Method and apparatus for damping vibration in turbomachine components

• US 6,299,410 B1
• Filed: 02/23/1999
• Issued: 10/09/2001
• Est. Priority Date: 12/26/1997
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Pearson, David D., Hilbert, Gary R., Crawley, Edward F.
• Primary Examiner(s): Verdier, Christopher
• Assistant Examiner(s): WOO, RICHARD SUKYOON
• Application Number:
  US09/502,443
• Time in Patent Office: 959 Days
• Field of Search: 415/1, 415/119, 415/10, 415/14, 416/145, 416/144, 416/500, 416/248
• US Class Current: 416/145
• CPC Class Codes: F01D 5/16 for counteracting blade vibration
• CPC Class Codes: F16F 15/005 using electro- or magnetostrictive actuation means generating of mechanical vibrations operating with electrostriction B06B1/06, with magnetostriction B06B1/08; vehicle suspension arrangements characterised by use of piezoelectric elements B60G17/01941; piezoelectric, electrostrictive and magnetostrictive devices per se H10N30/00
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10S 416/50 Vibration damping features

Abstract

A method and apparatus reduces the magnitude of vibratory strain in a turbomachine component that experiences high steady state strain by, in the case of a passive embodiment, coupling a mechanical-to-electromagnetic energy converter to an interior and/or exterior surface of the component, and/or embedding the energy converter within the component, and by, in the case of an active embodiment, coupling a mechanical-to-electromagnetic energy converter to an interior and/or exterior surface of the component.

Claims

1. An apparatus for passive damping of vibratory strain in a turbomachine component that experiences high steady state strain, the vibratory strain having associated with it mechanical energy, the apparatus comprising:

a mechanical-to-electromagnetic energy transformer mechanically coupled to the component, said energy transformer receiving mechanical energy associated with the vibratory strain of the component and producing, from said mechanical energy, electromagnetic energy; and

an electromagnetic circuit electromagnetically coupled to said energy transformer, said circuit receiving electromagnetic energy, from said energy transformer, that is then dissipated through passive damping.

2. The apparatus of claim 1 disposed in an engine wherein the engine has a gas path and the component comprises an air management surface for the gas path.

3. The apparatus of claim 1 wherein the component is an airfoil.

4. The apparatus of claim 1 wherein the component is a rotating airfoil.

5. The apparatus of claim 4 wherein said mechanical-to-electromagnetic energy transformer is substantially compliant prior to affixing it to the component, said mechanical-to-electromagnetic energy transformer comprises a converter component having a shape that is sheet-like, and said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer.

6. The apparatus of claim 4 wherein the component has an integral retainer and said mechanical-to-electromagnetic energy transformer is located within said retainer, said mechanical-to-electromagnetic energy transformer comprises a plurality of converter component arranged in a stack, and said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer.

7. The apparatus of claim 4 wherein said electromagnetic circuit comprises an electrical circuit and said electromagnetic coupling of said mechanical-to-electromagnetic energy transformer and said electrical circuit comprises electrical coupling, said mechanical-to-electromagnetic energy transformer comprise a piezoelectric material, the component has a surface and said mechanical-to-electromagnetic energy transformer is affixed to said surface, and said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer when the component is subjected to high steady state stress.

8. The apparatus of claim 1 wherein said electromagnetic circuit comprises an electrical circuit and coupling of said mechanical-to-electromagnetic energy transformer and said electrical circuit comprises electrical coupling.

9. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer comprise a piezoelectric material.

10. The apparatus of claim 1 wherein said electromagnetic energy is dissipated electrically.

11. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer is compliant prior to affixing it to the component.

12. The apparatus of claim 1 wherein the component has a surface and said mechanical-to-electromagnetic energy transformer is affixed to said surface.

13. The apparatus of claim 12 wherein the turbomachine has a gas path and said mechanical-to-electromagnetic energy transformer is affixed to a location of said surface that is in said gas path.

14. The apparatus of claim 1 wherein the component is an airfoil having a shroud and said mechanical-to-electromagnetic energy transformer is affixed to said shroud.

15. The apparatus of claim 1 wherein the component has an integral retainer and said mechanical-to-electromagnetic energy transformer is located within said retainer.

16. The apparatus of claim 1 wherein the energy transformer comprises a retainer having ends affixed to the component and said retainer receives mechanical energy primarily through said ends.

17. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer comprises a converter component having a shape that is sheet-like.

18. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer comprises a plurality of converter component arranged in a stack.

19. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer comprises a viscoelastic material and receives mechanical energy from the component through said viscoelastic material.

20. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer.

