied by mixing various sized tungsten powder particles into the silicon rubber. This mixture is very good for backing since it has very high attenuation. The backing layer 47 may be bonded to the conductive surface 45b by means of a thin glue layer applied on backing type material. The backing layer 47 conforms in surface dimension to the size of the active area, i.e. approximately 0.5 x 1.0 mm. In order to allow sufficient ringdown after pulsing, the backing layer 47 is preferably provided with a maximum thickness, or depth dimension, consistent with the dimensions of the sensor housing 40, drive cable, elongate member, etc. As shown in Figure 3, in the present embodiment, the backing layer 47 may be made to a dimension equal to the cross-section of the drive cable 28 and/or housing 40. This allows for a backing layer of a maximum size to provide for sensor ringdown time and yet is small enough to fit deep into the coronary arterial environ¬ ment. The backing layer may be approximately 0.012 inches in thickness.
The transducer sensor 42 is connected by the sides 48 and 49 thereof to the interior of wall 50 of the housing 40. The transducer sensor 42 is mounted so that the central axis of the sensor assembly 24 passes through or is close to the plane defined by the flat surface of the transducer sensor 42. Thus, the flat surface of the transducer faces perpendicular to its axis of rotation. This permits maximizing the dimensions of the matching layer and backing layer. This construction also allows for secure mounting of the sensor assembly 24 to the drive cable 28 by inserting and connecting the housing 40 to the distal end of the drive cable 28.
The housing 40 has a first acoustic window (or aperture) 52 and a second window 53 oppositely located from each other in the cylindrical wall of the housing 40. These windows are preferably approximately rectangular in shape having parallel sides in the longitudinal direction of the housing 40 and rounded sides in the chordal direction. These windows may be formed by removing portions of the material of the cylindrical wall of the housing but leaving narrow bands 54 and 55 of the wall 50 of the housing 40 onto which the transducer sides 48 and 49 may be bonded. In a preferred embodiment, both windows 52 and 53 are approximately 0.6 x 2.0 mm. In the sensor assembly 24, the transducer sensor 42 is mounted and located in the housing 40 directly facing the first window 52 so that the ultrasonic signal is emitted from the transducer sensor 42 through the first window 52.
The size and geometry of the windows are related to the pulse generating characteristics and the advantages of the disclosed window geometry are de¬ scribed below in conjunction with the description of the operation of the pulser.
These windows 52 and 53 may also be useful during the construction and testing of the sensor assembly 24. The sensor assembly 24 can be constructed and tested before mounting to the drive cable 28 by connecting the wires between the tested sensor and the tested cable inside the window. This ability to screen sensor assemblies prior to attachment to the drive cable increases transducer drive shaft assembly yield dramatically. Also, the housing design also allows alignment of the transducer in the elongate member during rotation by the smooth rounded end and fit between elongate member 26 and the housing 40. Referring to Figure 4, the sensor assembly 24 is connected at its proximal end to the distal end of the drive cable 28. Specifically, the first conductive layer 45a of the transducer sensor 42 is connected to the distal end of an internal conductor 58 of the drive cable core wire 60. A distal end of an external layered coil portion 62 of the drive cable 28 is con¬ nected to the housing 40. These connections may be made by means of an epoxy adhesive. An external conductor 63 (also referred to as the reference plane conductor) of the core wire 60 is sealed by means of an epoxy. The reference plane conductor 63 of the core wire 60 is connected electrically to the housing 40 via the external layered coil portion 62 of the drive cable 28. In a preferred embodiment, a single trans¬ ducer is mounted in a single transducer housing which is connected at the distal end of a drive cable. However, in other embodiments, as described below, more than one transducer with one or more housings, may be connected serially at the end of a drive cable in order to make scans of a length of a vessel. In such multi- transducer embodiments, an appropriate switching device may be utilized in conjunction with the signal process¬ ing unit and the transducers to coordinate pulsing and receiving data.
III. DRIVE CABLE
Referring to Figure 5, there is depicted a portion of the drive cable 28, partially disassembled. In the assembled imaging system 20, the drive cable 28 is positioned inside the elongate member 26 and is con- nected to the sensor assembly 24, as described above. The drive cable 28 serves as both the mechanical and electrical link to the sensor assembly 24.
The drive cable 28 conducts the electrical signal from the proximally located signal processing unit 34 (via the proximal drive cable 32) to the sensor assembly 24 and conveys the sensed signal from the sensor assembly 24 back to the signal processing unit 34. In order to provide a drive cable of a suitably minimal dimension for coronary applications while providing both the necessary mechanical and electrical properties, the electrical components of the drive cable provide for mechanical motion transmittance as well. Thus, the drive cable 28 connects the sensor assembly 24 to the proximally located motor 36, via a drive shaft located in the proximal drive cable 32, in order to rotate the sensor assembly 24 to scan -the coronary vasculature with an ultrasonic signal.
In order to provide high quality electrical signal transmission, the drive cable 28 possesses a controlled matched impedance, a low signal loss, and high shielding and conductivity at high frequencies. As mentioned above, the need for a matched impedance in the drive cable 28 follows from the requirement for matching impedances at interfaces of the overall imag- ing system from the signal processing unit 34 to the sensor assembly 24 in order to eliminate reflections. Because of the relative difficulty in adjusting the impedance at the sensor assembly 24 end of the system, the rest of the system components, including the drive cable 28, are matched to that of the impedance of the transducer sensor 42. Accordingly, the impedance of the drive cable 28 is matched to that of the sensor assembly 24 and in this embodiment is established to be 50 ohms. Mechanically, the drive cable 28 possesses high torsional stiffness (i.e. minimal angular deflec¬ tion under operating torsional load) yet possess longi¬ tudinal (axial) flexibility to allow percutaneous posi¬ tioning in the coronary vessels. In addition, as mentioned above, the drive cable 28 also possesses dimensional properties suitable for positioning in a patient's coronary vasculature, specifically the drive cable 28 has a low profile diameter to navigate torturous coronary arteries. A present embodiment provides these features in part by a coaxial multi¬ layer drive cable construction. The drive cable 28 includes a core wire 60 located inside of an outer layered coil assembly 62, as explained below.
The core wire 60 is located at the center of the drive cable 28. The core wire 60 includes an insulated internal conductor 58. The core wire 60 has a diameter of 0.014 inch and its internal conductor 58 is 38 AWG (7 strands of 46 AWG) copper wire. The internal conductor 58 is surrounded by a teflon coating that forms an insulator layer 66. Teflon is used as an insulator for the internal conductor 58 of the core wire 60 because of the relatively low dielectric constant which allows for a smaller cable, less loss, and higher speed of electrical transmission for a given impedance. Around the insulated internal conductor 58 is an external conductor 63 in the form of a braided shield which forms the exterior electrical shield of the core wire 60. The braided shield is preferably composed of eight silver-plated, rectangular copper strands 70, four in each direction of rotation. Spe¬ cifically, each strand is 0.001 x 0.007 inch oxygen free highly conductive (OFHC) copper with 50 micro- inches of silver plating.
Use of flat wire of these dimensions for the construction of the braided shield allows excellent coverage of the core wire 60 while maintaining a low braid profile. This flat wire braid contributes only about 0.004 inch to the overall cross-section of the drive cable 28. Furthermore, the 7 mill cross- sectional area of each strand provides enough strength to form the braid with standard braiding equipment. The use of flat wire for the braided shield of the external conductive wire 63 also provides advantages for electrical transmission through the drive cable 28. A flat wire braided shield with its inherently large surface area produces a conductor of low resistance (i.e. low cable loss) when compared to dimensionally equivalent round wire braided shields. Because electrical current travels through a braided shield following a path of least resistance, the use of a rectangular braid for the shield provides a large surface area at overlapping wires allowing lower resistance contacts thereat.
Use of silver plating on the external conduc- tive wire 63 provides several further advantages.
First of all, the silver plating provides a high qual- ity environmental seal from corrosion. In addition, the silver plating on the flat copper wires of the braided shield of the external conductive wire 63 also advantageously reduces the shield's electrical resistance at the high electrical frequencies due to "skin effect". Electrical transmission through a con¬ ductor wire at high frequencies exhibits a "skin effect" which is a phenomena wherein the electrical current tends to increasingly travel in the outer periphery of a conductor as the signal frequency is increased. At the frequencies of operation of the imaging system, most of the current would be carried in the conductor within less than 0.0005 inch of the sur¬ face of the conductor. This is one of the reasons that the external conductor wire 63 is made with silver plating because silver has a lower resistivity than copper. For a given thickness more current will be carried in a silver layer than in the copper base.
A further reason for using silver plating is its property of non-corrosiveness which helps maintain low electrical resistance at the overlapping joints of the braided shield of the external conductor 63. The application of the silver plated, braided shield to the insulated internal wire thus forms a high quality miniature 50 ohm coaxial cable with a total diameter less than 0.030 inch (0.75 mm).
In the drive cable 28, around the core wire 60 is located the layered coil assembly 62. In a preferred embodiment, the layered coil assembly 62 comprises a multi-layer, multi-strand coil for optimum torque transmittance. The layered coil assembly 62 of the present embodiment is comprised of three layers 74, 76, and 78. Each coil layer is composed of three separate wires strands, e.g. coil layer 78 is comprised of strands 80, 82, and 84. Each strand may be com¬ prised of a 50 micro-inch silver plated, oxygen free highly conductive (OFHC) copper ribbon wire having dimensions of 0.001 x 0.007 inch. This construction of the layered coil assembly provides for suitable torque transmission (or stiffness) by reducing the torsional load per strand.
These three layers 74, 76, and 78 are applied in opposing winding directions to the layer immediately adjacent thereto. For example, coil layer 74 is wound in an opposite helical direction from that of coil layer 76, and coil layer 76 is wound in an opposite helical direction from that of coil layer 78 (but coil layer 78 would be wound in the same helical direction as coil layer 74) . The coil winding direction is determined so as to be consistent with the direction of drive cable rotation so that during operation of the system, the layered coil assembly will tend to tighten upon itself thereby providing additional torsional stiffening effects to the drive cable during operation without decreasing the cable's longitudinal flexibility during positioning. Increasing the torque stiffness reduces the angular deflection per coil layer.
Again, the use of flat wire for the layered coil assembly has several advantages. Using flat wire helps in maintaining the low profile of the drive cable, e.g only approximately 0.028 inch. This is significantly smaller than would be possible if a round wire of equivalent inertial moment were used. In addition, the use of multiple flat wire coils provides a significant amount of shaft flexibility due to the inherent slip planes between coils and strands which facilitates placement of the drive cable in the coronary arteries.
The utilization of silver plated OFHC copper for the layered coil assembly 62 advantageously bene- fits the drive cable's electrical properties as well. The use of the silver plated OFHC copper provides shielding effectiveness and lower resistance than other conductors (both DC resistance and high frequency resistance due to "skin effect" in conductors) . These properties reduce the electrical signal attenuation through the drive cable 28 and aid in producing the cable's matched impedance. These electrical character¬ istics improve the overall system performance by improving the signal to noise ratio and eliminating the need for impedance matching components.
Manufacturing Process for the drive cable
The drive cable 28 may be constructed accord¬ ing to the following procedure.
First, the core wire 60 is constructed. The braided shield for the reference plane conductor is constructed over a 0.014 inch diameter teflon insulated core wire using a Kokubun braiding machine. The Kokubun braider utilizes 16 bobbins containing braid wire moving in a inter-twining planetary action to create an interlaced braid. Bobbin movement, in terms of orbiting speed, and feed rate of the central core wire through the braiding area are controlled by two speed regulated motors, such as 2 1/4 H.P. Emerson Motors, P/N 3120-406. Motor speed of the core wire take up pulley and the bobbin rotation are closely regulated to predetermined values to ensure finished shaft's mechanical and electrical properties. This may be done with a Focus 1 Speed Controller.
The following process is followed to set up the Kokubun braiding machine. The teflon insulated internal wire 58 is routed through the center guide of the braider's bobbin carriage. Due to the fragility of the internal wire and the ribbon wire to be braided over it, an additional core wire guiding apparatus providing wire support, back tension, and braid wire entrance angle guiding is added to the Kokubun braiding machine. Also, the back tension provided at the bobbins for the braid flat wire has been reduced to approximately 35% of its original value. A modified upper guide has been added to control the small diameter braided wire's movement during the braiding process.
The Kokubun braider provides positions for 16 bobbins from which to create a 16 strand braid. Eight of these bobbins are removed to generate a coarser braid. The eight bobbins removed consist of 4 in each direction in an alternating fashion such that the remaining interleaved braid consists of four strands in each direction.
The braiding machine is started and bobbin carriage and braid take up wheel motor speed are adjusted. The bobbin carriage speed is set to 395 +/- 5 RPM. The braid take up wheel speed is set to 530 +/- 5 RPM. The braider configuration is modified such that the bobbin carriage motor has been fitted with a 5:1 gear reducer and similarly, the braid take up wheel motor utilizes a 30:1 gear reducer to provide the appropriate carriage and take up speeds.
The internal wire is routed through the braider's main guide and the upper broad guide and attached securely to the take up wheel.
Bobbins containing the 0.001 inch x 0.007 inch silver plated OFHC copper ribbon wire are threaded through the upper guide and attached to the braider's take up wheel, one strand at a time. Using the manual carriage crank, the bobbin carriage is rotated through 5 full rotations in order to initiate the braid on the internal wire.
