Broadband phased array transducer design with frequency controlled two dimension capability and methods for manufacture thereof

• US 5,438,998 A
• Filed: 09/07/1993
• Issued: 08/08/1995
• Est. Priority Date: 09/07/1993
• Status: Expired due to Term

• Current Assignee: Siemens Medical Solutions USA Incorporated (Siemens AG)
• Original Assignee: Acuson Corporation (Siemens AG)
• Inventors: Hanafy, Amin M.
• Primary Examiner(s): JAWORSKI, FRANCIS J
• Application Number:
  US08/117,869
• Time in Patent Office: 700 Days
• Field of Search: 128/661.01, 128/662.03, 73/633, 310/334, 310/368, 310/369
• US Class Current: 600/459
• CPC Class Codes: B06B 1/0622 on one surface
• CPC Class Codes: B06B 1/0644 using a single piezoelectric element B06B1/0688 takes precedence
• CPC Class Codes: G10K 11/32 characterised by the shape of the source
• CPC Class Codes: H04R 17/08 signals being recorded or played back by vibration of a stylus in two orthogonal directions simultaneously

Abstract

There is provided a transducer array with a plurality of piezoelectric elements having a minimum and maximum thickness. In one embodiment, the maximum thickness is less than or equal to 140 percent of the minimum thickness. In an alternate embodiment, the maximum thickness is greater than 140 percent of the minimum thickness and the transducer array is capable of simulating the excitation of a wider aperture two-dimensional transducer array. One or more matching layers may be used to further increase bandwidth performance. In addition, a two crystal transducer element as well as a composite transducer structure may be formed using the principles of this invention.

Claims

1. A transducer for producing an ultrasound beam upon excitation comprising:

a plurality of piezoelectric elements, each of said elements comprising a thickness at at least a first point on a surface facing a region of examination being less than a thickness at at least a second point on said surface, said surface being generally non-planar, said surface having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction.

2. The transducer of claim 1 wherein the surface of said each of said elements acts to produce an exiting pressure wave comprising at least two peaks.

3. The transducer of claim 1 wherein said surface is a curved surface.

4. The transducer of claim 3 further comprising a back portion opposing said surface, said back portion being a generally planar surface.

5. The transducer of claim 3 further comprising a back portion opposing said surface, said back portion being concave in shape.

6. The transducer of claim 3 further comprising a back portion opposing said surface, said back portion being convex in shape.

7. The transducer of claim 3 further comprising an acoustic matching layer positioned between a body being examined and at least one of said elements.

8. The transducer of claim 7 wherein said matching layer has a matching layer thickness LML approximated by (1/2)(LE)(CML/CE), where, for a given point on the transducer surface, LML is the thickness of the matching layer, LE is the thickness of the transducer element, CML is the speed of sound of the matching layer, and CE is the speed of sound of the element.

9. The transducer of claim 8 further comprising a coupling element disposed on said matching layer comprising acoustic properties similar to said body being examined.

10. The transducer of claim 9 wherein a surface of said coupling element is slightly concave in shape.

11. The transducer of claim 3 wherein said curved surface of said element enables said element to be operable at a dominant fundamental harmonic frequency and is operable at a dominant second harmonic frequency.

12. The transducer of claim 1 wherein each of said elements is plano-concave.

13. The transducer of claim 12 wherein each of said elements further comprises side portions at each end of said element, said thickness being a maximum near said side portions of each of said elements and said thickness being a minimum substantially near a center of each of said elements.

14. The transducer of claim 13 wherein said element is formed of one of lead zirconate titanate, composite material, and polyvinylidene fluoride.

15. An ultrasound transducer comprising:

a plurality of piezoelectric elements each comprising a front portion facing a region of examination, a back portion, two side portions, and a thickness between said front portion and said back portion;

said thickness being greater at each of said side portions than between said side portions;

said front portion being generally non-planar, said front portion having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction;

wherein each of said elements produces an ultrasound beam having a width which varies inversely as to a frequency of excitation of a given element.

16. The transducer of claim 15 wherein each of said elements is plano-concave.

17. The transducer of claim 16 further comprising at least one acoustic matching layer positioned between a body being examined and at least one of said elements.

18. The transducer of claim 15 wherein each of said curved surface of said elements enables said element to be operable at a dominant fundamental harmonic frequency and is operable at a dominant second harmonic frequency.

19. A transducer for producing an ultrasound beam upon excitation at a given frequency comprising:

a piezoelectric element comprising a front portion facing a region of examination being generally non-planar, said front portion having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction, wherein said element operates at a dominant fundamental harmonic frequency and a dominant second harmonic frequency.