21. The apparatus of claim 20 wherein said manner comprises applying a force to the component causing the component to bend, said mechanical-to-electromagnetic energy transformer is then affixed to the component, and said force is then removed.

22. The apparatus of claim 1 wherein said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer when the component is subjected to high steady state stress.

23. A method for passive damping of vibratory strain in a turbomachine component that experiences high steady state strain, the vibratory strain having associated with it mechanical energy, the method comprising:

providing a mechanical-to-electromagnetic energy transformer mechanically coupled to the component, said energy transformer receiving mechanical energy associated with the vibratory strain of the component and producing, from said mechanical energy, electromagnetic energy; and

providing an electromagnetic circuit electromagnetically coupled to said energy transformer, said circuit receiving electromagnetic energy, from said energy transformer, that is then dissipated through passive damping.

24. An apparatus for damping of vibratory strain in a turbomachine component that experiences high steady state strain, the component having a surface, the vibratory strain having associated with it mechanical energy, the apparatus comprising:

a mechanical-to-electromagnetic energy transformer mechanically coupled to the surface of the component, said energy transformer receiving mechanical energy associated with the vibratory strain of the component and producing, from said mechanical energy, electromagnetic energy; and

an electromagnetic circuit electromagnetically coupled to said energy transformer, said circuit receiving electromagnetic energy, from said energy transformer, that is then dissipated through passive damping.

25. The apparatus of claim 24 wherein the engine has a gas path and the component comprises an air management surface for the gas path.

26. The apparatus of claim 24 wherein the component is an airfoil.

27. The apparatus of claim 24 wherein the component is a rotating airfoil.

28. The apparatus of claim 27 wherein said mechanical-to-electromagnetic energy transformer is substantially compliant prior to affixing it to the component, said mechanical-to-electromagnetic energy transformer comprises a converter component having a shape that is sheet-like, and said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer.

29. The apparatus of claim 27 wherein the component has an integral retainer and said mechanical-to-electromagnetic energy transformer is located within said retainer, said mechanical-to-electromagnetic energy transformer comprises a plurality of converter component arranged in a stack, and said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer.

30. The apparatus of claim 27 wherein said electromagnetic circuit comprises an electrical circuit and said electromagnetic coupling of said mechanical-to-electromagnetic energy transformer and said electrical circuit comprises electrical coupling, said mechanical-to-electromagnetic energy transformer comprise a piezoelectric material, the component has a surface and said mechanical-to-electromagnetic energy transformer is affixed to said surface, and said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer when the component is subjected to high steady state stress.

31. The apparatus of claim 24 wherein said electromagnetic circuit comprises an electrical circuit and said electromagnetic coupling of said mechanical-to-electromagnetic energy transformer and said electrical circuit comprises electrical coupling.

32. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer comprise a piezoelectric material.

33. The apparatus of claim 24 wherein said electromagnetic energy is dissipated electrically.

34. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer is compliant prior to affixing it to the component.

35. The apparatus of claim 24 wherein the turbomachine has a gas path, said mechanical-to-electromagnetic energy transformer is affixed to a location of a surface of the component and said surface that is not in said gas path.

36. The apparatus of claim 24 wherein the component is an airfoil having a shroud and said mechanical-to-electromagnetic energy transformer is affixed to said shroud.

37. The apparatus of claim 24 wherein the component has an integral retainer and said mechanical-to-electromagnetic energy transformer is located within said retainer.

38. The apparatus of claim 24 wherein the energy transformer comprises a retainer having ends affixed to the component and said retainer receives mechanical energy primarily through said ends.

39. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer comprises a converter component having a shape that is sheet-like.

40. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer comprises a plurality of converter component arranged in a stack.

41. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer comprises a viscoelastic material and receives mechanical energy from the component through said viscoelastic material.

42. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer.

43. The apparatus of claim 40 wherein said manner comprises applying a force to the component causing the component to bend, said mechanical-to-electromagnetic energy transformer is then affixed to the component, and said force is then removed.

44. The apparatus of claim 24 wherein said mechanical-to-electromagnetic energy transformer is affixed to the component in such a manner as to provide compressive force to said energy transformer when the component is subjected to high steady state stress.

45. An method for damping of vibratory strain in a turbomachine component that experiences high steady state strain, the component having a surface, the vibratory strain having associated with it mechanical energy, the apparatus comprising:

providing a mechanical-to-electromagnetic energy transformer mechanically coupled to the surface of the component, said energy transformer receiving mechanical energy associated with the vibratory strain of the component and producing, from said mechanical energy, electromagnetic energy; and

providing an electromagnetic circuit electromagnetically coupled to said energy transformer, said circuit receiving electromagnetic energy, from said energy transformer, that is then dissipate through passive damping.