After initiation of the braid onto the internal wire, the braid is bonded to the core wire using a cyanoacrylate adhesive over the entire existing braid length. The braiding machine is started by simultane¬ ously switching on both the carriage motor and the take up wheel motor. The motor speeds are verified with respect to their preset values. The braider is then allowed to operate for sufficient time to produce the required length of braided core cable based on the braider's approximate production of 0.33 feet/min.
Upon completion of the braided length, the braid is bonded using a cyanoacrylate adhesive over 0.5 inch bond length. The braid is cut at the bond area and removed from the braiding machine. The core wire portion is completed.
Next, the layered coil portion 63 is added to the core wire 60. A length of core wire of 66 inches is provided. The core wire 60 is prepared for the addition of the layered coil portion 62 by bonding the braided wire ends of the external conductor 63 using cyanoacrylate adhesive over a 0.5 inch length to prevent unravel of the braid. The application of layered coil portion 62 to the core wire 60 is performed using an Accuwinder Model CW-16A. The core wire is loaded in to the coil winder head and tail stock chucks. Three spools of 0.001 inch x 0.007 inch silver plated, OFHC copper ribbon wire are loaded on the coil winder's spool carriage. The wires are individually threaded through the coil winder's two guides and two tensioning clamps and finally through the three wire, lead angle guide. Wires must be routed under the three wire guide wheel and over the lead angle guide. The tensioning clamps are set to light tension. The spool carriage is moved into its initial coiling position; it is located such that the lead angle wire guide is approximately 0.25 inches (axially) from and head stock, and approximately 0.005 inches (radially) from the core wire. Guide adjustments are made by loosening their retaining screws. The first multistrand coil 74 is wound with the coil winder's rotation direction switch in the clockwise (CW) position. This coil winding rotation direction requires the three coil strands to be routed beneath the core wire and secured to the head stock spindle.
The coil winding computer controller is powered on in conjunction with the coil winder itself. Control by the computer over the coil winder is obtained by initiating the following winding parameters via the winding program ULTRA_SD: coil pitch=0.0232 inches, maximum winding speed=1780 RPM. The lead angle at which the wire approaches the core wire is con¬ trolled by way of the lead angle guide and the coil pitch. The winding control program is down loaded to the coil winder.
Axial tension is slowly added to the core wire until a value of.3 to .5 pounds-force is reached. The operating lever is lowered. Using the speed control knob, the coil winding speed is slowly increased to a maximum value of 60%. Core wire tension is continuously monitored during the coil winding process to maintain a wire tension of .3-.5 pounds- force. Coil winding is continued until the lead angle guide is within 1 inch, axially, of the tail stock chuck. The coiling process is halted by raising the operating lever and reducing the speed control to 0%. The coils are bonded to the core wire at the head and tail stock location over a 0.5 inch bond length. The three strands used to form the coil 74 are cut at the core wire 60 and care is taken to prevent damage to the core wire 60. The spool carriage is returned to the head stock location in preparation for applying the second, opposing, coil 76. The tail stock pulley is loosened such that it can move independently of the coil winder drive shaft. The tail stock spindle is rotated 5 full revolutions in the CCW direction (when viewing the front of the tail stock chuck) in order to preload the first coil. The tail stock pulley is tightened.
The three ribbon wires to be coiled are routed under the three wire guide, over the lead angle guide, and placed over the core wire; the wires are temporarily secured to the head stock spindle. The coil winder's rotation direction switch is moved to the Counter Clock Wise (CCW) position. The operating lever is lowered and the speed control is increased gradually to 60%. The core wire tension is maintained at .3-.5 pounds-force.
Coiling is continued until the lead angle guide is within 1 foot, axially, of the tail stock chuck. The coiling process is halted by raising the operating lever and reducing the speed control to 0%. The coils in this layer 76 are bonded to the core wire 60 at the head and tail stock locations over a 0.5 inch bond length. The three strands used to form the coil 76 are cut at the core wire 60 and care is taken to prevent damage to the core wire 60. The spool carriage is returned to the head stock location in preparation for applying the third coil 78.
The tail stock pulley is loosened such that it can move independently of the coil winder drive shaft. The tail stock spindle is rotated 5 full revolutions in the CW direction (when viewing the front of the tail stock chuck) in order to preload the second coil. The tail stock pulley is tightened.
Ribbon wires to be coiled are routed under the three wire guide, over the lead guide, and placed under the core wire; the wires are temporarily secured to the head stock spindle. The coil winder's rotation direction switch is moved to the Clock Wise (CW) position. The operating lever is lowered and the speed control is increased gradually to 60%. The core wire tension is maintained at .3-.5 pounds-force. Coiling is continued until the lead angle guide is within 1 foot, axially, of the tail stock chuck. The coiling process is halted by raising the operating lever and reducing the speed control to 0%. The coils are bonded to the core wire at the head and tail stock locations over a 0.5 inch bond length. The three strands used to form the coil 78 are cut at the core wire 60 and again care is taken to prevent damage to the core wire 60. The spool carriage is returned to the head stock location. Exiting the coil winding computer control program is accomplished by pressing the escape key (esc) at the computer keyboard, lowering the operating lever, and gradually raising the speed control above 0%. This sequence will create a user prompt to continue or exit to the main menu. A "M" is keyed to return the user to the main menu.
The completed drive cable 28 is removed from the coil winder. The remaining coil strands at the head stock are removed by trimming. Utilizing the above described method, a preferred embodiment of the drive cable 28 is provided having an impedance of 50 ohms, a low electrical signal loss of 10-12%, and high shield and signal conductivity at high frequencies in the range of 10 - 50 MHz (which includes the preferred operating frequency of 30 Mhz) . A cable constructed according to the above described method can possess a relatively low loss, from 0.9 to 1.4 Db loss over the required frequency range. In the preferred embodiment, the drive cable 28 has a diameter of 0.028 inch which is suitable for use inside a lumen of the elongate member 26 having an internal diameter of approximately 0.035 inches.
IV. THE SHEATH
As mentioned above, during operation of the intravascular imaging system 20, the drive cable 28 and sensor assembly 24 rotate at an angular speed while the transducer sensor 42 is excited and monitored. In order to accommodate this rotation in the human body, the drive cable 28 and sensor assembly 24 are located in the flexible elongate member 26. The elongate member 26 is composed of a non-rotating, bio-compatible sheath that not only encloses both the drive cable 28 and sensor assembly 24 but also serves to position the transducer sensor 42 at a desired location in the coronary vasculature. Referring to Figure 6, in the preferred embodiment, the elongate member 26 comprises a tubular sheath 80 having a distal portion 82 that can be positioned in a coronary artery and a proximal portion 84 that extends out of the body of the patient. The proximal portion 84 of the sheath 80 is fixed to a stationary (non-rotating) component, specifically to a catheter manifold 85 which in turn is connected to the housing of the uncoupling member 30 (as described below and as depicted in Figure 14) . As shown in Figures 1, 2, and 4, the sensor assembly 24 is located in a lumen of the elongate member 26 and specifically in a lumen 86 of the sheath 80 in a distal portion thereof.
In order to permit the transmission of the ultrasonic signal from the transducer sensor 42 which is inside of the sheath 80 into the body of the patient (and the reflections back again) , the sheath 80, or at least a distal portion thereof, is made of a material that is transparent to the ultrasonic signal. In the present embodiment, the sheath 80 or the distal portion thereof is made of a TPX material, specifically a methylpentene copolymer plastic. The TPX material has an acoustic impedance close to water, a low coefficient of friction, and good mechanical properties. Because the acoustic impedance of the TPX material is close to water, very minimal signal reflections are created at the sheath/blood interface. This characteristic allows the TPX material to appear transparent to the trans¬ ducer.
In a most preferred embodiment, the sheath 80 is formed of a polyurethane material. In order to make the sheath transparent to the passage of ultrasonic waves, the transducer sensor 43 is mounted in the housing 40 at a slight forward tilting angle, e.g. 10 degrees. This allows for the passage of the ultrasonic waves through the sheath 80 without reflections.
The sheath 80 is formed having a low profile suitable for positioning in the coronary vasculature. In a preferred embodiment, the sheath has 80 an external diameter of 0.040 inch. The TPX material lends itself easily to the extrusion process and can be readily drawn to very thin wall diameters. In this embodiment, the wall diameter of the sheath is 0.0025 and the diameter of inner lumen is 0.035.
In addition to providing a non-rotating interface to the body, the sheath 80 furnishes other features. Because the TPX material has a low coeffi¬ cient of friction, it provides a low frictional resistance bearing surface between the internal drive cable 28 and the wall of the lumen 86 of the sheath 80. In addition, the sheath 80 provides mechanical support to the drive cable 28 in order to develop good "pushability" for cable manipulation. The TPX material possesses good mechanical properties for an extruded copolymer. The mechanical strength of the TPX material coupled with the axial stiffness of the drive cable 28 generates a sufficient degree of "pushability", i.e. structural support in the sheath assembly, for positioning the sensor assembly 24 in coronary arteries.
Located in the lumen 86 of the sheath 80 near the distal end is an inner lumen seal 87. This inner lumen seal 87 serves to establish a barrier between the interior of the sheath 80 and the patient's blood vessel. This shields the blood vessel from the turbulence caused by the rotation of the drive cable 28 and sensor assembly 24. When the sensor assembly 24 is positioned in the sheath 80, the distal end of the sensor assembly 24 is approximately 0.050 inches from the inner lumen seal 87.
At a distal end of the sheath 80 is a guiding tip 88. The guiding tip 88 may be located in the lumen 86 of the sheath 80 distally from the inner lumen seal 87. The guiding tip 88 may be comprised of a radiopaque material, such as a coil of thin platinum wire. Platinum, with its inherent radiopacity, wound in a coil configuration produces a soft, flexible, radio-opaque, crush resistant tip. Mounting the coil inside the lumen 86 of the sheath 80 permits retaining the smooth outer surface of the sheath 80 thereby facilitating maneuvering the sheath 80 through a guiding catheter and eventually into a coronary artery. As mentioned above, at a proximal end of the sheath 80 is located the catheter manifold 85. The catheter manifold 85 has a first or main port 89 gener¬ ally aligned and communicating with the lumen 86 of the sheath 80 and a second port 90 also communicating with the lumen 86 of the sheath 80. A strain relief coil 91 is located around the outside of the proximal end of the sheath 80 and extends into and is bonded between the sheath 80 and the catheter manifold 85. The catheter manifold 85 is utilized to connect the sheath 80 to the uncoupling member 30, as described below. The drive cable 28 is installed into the sheath 80 via the main port 89. The second port 90 may be used for flushing of the sheath 80, as described below.
The sheath 80 may also provide for a means of rotational compensation in order to continuously calibrate the transducer's angular orientation during operation. One of the drawbacks associated with rotat¬ ing ultrasonic imaging devices is angular distortion between the encoders at the proximal end and the sensor at the distal tip of the catheter. There are two main types of the distortions, those changing in time and those fixed to the phase of revolution. The fixed distortion is caused by friction or stiffness that causes a repeatable torque variation with each cycle. This can be found in almost every rotating element to some degree. The distortion that changes in time causes the image to rotate periodically. The major source of this is the heart moving, which flexes the elongate member causing a frictional torque variation synchronous with the heart beat.
The present embodiment provides a solution to this problem by means of an acoustical indexer. An acoustical indexer is a locational marking that is put on, or built into the sheath to provide a rotational registration. This registration is constructed in the manner so that it can be readily identified in the signal processing.
Referring to Figures 7a and 7b, rotational compensation markers 92 can be incorporated circumfer- entially in the wall of sheath 80 in a distal portion thereof. The markers 92 may be splines or patterns incorporated on the interior surface of the sheath 80, as depicted in Figure 7a, or on the exterior surface of the sheath, as depicted in Figure 7b. Preferably, the markers 92 are located at periodic positions 45 degree from each other around the circumference of the sheath wall. The markers 92 can be made from a variable thickness in the sheath material, but could be made from two different materials. These markers 92 may be formed in the extruding process for the sheath and may be made just in the region of the sensor or may extend over the entire length of the sheath. Each wall thickness change may be recognized by the signal processing unit 34 and can be used to verify the transducer's angular position during operation. The thickness steps could be made at various ramp rates. With a pattern in the sheath wall, the signal process¬ ing unit can follow the image variation in distance. By following and holding steady one edge or feature, the time variable distortion is corrected. This com- pensation ability removes any discrepancy in a image due to an angular speed change of the transducer. By using a pattern of acoustic indexing markers as shown in Figures 7a or 7b where the thick¬ ness is varied every 45 degrees, fixed distortions can be corrected. Periodically, the data of the image representing the sheath would be analyzed to determine the correct time spacing of the triggers. This data is transferred to the pulser that has a variable time spaced pulse capability. By using a 1000 pulse per revolution encoder connected to the motor that provides the synchronizing of the motor to the pulser, there is more than enough resolution to generate the required pattern. The screen is divided up into 200 pie shaped angular divisions, each of these divisions is called a vector. For a 200 vector screen, the pulser needs to generate 200 pulses per revolution by dividing up the 1000 pulses into the required spacings.
A block diagram of the indexing data -process¬ ing is shown in Figures 8a and 8b. A real time con- figuration tracks an edge in real time and adjusts the pulse pattern very quickly, as represented in«fig- ure 8a. The data is intercepted from the raw data pipeline, processed and transferred to the pulser com¬ puter. The EKG signal would be useful for calibrating the image to the heartbeat and removing the time-motion effect. A non-real time configuration could be used almost as effectively, as represented in Figure 8b. Here the data is processed and transferred periodically as needed. The data is captured and processed by the main processor and the result sent to a pulser computer that would pulse the excitation at the proper times. A variation of this method but yielding basically the same result would apply a pulse to the sensor every increment of a motor encoder and determine the position of each vector in the pipeline processing.