20. The transducer of claim 19 wherein said element is plano-concave.

21. An ultrasound transducer comprising:

a plano-concave piezoelectric element comprising a curved front surface facing a region of examination, a back surface, two sides, and a thickness between said front surface and said back surface, said front surface comprising a radius of curvature approximated by the equation h/2+(w² /8h), where h is the difference between a minimum and maximum thickness of said transducer element and w is the width of said transducer element between said sides, wherein said element produces an ultrasound beam having a width which varies inversely as to a frequency of excitation of said element.

22. The transducer of claim 21 wherein said curved surface of said element enables said element to be operable at a dominant fundamental harmonic frequency and is operable at a dominant second harmonic frequency.

23. An array-type ultrasonic transducer comprising:

a plurality of transducer elements disposed adjacent to one another, each of said elements comprising a front portion facing a region of examination, a back portion, two side portions, and a transducer thickness between said front portion and said back portion,

said transducer thickness being a maximum thickness at said side portions and a minimum thickness between said side portions, said maximum thickness being less than or equal to 140% of said minimum thickness.

24. The transducer of claim 23 wherein said maximum thickness is less than or equal to 140% of said minimum thickness and greater than or equal to 120% of said minimum thickness.

25. The transducer of claim 23 further comprising a curved acoustic matching layer disposed on said front portion of each of said elements, said matching layer comprising a matching layer thickness LML approximated by (1/2)(LE)(CML/CE), where, for a given point on the transducer surface, LML is the thickness of the matching layer, LE is the thickness of the transducer element, CML is the speed of sound of the matching layer, and CE is the speed of sound of the element.

26. The transducer of claim 23 wherein said elements are comprised of PZT and are plano-concave in shape, said front portion being curved in surface, and said minimum thickness being substantially near a center of each of said elements.

27. An ultrasound system for generating an image comprising:

transmit circuitry for transmitting electrical signals to a transducer probe;

a transducer probe for transmitting an ultrasound beam produced by a given frequency excitation and for receiving pressure waves reflected from a body being examined;

receive circuitry for processing the signals received by said transducer probe;

a display for providing an image of an object being observed;

said transducer probe comprising a plurality of piezoelectric elements, each of said elements comprising a thickness at at least a first point on a surface facing a region of examination being less than a thickness at at least a second point on said surface, said surface being generally non-planar and having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction, wherein said ultrasound beam has a width which is related to said frequency of excitation of said element.

28. The system of claim 27 wherein each of said elements is plano-concave.

29. The system of claim 28 further comprising an acoustic matching layer positioned between said body being examined and at least one of said surfaces.

30. A method of making a transducer for producing an ultrasound beam upon excitation comprising the steps of:

forming a plurality of piezoelectric elements, each of said elements comprising a thickness at at least one point on a surface facing a region of examination being less than a thickness at at least one other point on said surface such that an aperture of said ultrasound beam varies inversely as to a frequency of excitation of each of said elements, said surface being generally non-planar and having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction; and

establishing an electric field through at least one portion of each of said elements.

31. The method of claim 30 wherein said step of establishing an electric field comprises placing a first electrode on each of said surfaces and placing a second electrode on a portion opposing each of said surfaces.

32. The method of claim 31 further comprising the step of placing an acoustic matching layer positioned between an object being examined and at least one of said elements.

33. The method of claim 32 wherein said matching layer has a matching layer thickness LML approximated by (1/2)(LE)(CML/CE), where, for a given point on the transducer surface, LML is the thickness of the matching layer, LE is the thickness of the transducer element, CML is the speed of sound of the matching layer, and CE is the speed of sound of the element.

34. The method of claim 33 further comprising the step of placing a coupling element comprising acoustic properties similar to said object being examined on said matching layer.

35. The method of claim 34 wherein a surface of said coupling element is slightly concave in shape.

36. A method of making a transducer for producing an ultrasound beam upon excitation comprising the steps of:

forming a plurality of transducer elements disposed adjacent to one another, each of said elements comprising a front portion facing a region of examination, a back portion, two side portions, and a transducer thickness between said front portion and said back portion, said transducer thickness being a maximum thickness at said side portions and a minimum thickness between said side portions, said maximum thickness being less than or equal to 140% of said minimum thickness; and

establishing an electric field through at least one portion of each of said elements.

37. The method of claim 36 further comprising the step of placing an acoustic matching layer positioned between an object being examined and at least one of said elements.