Manufacturing of the Elongate Member
A sheath 80, as described above, may be made by irst bonding a tubular portion into the catheter manifold 85 using an epoxy or other suitable adhesive. The sheath 80 should extend to a distal side of the entrance of the flush ports into the manifold 85. Care should be taken to ensure that adhesive does not flow into the lumen 86 of the sheath. Then the strain relief coil 91 may be installed into the manifold hub. The hub is then filled with adhesive. This assembly is then allowed to cure.
Using an adhesive applicator syringe with a 0.025 inch maximum diameter tip, the adhesive lumen seal 87 is installed in the distal end of the sheath 80. The seal 87 is preferably located 0.5 inch from distal tip of sheath 80. The seal 87 should be 0.100 inch in total length. Next, the distal marker coil is installed. Using a syringe, adhesive is applied to 0.05 inch of the distal end of the marker prior to installation. The distal marker is installed in the distal end of sheath 80. The marker coil is allowed to interfere with the sheath's seal 87 by 0.05 inch. Then the assembly is allowed to cure at 140°F for 4 hours.
flushing methods The sheath 80 includes a means for flushing the sensor assembly 24 and sheath lumen 86. Any pres¬ ence of entrapped gas or contaminants in around the sensor assembly 24 reduces the performance of the imag¬ ing system. Any gas or contaminants on the surface of the transducer sensor 42 may generate severe reflec- tions and essentially blind the transducer in that region. The flushing process assures that all gas and contaminants are removed.
Flushing of the sensor assembly 24 and the sheath 80 may be provided by three alternative systems: Referring to Figure 9, a first embodiment of the flushing system utilizes a flushing lumen 93 which may be a flexible tubular member having a diameter less than the diameter of the lumen 86 of the sheath 80. The flushing lumen 93 may be fed through the catheter manifold's second port 90 proximal to the distal seal 87 of the lumen 86. The flushing lumen 93 is then pressurized with a flushing medium. The flushing lumen 93 is slowly withdrawn from the sheath 80 while press¬ ure is maintained on the flushing medium. The process is continued until the flushing medium flows from the proximal end of the manifold's main port 89 and the flushing lumen is removed.
Referring to Figure 10 and 11, a second embodiment of the flushing system is depicted. The second flushing embodiment uses a sheath 94 having dual lumens, a main lumen 95 and an outer lumen 96. The outer lumen 96 provides a flushing channel to the distal end of the sheath 94 where it communicates with the distal end of the main lumen 94 through a opening 97 between the lumens 95 and 96. A flushing medium. typically water, is continuously fed under pressure through a proximal catheter manifold's flush port 98 through the flushing lumen 96 from the proximal end to the distal end, through the opening 97 into the main lumen 95, and back through the main lumen 95 from the distal end to the proximal end until the medium flows from the manifold's main port.
Referring to Figure 12, a third embodiment of the flushing system is depicted. This embodiment in- eludes a sheath 99 having an air permeable seal 100 in the sheath's distal tip to allow entrapped gases to diffuse out during flushing pressurization. The seal 100 has a permeability which allows the air mass in the sheath lumen to be dissipated through the distal tip area in a reasonably short amount of time. In a com¬ plimentary fashion, the seal's porosity is low enough to restrict water mass transfer, i.e. the surface tension of the water coupled to the porosity of the seal prohibits mass transfer. The seal may be made with materials with permeabilities in the range of: 2 to 2,000,000 ng/(s-m-Pa) . This permeability range covers both flushing pressure variations of 6.895 kPa to 689.5 kPa and flushing times of 1 second to 1200 seconds. In the preferred embodiment, permeability for sheath flushing in 20 seconds at a 202.7 kPa flushing pressure through a 2.54 mm long seal is 1290.1 ng/(s-m- Pa).
IV. COUPLING AND UNCOUPLING
Referring to Figure 13, the elongate - em- ber 26 (with the distal drive cable inside thereof) is connected at its proximal end to the coupling member 30 by means of the manifold 85. The coupling (and un¬ coupling) member 30 connects the distal drive cable 28 to the proximal drive cable 32 which in turn connects to the proximally located components, i.e. the signal processing unit 34 and the motor 36. By means of the coupling member 30, the imaging system 20 provides a means of coupling and uncoupling the distal transducer side of the system from the proximal components at a point outside the body of the patient.
This coupling member 30 provides several advantages for the imaging system 20. Providing for coupling and uncoupling of the distal sensor facili¬ tates loading and handling of the drive cable 28 and the sensor assembly 24 into the elongate member 26.
Also, by providing a means for coupling and uncoupling, the imaging system 20 can utilize larger size, less expensive components for electrical and mechanical transmission proximally from the coupling location where the dimensions of the components are not limited by the constraints of positioning in the coronary vasculature. Thus, critical electrical information can be transferred from the rotating drive cable 28 to a less expensive, commercially available, stationary, 50 ohm coaxial cable while maintaining a mechanical link between the motor 36 and the sensor assembly 24. As required for the rest of components used for electrical transmission, transfer of electrical information by the coupling member 30 is preferably maintained in a controlled impedance environment matched to the transducer.
At the coupling location, the transmission of mechanical torque can also be transferred proximally to larger, commercially available components that are less expensive to manufacture. Further, at the point of coupling between the proximal drive cable 32 and the distal drive cable 28, a mechanical 'fuse' may be pro¬ vided to prevent torsional overload to the drive cable in the body. In the coupling member 30, the electrical and mechanical functions which are united in the same com- ponents in the distal drive cable 28, are split into separate, adjacent cables one for the mechanical trans¬ mission and another for the electrical transmission inside the proximal drive cable 32. Thus, in the un- coupling member 30, the electrical signal transmission, which in the distal drive cable 28 is conducted by the core wire that is rotating at operating speed, is transferred to a non-rotating coaxial cable connected to the proximal signal processing unit 34. The coupling member 30 may be located approximately 60 inches proximal of the sensor assem¬ bly 24 so that it is outside of the patient's body. The coupling member 30 is comprised of a sleeve 101 inside of which is contained a matable coaxial con- nector pair. The coupling member 30 in this embodiment of the imaging system is provided by two assemblies that are mechanically coupled together: a transducer pin assembly 102 that connects to the components on the distal side of the system, such as the sensor assembly 24 and the elongate member 26, and a slip ring assembly 104 that connects to the components on the proximal end of the system, such as the signal processing unit 34 and the motor 36.
The coupling member sleeve 101 is formed by a first or distal sleeve portion 106 that is part of the transducer pin assembly 102 and a second or proximal sleeve portion 108 that is part of the slip ring assem¬ bly 104. These sleeve portions 106 and 108 may be made of a metal, such as aluminum. The sleeve portions 106 and 108 are held together through the use of a coupling nut 110. Accordingly, the coupling nut 110 provides the means for securing the distally located transducer pin assembly 102 to the proximally located slip ring assembly 104 and their respective coaxial connector halves located therewithin together, as described below, during system operation. This nut 110 may be removed or tightened to disconnect or connect the distal components from the proximally located com¬ ponents.
Referring to Figures 14 and 15, the coupling nut 110 slidably fits over the sleeve portion 106 and abuts against a shoulder 112 on the proximal end of the sleeve portion 106. The coupling nut 110 has threads 114 internal thereto oriented in a proximal direction to engage corresponding external threads 115 on the exterior of the slip ring sleeve portion 108, as shown in Figure 15.
In each of the sleeve portions 106 and 108, there is provided one half of the matable coaxial con¬ nector pair. As shown in Figures 14 and 15, a male component 116 of the matable coaxial connector pair is located in the transducer pin assembly 102 and a female component 117 of the matable coaxial connector pair is located in the slip ring assembly 104. This coaxial connector mated pair 116 and 117 provides for both the electrical and mechanical separation point between the transducer pin assembly 102 and slip ring assembly 104. Mechanical coupling between the mated connector halves is controlled by the spring force exerted by interfer¬ ence between the male coaxial connector shield spring contacts 118 and the female coaxial connector shell
119. This spring force generated between the male and female components of the matable coaxial pain allows for torque to be transmitted across the coupling mem¬ ber 30. This matable coaxial pair may be a commerci- ally available coaxial connector pair, such as made by Amphenol Corp., modified to be connected in the coupling member 30.
This internal coaxial connection is made with a controlled impedance matched to the drive cable 28 and the transducer sensor 42, i.e. with an impedance of 50 ohms. Matching the impedance in the coupling member 30 with these components avoids mismatch signal reflec¬ tions, as described above.
Referring to Figure 14, the transducer pin assembly 102 is connected to the proximal end of the drive cable 28 so as to allow rotation of the drive cable 28 inside the transducer pin assembly 102. Located at and covering the distal end of the sleeve portion 106 of the transducer pin assembly 102 is a sleeve cap 120 having a passage 121 therethrough. The sleeve cap 120 is secured to the sleeve portion 106 by stamping or a compression fit or other means. The sleeve cap 120 includes a nipple portion 122 which extends distally and in which is located the distal portion of the passage 121. The nipple portion 122 is connected to or may be formed of the sleeve cap 120. Threads 128 located on the exterior of the nipple 122 engage internal threads located in the proximal end of the manifold 85. A compression 0-ring 129 may be provided between the distal end of the nipple 122 and the manifold 85 to ensure a secure fit.
Located inside and connected to the sleeve 106 proximally from the end cap 120 is a coaxial connector bearing 130 and a bearing retaining ring 131. The bearing 130 and end cap 120 define an interior portion 132 of the transducer pin assembly 102. The bearing 130 may be made of bronze and oil-impregnated to provide for free rotation inside the pin assembly's outer shell. A drive cable clamp 134 is secured to the drive cable 28 so as to be located in the interior portion 132 of the transducer pin assembly 102. The clamp 134 may be secured to the drive cable 28 by an adhesive or other means. A strain relief sleeve 136 may be connected to or formed on the distal surface of the clamp 134 and extend distally on the drive cable 28 to a location through the nipple 122 (e.g. 0.75 inches) . The strain relief sleeve 136 may be made of teflon.
Located around the clamp 134 is a shell 138. The shell 138 is comprised of a first shell half 139 and a second shell half 140 that can be secured together such as by means of threads. When the shell halves 139 and 140 are secured together, they also secure by compression the clamp 134 between them. The shell 138 include a distal opening 141 and a proximal opening 142, both aligned with the passage 121 so as to receive the drive cable 28. The opening 141 may also receive a portion of the strain relief sleeve 136. A bushing 143 may be located in the proximal opening 142. The bushing 143 may be made of teflon. Connected to the distal side of the shell 138 is the male portion 116 of the coaxial connector pair.
The drive cable 28 is thus rotatably secured within the transducer pin assembly 102. The drive cable 28, the clamp 134, the strain relief sleeve 136, the shell halves 139 and 140, the bushing 143 and the male coaxial connector 116 are rotatable.
Referring to Figure 15, there is depicted the slip ring assembly 104 which forms the proximal half of the coupling member 30. In the slip ring assembly 104, the electrical signal is transferred from rotatable distal components to non-rotatable proximal components, i.e. the electrical signal transmission which is carried by rotating components distally is transferred to non-rotating components proximally. In addition, in the slip ring assembly 104, the electrical signal, which is carried by the same components that transmit the mechanical torque distally, is carried proximally by components separate from those that transmit the mechanical torque. As described above, the slip ring assembly
104 includes the sleeve portion 108 the proximal end of which connects by means of the threads 115 and the coupling nut 110 to the transducer pin sleeve portion 106 to form the non-rotating coupling member sleeve 101. A slip ring end cap 158 connects to and covers the proximal end of the slip ring sleeve 108. The slip ring end cap 158 includes a first opening 160 aligned centrally therein and a second opening 162 offset from the first opening 160. Located in and extending through the first opening 160 is a slip ring drive shaft 164. A proximal bushing 166 is positioned in the first opening 160 around the slip ring drive shaft 164. An outer slip ring 167 and an inner slip ring 168 are connected to the distal end of the slip ring drive shaft 164. The outer and inner slip rings 167 and 168 are connected distally to a modified coaxial connector
170 which forms the proximal portion of female portion 117 of the mated connector pair. A proximal bushing
171 is mounted in the proximal end of the sleeve portion 108 around the female portion 117 of the mated coaxial pair.
Through the second opening 162 in the slip ring end cap 158 extend leads 172 and 174 from the proximal drive cable 32. Specifically, the lead 172 connects to the signal conductor and the lead 174 connects to the reference plane conductor of a coaxial cable in the proximal drive cable 32, as explained below. The distal end of the lead 172 connects to an inner brush ring 176 and the distal end of the lead 174 connects to an outer brush ring 178. The inner and outer brush rings 176 and 178 may be made of brass and may be approximately 0.063 inch wide. An inner spring 180 is located between the inner brush ring 176 and the end cap 158 and an outer spring 182 is located between the outer brush ring 178 and the end cap 158. The inner and outer springs 180 and 182 bias the inner and outer brush rings 176 and 178, respectively, in a distal direction away from the end cap 158.
The inner brush ring 176 bears against a set of inner brushes 184 and the outer brush ring 178 bears against a set of outer brushes 186. These two sets of brushes 184 and 186 are mounted coaxially to each other. In a preferred embodiment, each set of brushes 184 and 186 includes three brushes, (only two brushes of each set are shown in Figure 15) . Each brush is located at 120 degree intervals to the other two brushes in its respective set.
The inner set of brushes 184 and the outer set of brushes 186 are slidably held by a brush guide 188. The brush guide 188 is mounted into the inside of the slip ring sleeve 108. The brush guide 188 is a cylindrical plug having two sets of three slots each located at 120 degrees from each other (i.e. for a total of six slots) therethrough for retaining the two sets 184 and 186 of three brushes each. The brush guide 188 also includes a large central opening 189 through which passes the slip ring drive shaft 164.
Biased by the inner spring 180, the set of inner brushes 184 bears against and rides on the inner ring 168. The inner ring 168 is used to conduct the signal and is attached to the internal conductor of the coaxial connector 117. Biased by the outer spring 182, the set of outer brushes 186 bears against and rides on the outer ring 167. The outer ring 167 is used for connection to the reference plane signal and is attached to the reference plane conductor in the coaxial connector 117 and/or the sleeve 108.
The brushes provide the path for transferring the electrical signal information between the station¬ ary inner and outer brush rings 176 and 178 and the rotating inner and outer slip rings 168 and 167. In a preferred embodiment, the brushes are made of silver graphite. Silver graphite provides for a brush ma¬ terial that is highly conductive and self-lubricating. Relatively large brass slip rings are util¬ ized to increase the conductive contact area available between both the slip rings and coaxial connector 117, and the slip ring and brushes. The use of large contact areas reduces electrical resistance and signal loss through the slip ring assembly 104.
In the slip ring assembly 104, only the coaxial connector 117, the slip ring drive shaft 164, and the slip rings 167 and 168 rotate during operation. The sets of brushes 184 and 186, brush rings 176 and 178, brush guide 188 and sleeve 108 all remain stationary during operation.
Mechanical coupling
In addition to providing for electrical transmission, the slip ring assembly 104 also furnishes the mechanical torque transmission across the coupling member 30. The springs 180 and 182 in the slip ring assembly 104 develop the friction force which supports the torsional load created by the transducer drive cable 28. Mechanical coupling between the mated con¬ nector halves 104 and 106 is provided by the spring force generated by the interference between the male coaxial connector shield contacts 116 and the female coaxial connector shell 117. This spring force creates a friction fit between the mated connector pair 116 and 117 and allows torque to be transmitted across the coupling member 30. In the preferred embodiment, the torque transmittance in the slip ring assembly 104 is tuned by adjusting the spring force to provide a maximum torque of 3 inch-ounces before relative slip¬ page between connector halves 116 and 117 occurs. This provides for a mechanical 'fuse' feature in the system that ensures torque transmittance to the drive shaft assembly and not the pin assembly shell.
The coupling member 30, comprised of the transducer pin assembly 102 and the slip ring assembly 104, is easy to use and eliminates or reduces obstruc¬ tions in the area of the patient. This facilitates the placement and manipulation of the elongate member 26 and sensor assembly 24 in the coronary vasculature of the patient without the burden of having bulky com- ponents in close proximity to the patient. The assem¬ bled coupling member 30 has a cylindrical shape of approximately 0.75 inch in diameter and approximately 4 inches in length. (The transducer pin assembly 102 is approximately 0.75 inch in diameter and 1.75 inch in length.)
The fact that the slip ring assembly 104 uses controlled impedance components for electrical trans¬ mission except for a portion of a length less than 0.5 inches. This feature provides for the reduction of signal reflections from impedance mismatches.
V. THE PROXIMAL DRIVE CABLE
The distal end of the proximal drive cable 32 connects to the proximal end of the slip ring sleeve portion 108, as shown in Figure 15. The distal end of the proximal drive cable 32 includes a proximal cable sheath 190 that connects to the slip ring assembly sleeve portion 108. The proximal cable sheath 190 may be formed of a section of heat shrink tubing. Provided in the interior of the cable sheath 190 are the drive shaft 192 that connects proximally to the motor 36 and the proximal coaxial cable 194 that connects proximally to the signal processing unit 34. The drive shaft 192 and the proximal coaxial cable 194 are adjacent to each other with the drive shaft 192 aligned approximately along a central axis of the sheath 190 and the coaxial cable 194 offset therefrom. Proximally from the cable sheath 190, the drive shaft 192 and the proximal coaxial cable 194 are enclosed in a proximal cable covering 195. The drive shaft 192 connects to the slip ring drive shaft 164 inside the sheath 190. This connection is made by means of a shaft coupler 196 which may be a tubular member made of DELRIN®. As described above, the slip ring drive shaft 164 extends distally from its connection to the drive shaft 192 into the slip ring assembly 104 through the opening 160 in the slip ring assembly end cap 158. The drive shaft 192 is prefer¬ ably longitudinally flexible yet torsionally rigid so that it can rotate through operation of the motor and transmit this rotation to the slip ring assembly on to the drive cable and transducer assembly 24. The drive shaft 192 may be a flexible cable made of high tensile strength steel or stainless steel. A commercially available flexible drive shaft may be used, such as S. S. White Industrial Products, Inc. shaft # 098-9.
Also inside the proximal cable sheath 190 is the distal end of the proximal coaxial cable 194. The distal end of the reference plane conductor 198 of the proximal coaxial cable 194 connects to the proximal end of the reference plane lead 174 and the distal end of the signal conductor 200 of the proximal coaxial cable 194 connects to the proximal end of the signal lead 172. The coaxial cable 194 is preferably flexible and is stationary, i.e. it does not rotate with the drive shaft 192. A matching capacitor 202 may be connected between the signal and reference plane conductors 200 and 198 of the coaxial cable 194 for impedance matching purposes. (The matching capacitor 202 would normally have a heat shrunk cover, which is not shown in Fig- ure 15) . The proximal coaxial cable 194 may be a commercially available 50 ohm coaxial cable, such as RG 178 B/N, available from Belden Corporation.
Referring to Figure 16, in the proximal cable 32, the drive shaft 192 and the proximal coaxial cable 194 extend proximally from the proximal cable sheath 190 adjacent to each other inside the proximal cable cover 195. The proximal coaxial cable 194 may be enclosed in an isolation shield 206 that may be made of tin plated copper braid. The drive shaft 192 in enclosed in a non-rotating metallic sleeve 208. At a branching member 210, the coaxial cable 194 and the drive shaft 192 separate. The branching member 210 may be made of a heat shrink tubing. From the branching member 210, the coaxial cable 194 extends proximally inside a coaxial cable jacket 212 to coaxial connector 214 that can be fitted to the signal processing unit 34. From the branching member 210, the drive shaft 192 extends proximally inside a drive shaft jacket 216 to a coupling connector 218 to provide for connection to the motor 36. The motor may be a 40 watt DC rare earth motor, such as manufactured by Maxon Motor Co., Model No. RE035-071-39EAB200A.
V. THE PULSER AND SIGNAL PROCESSING OPERATION
The signal processing unit 34 includes a pulser which generates the high energy pulses that are converted by the sensor into an acoustical wave that is used for imaging. A full single cycle pulser is used since it gives twice the energy as a half cycle pulser for the same peak voltage and further it gives better settling. For isolation between the high voltage circuitry and the elongate member, a transformer is used. High frequency transformers are easier to design for cyclic waveforms with no DC frequency component, if fast settling is important. A full single cycle pulse of the sensor generates a return signal with almost no increase in ringdown time as compared to an impulse. Any increase in the number of cycles beyond one increases the ringdown time almost directly propor¬ tionally. For a good image, signal quality is very important. This means high amplitude with ringdown quickly to a -40dB level. A pulser technique is utilized that provides for a sharper pulse and better ringdown of the signal. Prior pulsers implement a pulse shape of an integer number of half cycles at a given frequency. A pulser that is capable of gener¬ ating a pseudo-random pulse would be able to excite the transducer and settle the reflections out by the sequence of pulses at certain amplitudes and at the right time.
As mentioned above, the size and shape of the sensor window is directly related to the quality of the ultrasonic image obtained. Ultrasonic imaging in two dimensions, (i.e. of a cross section of the arterial wall) is acoustically a three-dimensional problem.
Referring again to Figures 2 - 4, the objective for a good imaging system is to have a thin sharp rotating beam over the distance of interest, e.g., in a direction, y, radial to the artery wall. However, the beam, of course, propagates in all directions. The performance of the beam in the two lateral directions from the radial direction is termed the acoustical optics of the sensor. In the two lateral directions } and x2 (i.e. the directions perpendicular to the radial direction) , the beam shape is a function of the distance from the sensor, sensor focus, physical shape and the operating frequency. For an imaging device that makes circular scans of the arterial walls, the resolution in the radial direction is limited by the number of cycles of propagation of the pulse waveform. This time or distance is determined typically by the - 40 dB amplitude points of the waveform, as illustrated in Figure 17.
Using a rectangular transducer sensor is one of the keys to making a very small intravascular ultra- sound device for use deep in the coronaries. There are some tradeoffs with respect to circular apertures, but at the very small sizes the best performance is obtained from a rectangular aperture.
The beam shape is a function of the housing aperture size in the respective direction. This function is
Z = A2/L where Z is the near field distance, A is the aperture size, and L is the wavelength. For the above 0.5 x 1.0 mm window with a 0.056 mm wavelength (as defined by the frequency and media speed of sound) , the near field is 1.1 mm in the x directions and 4.5 mm in the y direction. The significance of the near field is that, for an unfocused sensor, the beam width is nearly the aperture width through the length of the near field. In the near field the beam is rapidly changing in all directions. This is from the constructive and destruc¬ tive interference patterns. In the far field the beam is more uniform and diverges. The far field behaves as though the source was a point source. For focused crystals the beam can be focused up to the limit of the near field. A focused beam is narrower in the focused region but diverges faster than unfocused outside this region. For intravascular ultrasound in the coronary region, it is sought to obtain images out to about 5 mm in radius. For a window having dimensions such as described, an advantage of the rectangular shape is that even though the energy is spreading in the x directions, the energy in the y direction remains relatively constant through the distance of the region of interest, as illustrated in Figures 18 - 21. In the x directions, or lateral directions as used in this specification, the beam size is quite usable to gener¬ ate good intravascular images throughout the radius of interest. For a circular aperture of this size, the intensity would decrease very rapidly since the beam is spreading uniformly in all directions. The rectangular aperture has better distance vs. energy dropoff along with a larger surface area. For apertures 0.5 mm and smaller the rectangular shape has some characteristics that are more desirable for apertures than circular shapes.
Calibrated Waveform Pulser:
As mentioned above, for radial resolution the ringdown of the signal is very important and it would be desirable to have a single cycle response to a impulse excitation. Typically, the excitation that is used is either a half cycle type impulse excitation or a integer number of sine wave cycles. There are significant advantages to using an excitation that uses a main pulse rather than a modified pulse waveform to cause a faster -40 Db ring¬ down time. There are two major reasons for this. From computer modeling of the transducer, the resultant objective of the iterative optimization program is to generate a system transfer function that has a smooth phase and magnitude over the widest frequency range. This is achieved by optimizing the value of peak pulse amplitude squared divided by the integral of time weighted magnitude after the peak. By using a non- impulse excitation, the Fourier transform of the excitation is different so that the frequency spectrum of the excitation is different than an impulse. The ideal impulse has constant magnitude frequency com- ponents. By allowing the computer to vary the waveform from one discrete time increment to the next, an optimum excitation waveform can be generated.
There are limitations of the computer model, such as non-infinite backing distance, surface irregularities, mechanical tolerances, impedance mis¬ matches, etc These variables result in the perfor¬ mance of the actual device to depart from what the model predicts. By using basically the same technique to calibrate a device, certain reflections and imper- fections can be countered by using an optimized excita¬ tion.
This circuit could be implemented using a high speed Digital to Analog (D/A) converter, where the output could be programmed by a computer to a predeter- mined wave form, (see Figure 22) . This output could be amplified to any required level that is required. The optimized waveform is generated over a few hundred nanoseconds and is settled out before the image data is received.
VI. ADDITIONAL PREFERRED EMBODIMENTS A. Sensor Constructions:
Referring to Figure 23, there is depicted an alternative embodiment for the construction of the transducer sensor. In constructing a sensor, it is desirable to have a configuration that gives a uniform beam from one device to the next and is easy to produce. A uniform beam is necessary for both good repeatability of system performance as well as for implementing other, more advanced data conditioning algorithms necessary for image enhancement.
Referring to Figure 23, there is depicted an alternative embodiment of the transducer sensor. As in the embodiment described above and illustrated in Figures 2-4, the transducer sensor in Figure 23 is com- prised of a several separate layers including a trans- ducer core, conductive layers bonded to either side thereof, a backing layer and a matching layer. In the embodiment shown in Figure 23, a matching layer 301 (which may be composed of a PVDF material) is larger in dimension than sensor core 44 and includes a overhang 303 on a proximal end. This overhang 303 allows electrical contact between the conductive surface 45a over the sensor core 44 and the center conductor of the coaxial drive cable (not shown) . This provides for both a superior transducer surface with a very uniform active area. This embodiment also significantly facilitates manufacturing. These features can be fur¬ ther enhanced through the use of a conductive backing 305. The conductive backing 305 provides an electrical contact between the sensor back surface and the sensor holder. The sensor holder is electrically connected to the drive cable outer conductor (not shown) . The con¬ ductive backing can be composed of a number of differ¬ ent materials, such as silver, tungsten, copper, gold or a number of other elements or alloys. The matching layer 301 can be made from PVDF, or other materials.