38. The method of claim 37 wherein said matching layer has a matching layer thickness LML approximated by (1/2)(LE)(CML/CE), where, for a given point on the transducer surface, LML is the thickness of the matching layer, LE is the thickness of the transducer element, CML is the speed of sound of the matching layer, and CE is the speed of sound of the element.

39. A method of producing an image in response to excitation of a transducer for generating an ultrasound beam comprising the steps of:

providing electrical signals to a transducer probe for transmitting a beam of ultrasound pressure waves to a body being examined such that said transducer probe includes a plurality of piezoelectric elements, each of said elements comprising a thickness at at least one point on a surface facing a region of examination being less than a thickness at at least one other point on said surface, said surface being generally non-planar and having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction, and an aperture of an ultrasound beam varying inversely as to a frequency of excitation of said element;

receiving pressure waves reflected from said body and converting said received pressure waves into received electrical signals;

processing said received electrical signals; and

displaying the object being observed.

40. The method of claim 39 further comprising the step of placing an acoustic matching layer between said object being observed and at least one of said piezoelectric elements.

41. The method of claim 40 further comprising the step of placing a coupling element comprising acoustic properties similar to a body being examined on said matching layer.

42. The method of claim 41 wherein a surface of said coupling element is slightly concave in shape.

43. The method of claim 42 further comprising the step of applying said probe to said object and placing ultrasound gel between said probe and said object.

44. A transducer having bandwidth activation energy for producing an ultrasound beam comprising:

a plurality of piezoelectric elements each comprising a front portion facing a region of examination, a back portion, two side portions, and a thickness between said front portion and said back portion;

said thickness being a maximum value LMAX near each of said side portions and a minimum value LMIN between said side portions;

said front portion being generally non-planar;

wherein an increase in said bandwidth activation energy is approximated by the ratio LMAX/LMIN.

45. The transducer of claim 44 further comprising two acoustic matching layers positioned between a body being examined and at least one of said elements.

46. The transducer of claim 44 wherein said transducer suppresses the generation of reflections at an interface of said transducer and an object being examined.

47. The transducer of claim 44 wherein a signal produced by said transducer is stronger between said side portions than at said side portions.

48. A transducer for producing an ultrasound beam upon excitation comprising:

a plurality of piezoelectric elements, each of said elements comprising a thickness at a first point on a surface facing a region of examination being less than a thickness at a second point on said surface, said surface being generally non-planar, said thickness at said second point being less than or equal to 140% of said thickness at said first point;

wherein each of said elements produces an ultrasound beam having a width which varies inversely as to a frequency of excitation of a given element.

49. The transducer of claim 48 wherein said thickness at said second point is less than or equal to 140% of said thickness at said first point and greater than or equal to 120% of said thickness at said first point.

50. The transducer of claim 48 further comprising a curved acoustic matching layer disposed on said surface of each of said elements, said matching layer comprising a matching layer thickness LML approximated by (1/2)(LE)(CML/CE), where, for a given point on the transducer surface, LML is the thickness of the matching layer, LE is the thickness of the transducer element, CML is the speed of sound of the matching layer, and CE is the speed of sound of the element.

51. A transducer for producing an ultrasound beam upon excitation comprising:

a plurality of piezoelectric elements each comprising a front portion facing a region of examination, a back portion, two side portions, a center portion between said side portions, and a thickness between said front portion and said back portion, said thickness being greater at each of said side portions than between said side portions, said front portion being generally non-planar and having a radius of curvature along an elevation direction which is different than a radius of curvature along an azimuthal direction;

a plurality of first electrodes, each one of said first electrodes disposed on said back portion of a corresponding one of said piezoelectric elements;

a plurality of second electrodes, each one of said second electrodes disposed between a body being examined and said front portion of a corresponding one of said piezoelectric elements;

wherein an electric field between said first and second electrodes is greater at said center portion than said side portions.

52. The transducer of claim 51 wherein the relationship of said transducer suppresses portions to suppress the generation of sidelobes.

53. The transducer of claim 51 wherein a signal produced by said transducer is stronger between said side portions than at said side portions.

54. The transducer of claim 51 wherein each of said elements is plano-concave.

55. The transducer of claim 54 further comprising at least one acoustic matching layer positioned between said body being examined and at least one of said elements.

56. The transducer of claim 55 wherein said matching layer has a matching layer thickness LML approximated by (1/2)(LE)(CML/CE), where, for a given point on the transducer surface, LML is the thickness of the matching layer, LE is the thickness of the transducer element, CML is the speed of sound of the matching layer, and CE is the speed of sound of the element.

57. The transducer of claim 51 wherein each of said elements produces a beam having a narrow aperture at higher frequencies.