Other alternative embodiments include using a PVDF type material having a conductive layer on both the front and back face of the sensor to carry the signals to their connection. Behind the layer on the back side of the sensor an attenuating layer may be needed to absorb the energy coming off in that direction. The two connections would be terminated at the drive cable coaxial electrical connections. A further alternative is to extend the conductive faced matching layer and the conductive faced backing layer from the sensor core to the proximal portion of the drive cable by integrating the flexible circuits into the construction of the drive cable. In order to electrically insulate the two conductive surfaces, an insulation layer is incorporated between the«__yers. This would require no joints in the electrical sensor construction within the catheter.
B. Imaging Guide Wire
An alternative embodiment of the present invention may combine the functions of a guide wire with those of an ultrasonic imager. A guide wire function is to navigate to a location of interest in a patient's vasculature and to position a catheter over the guide wire into place for a procedure, such as balloon angioplasty. Because it would be desirable to have a device that would image the artery before, during and after such procedures, it would be advant¬ ageous to combine the functions of the guide wire and the imaging device. Most catheters are of a coaxial design so that once the catheter is in place the guide wire could be withdrawn and an imaging guide wire put in its place.
Currently guide wires are used in dimensions of 0.018 inch or smaller. In the embodiment described above, the drive cable 28 has a diameter of 0.026 inches and accommodates a transducer sensor having an active area of approximately 0.020 x 0.040 inch. In order to combine the functions of the drive cable with those of a guide wire, the dimensions of the drive cable would be reduced in size to approximately 0.018 inch in diameter. The transducer sensor would be made with a housing aperture close to 0.017 inch. At that size the image resolution would be substantially the same as in the embodiment described above. With image enhancement techniques described elsewhere in this specification, it would be possible to have an image as good as or better than those currently achieved. A thinner transducer having a higher frequency or a different material could be used for the sensor. A distal end of an imaging guide wire 350 is illustrated in Figure 24. A drive cable 352 can be constructed substantially as described above, except that for reducing the size from 0.026 inch to 0.018 inch, two coils and a double braid would be used instead of three coils and an eight wire braid. This has the result of reducing the outer coils and con¬ ductors to 0.008 inch leaving 0.010 inch for a center conductor and insulation. In one aspect, the construction of the imaging guide wire would likely depart from that of the embodiment described above and that is in the mounting of the transducer sensor to the drive cable. In the imaging guide wire, the width of the active area of the sensor would be nearly equal to the diameter of the drive cable. In all other respects, the construction of the transducer sensor portion of the imaging guide wire would be very similar to that of the embodiment described above. This drive cable 352 has a sensor holder 354 mounted at the distal end thereof. Unlike the sensor housing described above having oppositely located windows, the sensor mount 354 of this embodi¬ ment would not include a second window located oppositely from the transducer opening. Instead, the mount 354 would provide physical support under the transducer sensor 356. Also, due to size constraints, there would be little room for backing material on the back side of the transducer sensor. This could be com¬ pensated for by several different methods. For example, the sensor could be made from a copolymer material which has a low acoustic impedance so that no matching layer would be needed to couple to the fluid and further the impedance difference between the backing support and the sensor material would be large enough so much less energy would enter into the backing compared to PZT directly mounted. Alternatively, the energy that enters into the back support can be some¬ what dissipated and scattered by using a material such as a porous sintered type metal for the backing support and canceling out reflections with a calibrated pulse waveform. A major problem with copolymer materials is the lower D33 coefficient. (D33 is the dielectric constant in the thickness direction.) This makes a sensor of the same surface area have a larger impedance. This impedance difference could be com- pensated for by using some of the techniques described elsewhere within this specification or active circuitry could be placed next to the sensor to buffer the signal to a lower impedance.
PZT materials can also be used in the imaging guide wire embodiment, but they would likely need a front matching layer and a back decoupling layer. The backing configuration may include a half wave decoupler where its impedance is low with respect to both the sensor and backing support. This backing decoupler would work in the opposite manner from that of the matching layer, i.e. where a quarter wave length aids in coupling, a half wave length thickness helps in decoupling energy transfer between two impedances. In the imaging guide wire, the electrical connections would be made through the backing support to the back side of the sensor and to the outer conductors of the drive cable. The front connection would be made the same way as in the embodiment de¬ scribed above. For the copolymer alternative, con- nections would be made using one of the center drive cable wires and connecting the leads directly to the metallized copolymer surface using conductive epoxy or low temperature solder.
1. Imaging Guide Wire - Overall Construction The imaging guide wire, as described herein, is an intravascular imaging device having an ultrasonic sensor located at a distal end of an intravascular wire sized and adapted to be located within the guide wire lumen of conventional catheters used for intravascular procedures. As such, the imaging guide wire has several significant advantages. For example, the imaging guide wire can utilize the path provided by the guide wire lumen of a conventional catheter to image at the arterial location to which the catheter is advanced. Moreover, in several embodiments, the imaging guide wire may be provided with conventional guide wire features, e.g. a floppy spring tip, to enable the imaging guide wire to be used as both a conventional guide wire for positioning an intravascular catheter as well as imaging features, e.g. a sensor, to enable imaging the intravascular regions accessible thereby.
In order to be utilized in the above described manner, an embodiment of the imaging guide wire 450 is provided, as shown in Figure 34. The imaging guide wire 450 includes a tip section 452, a sensor section 454, a drive cable section 456, and a proximal connector section 458. As mentioned above, an essential requirement for the imaging guide wire is that it possess an outer profile of a size that allows it to fit through a guide wire lumen in conventional interventional catheters. In catheters that use 0WPWPCCOMSPECPROMPT§ @AWAAΛN*Y. Further, the drive cable section 456 should be very straight. Electrically, the drive cable 456 is preferably capable of sending a signal from one end to the other with minimum loss. In order to properly match the sensor impedance, high impedance in the drive cable 456 is preferred. The electrical impedance of the drive cable 456 is preferably in the range of 20 to 100 ohms. An embodiment of the drive cable 456 is illustrated in Figure 48. The drive cable 456 includes a core wire 564, an insulation layer 566, a shield layer 568, and a coil layer 570. The core wire 564 may possess several alternative constructions. In one embodiment, the core wire 564 is formed of a solid wire. Alternatively, the core wire may be formed of multi-strand copper or silver-plated copper wires. The latter embodiment provides good electrical characteristics and allows the drive cable 456 to be relativley floppy. However, a multi-strand construction may not provide sufficient longitudinal stiffness. Therefore, the core wire may preferably be formed of a material having a high modulus of elasticity thereby increasing the longitudinal stiffness. Materials like stainless steel, tungsten, and beryllium copper are preferred. Of these, tungsten is most preferred since it has the highest yield strength and the highest conductivity.
To provide for low electrical loss in the core wire 564, a high conductivity material is applied to the outer surface of the core wire 563. Preferred materials for applying to the outer surface of the core wire 563 include silver or copper. Silver is most preferred since it has the highest conductivity. These materials are easily plated to a thickness suitable for good electrical transmission. At high frequencies, electrical current stays close to the surface of a conductor and therefore a 0.001 inch of conductor plating over the core wire is sufficient. In a preferred embodiment, taking into account both mechanical and electrical requirements, the ideal thickness of the coating is less than 0.001 inch.
The insulation layer 566 in the imaging guide wire separates the conductive core layer 564 from the conductive shield layer 568. For electrical purposes, this layer 566 is nonconductive and preferably has as low of an dielectric constant as possible. If a solid wire is used for the core wire 564, it is preferred that a means be incorporated into the insulative layer 566 to restrict longitudinal motion between the core wire 564 and the outer coil 568. If the insulative layer 564 is made of Teflon, a direct bond may be difficult to make between the layers. In this case, movement between the core wire 564 and the outer layers can be restricted at the joint between the drive cable 456 and the sensor housing 354. This is preferably accomplished by using a nonconductive sleeve to bond between the core 564 and outer layers that will be connected to the sensor housing 354. This sleeve is made out of glass ceramic or other hard, nonconducting material. To bond between the layers along the length of the drive cable, holes are formed in the Teflon at various patterns to allow glue or other bonding material to be used to connect the layers together.
A material other than Teflon can be used for the insulation layer 566. Such other materials include glass strands or a solid extrusion of glass, kynar strands, or a ceramic extrusion. The extrusions would form a solid, uniform layer over the core wire out to a given diameter. The strands would then be expoxied to form a composite layer much like a fiber glass or other composite structure that uses fiber and binder to generate a unique high strength material.
The shield layer 568 is located over the insulating layer 566 to make up the outer layer of a coaxial signal cable. The shield 568 can be made from a braid of wires or a coil of wires. In a preferred embodiment, these wires are rectangular silver-plated copper wires. A single layer of coils may be used to provide the smallest diameter drive cable. A low resistance shield layer provides for RF emission shielding and susceptibility. Cable loss is a function of the core and shield total resistance, and accordingly, it is desirable to provide the shield with as low resistance as possible. For this reason, it is preferred that a braid or double coil is used for the shield layer. The outer coil layers 570 are needed for good torque transmission for performing the functions of both the drive cable and guide wire. The outer coil layers 570 are formed of copper or alternatively other metals like stainless steel. In a proximal section of the outer coil layer 570, a binder is used to bind all the layers together over a length thereof so as to make that portion of the imaging guide wire straight and stiff. This proximal section is from the proximal connector of the imaging guide wire to a location corresponding the end of the guide catheter with which the imaging guide wire would be used. This distance is typically 130 cm. This allows the distal section of the imaging guide wire to be relatively more flexible where it needs to go through tight bends. Another alternative way to provide additional stiffness in a proximal section of the imaging guide wire drive cable 456 is to provide another layer of material over the metal coil outer layer 570 along a proximal section. This additional layer may be formed of other-than-metal strands of glass, kevlar or other high strength materials. The strands would be used in a coil or braid layer over the core cable 570. The strands could then be epoxied to form a composite layer much like a fiber glass or other composite structure that uses fiber and binder thereby resulting in a unique, high-strength material. As described above, this can be a dual section composite in which «ne section is made out of one fiber and binder and the other section the same or different fiber and binder or a combination thereof. 5. Imaging Guide Wire Proximal Section
Referring again to Figure 34, a proximal section 458 of the imaging guide wire provides several functions. These functions include a connection for electrical contacts for signal transmission, torque transmission during imaging, torque and longitudinal moWPWPCCOMSPECPROMPT§ §ΛWAAΛN*Yrovided and used in quadrature, thereby allowing the direction to be determined. For absolute position information, gray scale encoding may be preferable. Gray scale coding has the property that only one bit changes in going from one state to the next. This prevents errors compared to binary scale for example, since there is no way of ensuring in binary scaling that all bits will change simultaneously at the boundary between two encoded values for binary or other codes.
Patterns for both radial acoustic indexing and 3-D lateral indexing may coexist on the sheath. Both patterns could be formed of the sheath material or could be formed of different materials. One pattern could be formed on the inner side of the sheath while the other on the outer side. Also, these patterns could be formed on the same surface.
F. Hydraulic Drive and Acoustic Indexing: Using acoustical rotational indexing allows determination of the sensor angular position inde¬ pendent of the proximal angular position of a mechanical drive shaft or cable. With this capability, means other than a mechanical drive shaft can be used to scan the vessel with a rotating acoustic beam. In a further embodiment of the present invention depicted in Figure 30, there is provided a rotating imaging device 408 for scanning of a vessel of a patient with a rotating acoustic beam that is driven by means other than a mechanical drive cable. In the embodiment shown, a rotatable mirror 410 is driven by a rotating hydraulic source 409. The rotating hydraulic source may be a jet and fin type turbine 412. The turbine 412 would propel the mirror 410 in a rotational direction. The speed of rotation of the mirror 410 could be controlled by varying the fluid flow rate. Using fluid, the rotation of a mirror 410 would be very smooth since there would be little friction from rotating shafts compared to mechanical drive devices. Bearings 414 could be provided to provide for smooth rotation. Feedback to the pulser for pulsing and speed monitoring would be provided using an acoustical indexing pattern 416 on the sheath in the rotational direction as described above. A transducer sensor 418 could be mounted either distally or proximally from the mirror and aimed to direct an acoustic pulse toward the angled face of the rotating mirror 410.
This configuration provides advantages for combining other functions into the device. With no moving parts over most of the length of the device, there is available substantial room to add other features. For example, it would be possible to integrate a balloon onto the device. The hydraulic course would already be present, and if the balloon is ported to the same fluid used for driving the mirror, all that would need to be done to inflate the balloon would be to control the input pressure independent of the output flow rate. This could control both the inflation pressure as well as the mirror rotation speed.
In a further embodiment, a rotating sensor 420 could be used instead of a rotating mirror by using a slip ring holder 422 to couple the signals to and from the rotating sensor 420 to a signal cable on a catheter, as shown in Figure 31. A hydraulic turbine 424 would drive this device just as described in the embodiment above with the mirror. As in the previous embodiment, an acoustic encoding pattern 426 would be included on the sheath portion of the device. This embodiment has the advantage that the sensor 420 could be designed with a thin backing with a hole there¬ through large enough for admitting a guide wire 428 through the center of the device. This would provide for over-the-wire placement of the device.
G. Data Graphics Pipeline Architecture In ultrasonic intravascular imaging, a large amount of data needs to be processed between the transducer being pulsed and the image being displayed and various means can be used for this processing. For example, processing can range from all analog to all digital. In most digital systems, the conditioned signal is acquired through data acquisition, processed by a computer, and displayed through some graphics hardware. This can be accomplished over a computer buss as long as there is a limited amount of trans- ferring being done. Current systems are very basic in the digital conditioning and image processing, and can utilize this approach.
It would be preferred to use digital condi¬ tioning functions to enhance the ultrasonic image or to provide for feature extraction. This would likely require a different data flow architecture to provide for additional data transfers needed to produce the image reasonably quickly. Figure 32 depicts a pipeline structure that provides this architecture. This architecture includes a dual pipeline: one for raw data and another for graphics data. The analog input from the sensor/conditioning is acquired from a high speed data acquisition circuit. This circuit synchronizes the raw data pipeline and transfers the data down the pipeline at a lower speed. The data is passed from one function to the next in real time or near real time speeds. This pipeline basically processes polar data. Since there would be much less data in the polar domain, it would be preferable to process this data as much as possible. These processing functions may include deconvolutions, fourier transform processing, neurocomputing processing or other techniques to enhance the raw data and do feature extraction.
At the end of the raw data pipeline, the data is converted to a graphics data stream through a large "look up table" (LUT) . This LUT essentially performs a polar to rectangular conversion. There are other ways to generate the graphics data from the raw data, but this is the preferable method. The graphics data can then be handled in the graphics pipeline. Processing functions performed here are those that preferably should be done in rectangular instead of polar coordinates. These may include edge detection, area calculations/manipulations, logical pixel edge smooth- ing, other area operations, and image overlays.
This architecture is ideal for intravascular imaging applications since the data can be acquired and processed from one function to the next with minimal time delay. The pipeline structure is very flexible for feature enhancements and additions, all that needs to be done is to change a cable between the appropriate location to add a new pipeline function. This struc¬ ture can accommodate a variable number of pipeline elements, as needed. Some of these pipeline functions include the provision for recording and playback of raw data. Also, a function may be provided for the buffering of raw data as the catheter is advanced or withdrawn through the guide wire lumen of the interventional catheter. This would provide the physician with information about the entire artery from the incision location to the coronaries. This data would likely not need to be viewed at the time it is obtained, however, it would be available for analysis off line after the procedure. The raw data can be stored on an optical disk, e.g. a WORM, that can store up to 1 Gbyte of data. It is estimated that during the relatively short period of time that the imaging guide wire is being advanced or withdrawn through the guide wire lumen of the catheter, the data is being generated at a rate of approximately 100 Mbytes/minute. A small variation on this architecture would include the addition of parallel pipelines. This could be done for example by taking the raw data acquisition output, branching off to a second LUT, and combining the two at the initial graphics pipeline function. This would allow two displays of the same raw data at the same time in different locations on the screen. This would be desirable if a real time enhanced display is desired while at the same time showing a slower 3-D reconstruction or enhanced feature detection. The data pipeline and graphics pipeline architecture, as described above, are advantageously integrated into a system environment. Figure 56 shows the pipeline structure integrated into one type of system environment. Figure 56 shows how the communication portion of the architecture can be implemented to allow the central system CPU to handle pipeline setup and configuration. This allows user input to effect changes in overlays, images and signal conditioning of data. Not every pipeline function may require a direct interface to a common buss. **An alternative to common bussing is daisy-chained communications. Here, the common processor would be able to perform the setup and configuration t*sks using a serial or parallel communication link. An external controller may be provided in the overall system configuration. This controller may issue commands to the system or may be directly memory-mapped to the functions on the system. This intersystem communication may employ techniques known and accepted to those of skill in the art. In the first method, the external controller may be connected in a serial or parallel manner and communicate with the system CPU. As with the keyboard, these commands can be queued and processed, or a handshaking can occur for synchronized command execution and communication. The memory-mapped external system control is performed by having the external system take control of the system common buss and accessing the hardware and memory directly. H. Acoustic Waveform Deconvolution
A major goal in acoustic imaging is high resolution of the image. It is desired to have an image with features as well defined as possible. One of the limitations to the image resolution is the attenuation of the signal with frequency. If there were a much higher signal to noise ratio, a higher frequency could be used, yielding a higher resolution image for a given size aperture device. Alternatively, a smaller device could be produced having the same resolution. Resolution may be defined as the distance at which two points are barely distinguishable. With acoustic beams using traditional imaging techniques, the resolution of the image is a function of the beam width at the points of interest.
In ultrasound imaging this is complicated by the fact that coherent acoustic fields are being used, so at a certain distance apart two reflectors can appear as one or two objects depending on the interfer¬ ence phase. This interference pattern or "speckle" can give a sense of higher resolution object separation than is actually possible with a beam of a given width. This speckle pattern can be useful because it gives a material a texture that can be meaningful for associ¬ ating certain properties or identifying the material. In the near field, an unfocused beam varies rapidly from point to point radially from the sensor surface as well as laterally through the beam.
Quantifying and defining resolution is difficult in the near field. Imaging in a more uniform beam can provide a more predictable result. In a focused beam, there are two regions where the beam is somewhat predictable. In the far field, the beam is of the form of an airy disk for a circular aperture and a mathematical Sine2 function for a rectangular aperture.
For signals, convolution is the summing in time of a finite pattern input into a output pattern using a transfer function. Deconvolution is the reverse process where from a given output the input pattern is found. For deconvolution, the accuracy of the determined input is a function of the accuracy of the measured output function and the accuracy of the transfer function.
A transfer function also exists for acoustical imaging but is in two dimensional space and time as well. The two dimensional space transfer function is proportional to the intensity of the acoustical beam at a given radius. This problem is more difficult than the one above but the same basic principles apply.
For acoustic beams, a knowledge of the beam shape and point intensity as a function of time is the major variable in performing a deconvolution on the acquired information. The beam shape and point intensity values are a function of sensor aperture, surface, uniformity, sensor construction tolerances, and diffraction/reflection of where the beam has come from and gone though. To know the beam values to any great detail is a very time consuming task if they are computed or measured.
In the near field and not in a focused region, the beam shape is varying rapidly as distance from the sensor changes. In the focused region and in the far field, the beam is more uniform and predict¬ able. In these regions deconvolution will be of some use. In the other areas of the beam as sensor tech¬ nology produces more uniform sound beams, this tech- nique will enhance the entire image. For the current system, most of the imaging is done in the far field in the rotationally lateral direction.
The resulting benefits from this routine are a sharper apparent resolution and a higher signal to noise ratio. The side lobes magnitude and the main beam size are the main determinates of the resolution of the image. Deconvolution will improve upon the limits set by both of these factors. The noise is reduced if the noise waveform has a small similarity with the acoustic transfer function, which is mostly the case.
The standard technique for performing a deconvolution is to use Fourier analysis. This is done by taking the Fourier transform of the output, dividing this by the Fourier transfer function, taking the inverse Fourier transform, and using the result. For a system where the transfer function is varying with time and space, the exact procedure is more complicated than this simple example. This is a very time consuming routine for current conditioning equipment, but a parallel network of processors could be built into the previously mentioned data pipeline in a direct or a parallel manner depending on how fast the process is and how much improvement in image results.
I. Neural Network Feature Detection Feature detection is a very complex problem. The goal is to enable the computer to identify and label various layers of the artery and atheroma. A type of atheroma that is truly identifiable from the pattern displayed is calcific plaque. This is un¬ mistakable to the eye as indicated by a bright area with a blocked out region behind. Even though it is easy for a human to learn how to identify this feature of the displayed image of an atherosclerotic diseased artery, it would be very difficult to write a program to identify and mark the region. Image processing and technology for object and feature detection is currently in a very early stage as far a technical sophistication. Most computer object detection is per- formed by performing a sequence of image transformation operations. The correct sequence is usually found iteratively by trying different combinations of the operations from a library of operations. Correct object detection is still a probabilistic event where certain combinations have a higher hit ratio than others.
Other techniques could include doing fourier analysis or other mathematical modeling techniques to analyze the data to determine the different features. From some of the published initial analysis of the materials, it is seen that most of the materials that must be distinguished from each other for feature detection have very close physical properties. The acoustical properties that are of concern are acoustical impedance, impedance variation, texture, density, velocity, attenuation all a function of frequency. Even if there is some exhibited variation in the physical parameters, it is still a formidable task to correlate the variable from the information acquired from ultrasound data. Neural networks have been found to be very useful in solving a number of very difficult problems. They are being used currently for speech recognition, autonomous vehicle guidance and many other complicated problems like this one where there are no clear and fast rules to model the inputs to the desired outputs. Neural networks are a scalable architecture defined as a number of weighted summing nodes organized in a layered manner. In Figure 33 there is depicted a diagram illustrating interconnections of a three layer network. Each layer node feeds its value forward as well as feedback to other layers. They can have any number of layers as well as any number of nodes per layer. The major advantage to neural networks is that the correct weighings on the input nodes can be determined by a learning process. The network is programmed by exposing it to inputs and telling it the correct output. By doing this repeatedly with many examples the network can determine what the weighing values need to be to give the most accurate answer. Determining the features in an ultrasound scan of an artery using neural networks is the best approach. After the network has learned the correct responses, a circuit could be developed to process the data in real time. Initially the network would be designed to operate on the data going through the raw data pipeline. Here, the network could work on a limited number of vectors at one time as inputs. This would keep the circuitry down to a practical level of parts. Handling the input raw data from one vector would require handling 500 points. For a number of complete vectors to be processed a large number of inputs result. A more reasonable approach is to use a network that processes a limited number of points from each vector and use more vectors. A circuit handling 25 radial points and 5 to 10 vectors could be developed with presently available hardware and yet contain all the neighborhood information from the acoustic beam that would be useful in reducing the data to an output feature.
J. Non-contacting slip rings
With mechanical rotating imaging transducers, one of the major concerns relates to making a good electrical contact between the rotating drive shaft and the proximal electronics from the proximal end of the imaging device. In a first preferred embodiment in a 3 Fr size imager, described above, the transmission of the electrical signal from the imager elongate shaft to the proximal electronics is provided by a mechanical contacting slip ring assembly 104. Although the slip ring assembly, as described above, provides excellent transmission, in alternative embodiments, it would be advantageous, and potentially a simplification of the interface, if a non-contacting means were employed to couple electrical signal between the rotating and non- rotating parts. Two alternative means for providing this transmission link are capacitive coupling and magnetic coupling.
A first alternative embodiment of the signal coupling assembly is shown in Figure 57. This embodiment employs capacitive coupling. Capacitive coupling can be used when the capacitance is large enough between the rotating and non-rotating contact rings. The capacitance is a function of the surface area, the gap distance and the effective dielectric constant. For a 30 Mhz signal, 100 pF would be more than enough capacitance to provide suitable coupling. A values greater or less than this would work also.
Capacitive contact rings 600 are shown to be longitudinally spaced, although alternatively, the rings 600 could be positioned radially. If positioned radially, one ring would be placed on the inner diameter and the other contact ring on the outer diameter of the assembly. With either capacitive or magnetic non- contacting slip rings, the mechanical energy is transferred by a keyed configuration or a friction fit. There are other means that could be used to transfer the mechanical energy, for example by a magnetic drive. By making the rotating contact rings out of a magnetic material or by placing a permanent magnetic in the assembly, the slip and drive shaft could be rotated without physical contact. A similar principle is used in stepper motors. There are several well known ways of generating an appropriate rotating magnetic field that the rotating contact rings would follow or of generating a stepping multi-phase magnetic field that would drive the center through the rotation phases that following the stepper rotation. Figure 58 shows an embodiment of a magnetic non-contacting slip ring assembly 604. This alternative embodiment includes a rotating and a non- rotating transformer coil 608 and 610. The energy is transferred by magnetic fields through the magnetic circuit. A consideration with this embodiment is air gaps reducing the coupling between the two coils. For this reason, the gap area 612 is enlarged to minimize this problem.
K. EEPROM Catheter Information Storage In present preferred and alternative embodiments of ultrasound imaging catheters, there are numerous parameters that are device dependant. Currently, all imaging device dependant information is entered manually or by shunting contact pins to provide some device type information. These parameters may be as simple as device type, frequency, device serial number, and production information. Other imaging parameters that are sensor dependant include those that would be used for a calibrated waveform pulser or coefficients that describe the acoustic waveform that would be used in image enhancement routines, as described above. This information must be entered into the system before imaging begins. However, it is not very user-friendly to force the user to enter the information manually into the system.
A feature that can be incorporated into any of the embodiments discussed herein provides for automatic imager information entry. An embodiment incorporating this feature is shown in Figure 59. The device dependant information is stored in a non¬ volatile storage medium 614. Such a storage medium is an EEPROM. In this embodiment, the information is available when the imaging catheter or imaging guide wire is plugged into the driving apparatus and control system 38. The means for connection could be direct wiring or an isolated reading means could be used. A minimum of two wires are typically needed to transfer information. Common serial EEPROM devices are available that operate off three wires and have a wide range of storage capacity. Also potentially available but not as desirable is parallel access non-volatile storage.
Another easy method of entering this information is to provide a separate data card or disk. This can be plugged into the system and the computer control can read the information before imaging begins.
L. Cath Lab System Integration
To use the imaging catheter or guide wire, drive and electrical connections must be made. A setup for achieving and facilitating this type of activity is illustrated in Figure 60. Figure 60 shows a motor box 620 attached to the edge of a patient table 622. A gooseneck device 624 extends the catheter connector over the table 622 and holds the imaging catheter or guide wire in place. It is important to keep the imaging catheter or guide wire straight while imaging. This gooseneck type device 624 allows movement back and forward easily to follow to doctor as the imaging is performed. Before and after imaging, the gooseneck device 624 and imaging catheter can be pushed back out of the way to eliminate some of the clutter on the patient table 622 as well as to protect the imaging drive shaft from getting bent. This gooseneck device 624 could have cables internal or external to its supporting structure. The goose neck device 624 preferably possesses a physical configuration and structure that can support a weight at a distance and be moved between two three-dimensional points.
Ultrasound imaging in catheter labs is currently performed by wheeling an ultrasound imaging system into the cath lab, setting up the system and catheter and then imaging. There are other methods of system integration that depend on the catheter lab setup. In prior cath lab setups, a direct connection is made between the motor 630 and conditioning unit (MCU) 632. The motor is typically in a cabinet on a cart and the MCU is mounted on the table. In this configuration, the proximal drive cable is laying across the floor and can be tripped on if the system is not next to the doctor. When the system is not next to the doctor, the MCU should have a connector on the floor, the table or hanging from the ceiling.
According to a preferred setup, a connector 634 is mounted to the table 622 so the MCU 632 cable follows the table 622 when it is moved. The system also has a plug 636 and could be unplugged for portable configurations. In this configuration, there is also a connector for video input from the fluoroscope and video outputs for displaying on the doctors' overhead monitor. Other system configurations include a rack mount system integrated into existing or modified catheter lab control hardware. In this configuration, the system is already on-line and when the doctor needs to perform an imaging procedure, the MCU 620 is mounted to the table 622 and plugged in. At this time, imaging could begin. The external controller could issue the system commands and the video outputs are multiplexed and displayed at the doctors overhead screen.
Another alternative configuration provides for the system to be located within the MCU 620. This could be provided if the system electronics were small enough to fit within a reasonable sized box to place on the table rack. Here, there is a manual interface on the unit and that can be operated remotely from an external controller. Also, a small monitor can be provided internally, but the preferred method of viewing would be externally on the overhead monitor. In this configuration, there is a plug for communications, video signals and power. It is intended that the foregoing detailed description be regarded as illustrative rather than limiting and that it is understood that the following claims including all equivalents are intended to define the scope of the invention.

Claims

WE CLAIM:
1. An imaging device comprising: a flexible elongate member having a distal end positionable within a intravascular vessel while a proximal end is positionable outside the body, said elongate member having a diameter of approximately 1.0 mm; a transducer sensor located at a distal end of said elongate member, said transducer sensor operable to scan the vessel walls; a signal conditioning apparatus connected to a proximal end of said elongate member for generating and receiving pulses to and from said transducer sensor.
2. The device of Claim 1 in which said elongate member has a diameter of approximately less than 1.07 mm.
3. The device of Claim 1 further comprising a coupling member for connecting said elongate member to said signal processor, said coupling member sized and adapted to be located outside of the patient's body.
4. The device of Claim 1 in which said an elongate member, said transducer sensor, and said signal conditioning apparatus have a matched electrical impedance whereby the need for separate impedance matching components is obviated.
5. The device of Claim 4 further including a distal drive cable connected to said transducer sensor, a proximal drive cable connected to said signal processor, a coupling member connecting said distal and said proximal drive cables, and further in which said distal and said proximal drive cables have an electrical transmission impedance matched to that of said transducer sensor.
6. The device of Claim 5 in which the length of said coupling member is such that no signal reflec¬ tions due to mismatched impedance are produced at the operating frequency of said signal processing unit.
7. An ultrasonic imaging apparatus for coronary vessels of a patient comprising: a flexible tubular transducer sheath having a distal end positionable in a coronary vessel of the patient while a proximal end extends out of the patient; a drive cable located in a lumen of said sheath, said drive cable connected at a proximal end to a motor for rotating said drive cable with respect to said sheath, said drive cable also connected at a proximal end thereof to a signal processing unit for generating and receiving electric pulses; and a sensor portion connected to a distal end of said drive cable and rotatable therewith in relation to said sheath, said sensor portion located within said sheath and generally along a central axis of said drive cable, said sensor portion including a transducer portion having a generally flat surface oriented to face perpendicularly to said axis.
8. The ultrasonic imaging apparatus of Claim 7 in which said transducer portion further comprises: a core portion; conductive layers located on opposite faces of said core portion; a matching layer located over a conductive layer on a face of said core portion; and a backing layer located over a conductive layer on an opposite face of said core portion from said matching layer and extending perpendicularly therefrom;
9. The ultrasonic imaging apparatus of Claim
8 in which said backing layer is approximately 0.012 inches thick.
10. The ultrasonic imaging apparatus of Claim 7 in which said sensor portion further comprises: a housing member in which said transducer portion is mounted, said housing member comprising an elongate hollow member having a first window adjacent to the surface of said transducer portion and oriented radially to said drive cable.
11. The ultrasonic imaging apparatus of
Claim 10 in which said housing member further comprises an elongate hollow member having a second window oriented radially to said drive cable and opposite from the first window.
12. The ultrasonic imaging apparatus of
Claim 10 in which the first window is generally rectangular having a greater dimension in a direction parallel to said axis.
13. The ultrasonic imaging apparatus of Claim 7 in which said transducer portion includes a generally rectangular active area with greater dimension in a direction parallel to said axis.
14. The ultrasonic imaging apparatus of Claim 7 in which said sensor portion further includes a charged coupled device connected to the transducer portion at a distal end of the drive cable.
15. The ultrasonic imaging apparatus of Claim 7 in which said sensor portion further includes multiple sensors located and mounted in a mounting holder at the distal end of the a drive cable.
16. In a device for ultrasonic imaging of a small vessel of a patient's body, the imaging device having an elongate member with a distal end position- able within the vessel while a proximal end is located outside the body, a transducer located at a distal end of the elongate member and operable to scan the vessel with ultrasonic pulses, a drive cable connected to the transducer and operable to transmit electrical signals to and from said transducer, and a signal processor connected to a proximal end of the drive cable for generating and receiving electrical pulses to and from the transducer, the elongate member comprising: a sheath having at least a distal portion thereof formed of a material transparent to an ultrasonic signal from the transducer whereby the signal may be transmitted through a wall of the sheath to the body of the patient for ultrasonic scanning thereof.
17. The elongate member of Claim 16 further comprising: an indexing marker located on said sheath and detectable by said pulsing of the transducer whereby the position of the transducer can be determined.
18. The elongate member of Claim 17 in which said indexing member further comprises a circumfer- ential indexing pattern whereby the angular position of the transducer can be determined.
19. The elongate member of Claim 17 in which said indexing member further comprises a longitudinal indexing pattern whereby the longitudinal position of the transducer can be determined.
20. The elongate member of Claim 17 in which said longitudinal indexing pattern indexing member is a gray scale pattern.
21. The elongate member of Claim 17 in which said longitudinal indexing pattern indexing member is a binary pattern.
22. A method for flushing an elongate member useful for ultrasonic imaging of a patient's vasculature comprising the steps of: providing an elongate sheath with a closed distal end and proximal end connected to a ported manifold; installing a flushing tubular member into a lumen of the sheath through a port of the manifold, said flushing tubular member having proximal and distal openings and further in which said flushing tubular member has an outside diameter less than the diameter of the lumen of the sheath; advancing the flushing tubular member into the sheath so that a distal end of the flushing lumen is proximate to the closed distal end of the sheath while a proximal end of the flushing tubular member extends proximally from the manifold port; flushing a fluid through the flushing tubular member from a proximal end thereof to the distal end; pressurizing the fluid in the sheath; draining some of the fluid from the sheath through a second port of the manifold; sealing the manifold to retain the remainder of the fluid in the sheath; withdrawing the flushing tubular member from the sheath; and installing a transducer connected to a drive cable into the lumen of the sheath
23. A method for flushing an elongate member useful for ultrasonic imaging of a patient's vascula¬ ture comprising the steps of: providing an elongate sheath with a closed distal end and proximal end connected to a ported manifold, said sheath having a main lumen and an outer lumen, the main lumen connected at a proximal end thereof to a manifold port and further in which a distal end of the main lumen communicates with the outer lumen; flushing a fluid into a proximal end of the outer lumen though and into the main lumen; pressurizing the fluid in the sheath; draining some of the fluid from the sheath through the port of the manifold; sealing the manifold to retain the remainder of the fluid in the sheath; installing a transducer connected to a drive cable into the lumen of the sheath.
24. A method for flushing an elongate member useful for ultrasonic imaging of a patient's vascula- ture comprising the steps of: providing an elongate sheath having a lumen with a permeable seal in a distal thereof, the seal made of a material to allow entrapped gases to diffuse therethrough, the sheath also having a proximal end connected to a ported manifold, flushing a fluid into a proximal end of the lumen while allowing gases entrapped in the lumen of the sheath to diffuse therethrough; pressurizing the fluid in the sheath; sealing the manifold to retain the fluid in the sheath; installing a transducer connected to a drive cable into
25. A drive cable for use in an imaging device for ultrasonic imaging of small vessels of a patient's body, the imaging device having an elongate member with a distal end positionable within a small vessel of the patient's body and a proximal end posi¬ tionable outside the body, a transducer located at a distal end of the elongate member and operable to scan the vessel walls, a drive cable connected to a proximal end of the transducer for generating and receiving pulses to and from the transducer, and a signal processor operable to transmit electrical signals to and from said transducer by means of the drive cable, the drive cable further comprising: an outer layered coil assembly; and a core wire located inside of said layered coil assembly.
26. The drive cable of Claim 25 in which said outer layered coil assembly further comprises a plurality of coaxial coil layers around said core wire.
27. The drive cable of Claim 26 in which said plurality of coaxial coil layers comprises three coaxial coil layers around said core wire.
28. The drive cable of Claim 26 in which said outer layered coil assembly further is comprised of at least one layer of flat wire.
29. The drive cable of Claim 27 in which each of said coil layers is comprised of a plurality of individual strands of flat wire helically wound.
30. The drive cable of Claim 26 in which each layer of said plurality of coil layers is com¬ prised of multiple individual strands of wires.
31. The drive cable of Claim 26 in which each layer of said plurality of individual layers is wound in an opposite helical direction from the layer immediately adjacent thereto.
32. The drive cable of Claim 25 in which said outer layered coil assembly includes a plating of a high conductivity material.
33. The drive cable of Claim 25 in which said core wire comprises a coaxial cable having an internal conductor and a external conductor separated from said internal conductor by an insulator.
34. The drive cable of Claim 33 in which said external conductor comprises: a braided shield formed of a plurality of wires.
35. The drive cable of Claim 34 in which said braided shield is comprised of a plurality of flat wires.
36. The drive cable of Claim 33 in which said external conductor includes a plating of a high conductivity material.
37. The drive cable of Claim 25 having a diameter of approximately 0.018 inches.
38. In an imaging device for ultrasonic imaging of small vessels of a patient's body, the imaging device having an elongate member with a distal end positionable within a intravascular vessel while a proximal end is located outside the body, a transducer located at a distal end of the elongate member and operable to scan the vessel with ultrasonic pulses, a distal drive cable connected at a distal end thereof to the transducer and operable to transmit electrical signals to and from said transducer, a proximal drive cable, a signal processor connected to a proximal end of the proximal drive cable for generating and receiving pulses to and from the transducer, a motor connected to the proximal end of the proximal drive cable to rotate the transducer, and a coupling member for connecting the distal drive cable and the proximal drive cable, the coupling member further comprising: a distal section connected to the elongate member and to a proximal end of the distal drive cable and adapted to allow rotational movement between the elongate member and the distal drive cable, and a proximal section releasably connectable to the distal section, said proximal section connected the proximal portion of the drive cable.
39. The coupling member of Claim 38 in which the distal section comprises: a sleeve portion connected to the elongate member; and a first rotating coaxial member located inside said sleeve portion connected to the distal drive cable.
40. The coupling member of Claim 39 in which the proximal portion comprises: a sleeve portion connected to the proximal drive cable; a second rotating coaxial member located inside said sleeve portion, said second rotating member matably engageable with said first rotating coaxial member; an electrical signal transfer apparatus con¬ nected to said second rotating coaxial member for transferring the electrical signal from the second rotatable coaxial member to a stationary electrical conductor; and a rotating drive shaft connected proximally to the motor and distally to the second rotatable coaxial member.
41. The coupling member of Claim 40 in which the electric signal transfer apparatus comprises: a first conductor connected to said second rotating coaxial member; and a second conductor slidably engaged against the first conductor whereby an electrical signal can be transmitted to and from said first to said second con¬ ductors.
42. The coupling member of Claim 41 in which said conductors are a brush and slip ring.
43. An imaging device for ultrasonic imaging of small vessels of a patient's body comprising: an elongate member with a distal end posi¬ tionable within a vessel of the patient and a proximal end positionable outside the body, a transducer located at a distal end of the elongate member and operable to scan the vessel walls, a drive cable having a rotatable distal portion a distal end thereof connected to said transducer and operable to transmit electrical signals to and from said transducer, a proximal portion including a rotating proximal portion and stationary proximal portion adjacent thereto; a signal processor for generating and receiv- ing pulses to and from said transducer, said signal processor connected to said stationary proximal portion of said drive cable, a motor for rotating said transducer, said motor connected to a proximal end of said rotatable proximal portion of said drive cable, and a coupling member for releasably connecting said proximal and said distal portions of said drive cable.
44. A data processing architecture for use in an imaging device for ultrasonic imaging of a small vessel of a patient's body, the imaging device having an elongate member with a distal end positionable within the small vessel and a proximal end positionable outside the body, a transducer located at a distal end of the elongate member and operable to scan the vessel walls, a drive cable connected to the transducer and operable to transmit electrical signal to and from the transducer, and a signal processor connected to a proximal end of the drive cable for generating and receiving pulses to and from the transducer, the data processing architecture comprising: a raw data pipeline adapted to process polar coordinate data derived from the signals produced by the transducer: a means responsive to the raw data pipeline and a look up table for converting data from the raw data pipeline to rectangular coordinate data and outputting rectangular coordinate data; and a graphics data pipeline responsive to the output of the converting means.
45. An imaging guide wire for navigating into small vessels of a person's vasculature and imaging the small vessels from within, comprising: an elongate drive shaft having dimensions suitable for positioning into small vessels of the person's vasculature via a lumen of a conventional catheter, said elongate shaft having a size to be positioned in and advanced via a guide wire lumen of the conventional catheter into the small vessels of the person's vasculature; a transducer portion connected to the distal portion of the elongate shaft, said transducer portion also sized to be positioned into the small vessels of the person's vasculature via the lumen of the catheter; a proximal section connected to the proximal end of the elongate shaft for transmission of electrical signals from a proximal control apparatus to the transducer via the elongate drive shaft and also to transmit mechanical energy from a proximal drive apparatus to the elongate drive shaft to rotate the transducer for imaging.
46. The imaging guide wire of Claim 45 in which said elongate drive shaft is not more than approximately 0.018 inch.
47. The imaging guide wire of Claim 45 in which said transducer portion is mounted in a transducer housing mount having an aperature therein through which ultrasonic signals can pass, said aperature having a dimension of approximately 0.012 inch.
48. The imaging guide wire of Claim 45 in which said transducer portion is comprised of: a piezoelectric sensor having a face portion, said face portion comprised of a plurality of separate elements.
49. The imaging guide wire of Claim 48 in which said separate elements are formed of a single piezoelectric material having slices formed in the face thereof.
50. The imaging guide wire of Claim 49 in which said slices are parallel to a longitudinal axis of the drive shaft.
51. The imaging guide wire of Claim 49 in which two or more of said plurality of elements are connected to a single pair of cable leads for simultaneous excitation of said two or more elements.
52. The imaging guide wire of Claim 49 in which all the elements forming said transducer portion are connected to a single pair of cable leads for simultaneous excitation of all the elements.
53. The imaging guide wire of Claim 49 in which said elements are connected across the thickness of the elements.
54. The imaging guide wire of Claim 49 in which said elements are connected across the width of the elements.
55. The imaging guide wire of Claim 49 in which said transducer portion is mounted in a transducer housing mount having an aperature therein through which ultrasonic signals can pass, and in which said aperature is circular and in which the slices are formed as straight lines parallel to a longitudinal axis of the drive shaft.
56. The imaging guide wire of Claim 49 in which said transducer portion is mounted in a transducer housing mount having an aperature therein through which ultrasonic signals can pass, and in which said aperature is circular and in which the slices are formed as circular concentric slices forming circular elements.
57. The imaging guide wire of Claim 49 in which said transducer portion is mounted in a transducer housing mount having an aperature therein through which ultrasonic signals can pass, and in which said aperature is circular and in which the slices are formed as spiral slices forming spiral elements.
58. The imaging guide wire of Claim 47 in which surfaces of the sensor and the mount are treated to increase the surface tension between the surrounding fluid and said surfaces.
59. The imaging guide wire of Claim 47 further comprising: a protective sheath formed over the aperture over the transducer portion.
60. The imaging guide wire of Claim 59 in which said sheath is formed in a shape having a surface that fills the space in front of said transducer portion.
61. The imaging guide wire of Claim 47 further comprising: an exponential matching layer located over the aperature over said transducer portion, said exponential matching layer formed of a series of layers in which the impedance follows in an exponential manner from one layer to another.
62. The imaging guide wire of Claim 45 further comprising: a backing layer located on a back side of said transducer portion; and a spline structure mounted adjacent the backing layer.
63. The imaging guide wire of Claim 45 in which said transducer portion is a wedge geometry transducer.
64. The imaging guide wire of Claim 63 in which one of the backing surfaces of said wedge geometry transducer has a quarter wavelength grating surface located thereon to attenuate reflections from said surface.
65. The imaging guide wire of Claim 45 further comprising: a control apparatus connected to the proximal section for sending and receiving signals, said control apparatus further comprising: a vector averaging circuit to filter out fast moving blood scattering return signals.
66. The imaging guide wire of Claim 45 in which said transducer portion is comprised of: a first sensor for operating at a first frequency; and a second sensor located over said first sensor, said second sensor for operating at another frequency.
67. The imaging guide wire of Claim 45 further comprising: a floppy spring tip connected to and extending distally of said transducer portion, whereby the imaging guide wire can be used for positioning an intravascular catheter as well as for imaging arterial features accessible by means of the guide wire lumen of the intravascular catheter.
68. The imaging guide wire of Claim 67 further comprising: a strain relief section connecting the floppy tip to the transducer section.
69. The imaging guide wire of Claim 68 in which said strain relief section comprises a gradually increasing core wire diameter.
70. The imaging guide wire of Claim 67 further comprising: a releasable locking means connected to said tip to allow said tip to stay stationary with respect to the artery when said transducer portion is being rotated for imaging and which locks said tip to the transucer portion when said imaging guide wire is used for steering.
71. The imaging guide wire of Claim 70 in which said releasable locking means comprises: a means for providing a fluid pressure on a hydraulic piston, said piston connected to said tip, whereby when said piston is pressurized said tip is locked to the transducer portion.
72. The imaging guide wire of Claim 45 in which said drive cable comprises: a core wire; an insulation layer surrounding said core wire; a shield layer surrounding said insulation layer; and a coil layer surrounding said shield layer.
73. The imaging guide wire of Claim 72 in which said core wire comprises: multi-strand, plated copper wires.
74. The imaging guide wire of Claim 73 in which said core wire is plated with a high conductivity material to a thickness of less than 0.001 inch.
75. The imaging guide wire of Claim 73 in which said core wire is plated with silver.
76. The imaging guide wire of Claim 72 in which said core wire comprises: a solid wire of a material having a high modulus of elasticity to increase longitudinal stiffness.
77. The imaging guide wire of Claim 76 in which said core wire is comprised of a material selected from a group consisting of: stainless steel, tungsten, and beryllium copper.
78. The imaging guide wire of Claim 72 in which said insulation layer is formed of a material selected from a group consisting of: Teflon, glass strands, a solid extrusion of glass, kynar strands, and a ceramic extrusion.
79. The imaging guide wire of Claim 78 in which said insulation layer comprises: a means to restrict longitudinal motion between said core wire and said shield layer.
80. The imaging guide wire of Claim 72 in which said shield layer is formed of a braid of rectangular silver-plated copper wires.
81. The imaging guide wire of Claim 72 in which said outer coil layers are formed of a material selected from a group consisting of: copper and stainless steel.
82. The imaging guide wire of Claim 45 in which said elongate drive shaft is not more than approximately 0.014 inch.
83. A method for ultrasonic imaging of a region of the cardiovascular system of a person in conjunction with an interventional procedure, comprising the steps of: positioning a catheter having an interventional therapeutic device associated with a distal portion thereof for the purpose of performing a therapeutic procedure at the region of the person's vasculature with the interventional therapeutic device, said catheter also having a lumen therein into which a guide wire can be received to position the catheter into the patient's vasculature so that the distal portion is proximate to the site; positioning an imaging guide wire having an ultrasonic transducer at a distal end thereof into the patient's vasculature through the lumen of the catheter having the interventional device associated therewith so that the ultrasonic transducer is located at the region of the person's vasculature; and scanning the region of the person's vasculature with the imaging guide wire having the ultrasonic transducer at the distal end thereof.
84. The method of Claim 83 in which said imaging guide wire includes a distal tip that can be used to position said wire intravascularly, and further comprising the steps of: routing the imaging guide wire into the region of the person's vasculature in advance of the catheter; and advancing the catheter over the imaging guide wire.
85. The method of Claim 84 further comprising: imaging by rotating the imaging guide wire while the transducer portion is at the site.
86. The method of Claim further 84 comprising: routing a sheath over the the imaging guide wire before the wire is rotated for imaging.
87. The method of Claim 86 in which the tip of the imaging guide wire extends distally of the sheath while imaging.
88. The method of Claim 86 in which the tip of the imaging guide wire is drawn back into the sheath before rotating for imaging.
89. The method of Claim 85 in which the imaging guide wire is rotated at a speed of a fraction of a hertz.
90. The method of Claim 85 in which the imaging guide wire is rotated manually.
91. The method of Claim 85 further comprising: rotating the imaging guide wire while the transducer portion of said imaging guide wire is underneath said interventional therapeutic device.
92. The method of Claim 85 further comprising: performing a therapeutic procedure at the region of the person's vasculature with the interventional therapeutic device.
93. The method of Claim 92 further comprising: after performing the interventional therapeutic procedure, withdrawing the interventional therapeutic device.
94. The method of Claim 93 further comprising: after withdrawing the interventional therapeutic device, imaging with the imaging guide wire at the site.
95. The method of Claim 94 further comprising: advancing a second interventional catheter over the imaging guide wire.
96. The method of Claim 84 further comprising: moving the interventional therapeutic catheter and the imaging guide wire together to another arterial location.
97. The method of Claim 83 in which the catheter has a short guide wire lumen at the distal end thereof and a proximal entrance to the short guide wire lumen is located in a portion of the catheter normally within the body during use.
98. The method of Claim 97 further comprising: positoning a reinforcing sheath over ~the imaging guide wire up to the proximal guide wire lumen entrance.
99. The method of Claim 83 further comprising: positioning the catheter with a separate, conventional guide wire; and withdrawing the conventional guide wire from the guide wire lumen of the catheter prior to positioning the imaging guide wire in the guide wire lumen of the catheter.
100. A data processing architecture for use in an imaging device for ultrasonic imaging of small vessels of a patient's body, the imaging device having a transducer sized and adapted to be positioned intravascularly to scan small vessels of the patient's body from within a small vessel, a drive cable having a distal end connected to the transducer and operable to transmit electrical signals to and from the transducer and to rotate the transducer to scan the vessel of the person's body with ultrasonic waves, and a signal processor adapted for generating and receiving signals to and from the transducer via the drive cable, the data processing architecture comprising: a raw data pipeline adapted to process polar coordinate data derived from the signals produced by the transducer; a means connected to said pipeline for storing raw data produced during advancement of the imaging device to the small vessels or withdrawal of the imaging device from the small vessels; a means responsive to the raw data pipeline and a look up table for converting data from the raw data pipeline to rectangular coordinate data and outputting rectangular coordinate data; and a graphics data pipeline responsive to the output of the converting means.
101. In an imaging device for ultrasonic imaging of small vessels of a patient's body, the imaging device having a transducer sized and adapted to be positioned intravascularly to scan small vessels of the patient's body from within the small vessel, a drive cable having a distal end connected to the transducer and operable to transmit electrical signals to and from the transducer and to rotate the transducer to scan the vessel of the person's body with ultrasonic waves, a signal processor adapted for generating and receiving signals to and from the transducer via the drive cable, and a motor adapted for connecting to the drive cable to rotate the transducer, a coupling member to connect a proximal drive cable to the signal processor and the motor, the coupling member comprising: a mechanical connector for releasably connecting the motor to a proximal end of the drive cable; a non-contacting signal transmission apparatus having; a rotating portion adapted to releasably connect to the proximal end of the drive cable; and a non-rotating portion connected to the signal processor and to transmit signals between said signal processor and the rotating portion, said rotating and said non-rotating portions not being in contact with each other along the signal transmission path.
102. The coupling member of Claim 101 in which said rotating and non-rotating portions further comprise: capacitive sensing means to transmit and sense the signal between said rotating and non-rotating portions.
103. The coupling member of Claim 101 in which said rotating and non-rotating portions further comprise: magnetic means to transmit and sense the signal between said rotating and non-rotating portions.
104. An imaging device for ultrasonic imaging of small vessels of a patient's body, the imaging device connectable to a signal processor for generating and receiving signals scan the vessels with ultrasonic pulses from within, the imaging device comprising: a transducer sized to be positioned into the small vessels of the person's vasculature to scan the person's vasculature with ultrasonic pulses from within; an elongate drive shaft connected at a distal portion thereof to the transducer, said elongate drive shaft also having dimensions suitable for positioning into small vessels of the person's vasculature, said elongate drive shaft adapted to transmit electrical signals therethrough between the signal processor and the transducer; and an information storage medium associated with the imaging device, said information storage medium adapted to store device specific information about the imaging device and be readable by the signal processor when the device is connected thereto.
105. The imaging device of Claim 104 in which said information storage medium is located in a portion connected to the drive shaft.
106. The imaging device of Claim 105 in which said information storage medium is an EEPROM.
PCT/US1992/002117 1991-03-13 1992-03-13 Intravascular imaging apparatus and method WO1992016147A1 (en)

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EP0529069A4 (en) 1995-09-27
CA2082161A1 (en) 1992-09-14
JP2000070270A (en) 2000-03-07
JPH05508099A (en) 1993-11-18
EP0529069A1 (en) 1993-03-03

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