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Panel damped hybrid blade 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-011/16
출원번호 US-0997832 (1997-12-24)
발명자 / 주소
  • Schilling Jan C.
  • Cornell Jay L.
  • Stevenson Joseph T.
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Hess
인용정보 피인용 횟수 : 56  인용 특허 : 8

초록

A fan blade includes a metal airfoil having first and second opposite sides extending radially between a root and a tip, and axially between a leading edge and a trailing edge. The airfoil further includes a pocket disposed in the first side having an elastomeric filler bonded therein. A panel is bo

대표청구항

[ Accordingly, what is desired to be secured by Letters Patent of the United States is the invention as defined and differentiated in the following claims:] [1.] A gas turbine engine fan blade comprising;a metal airfoil having first and second opposite sides extending radially between a root and a t

이 특허에 인용된 특허 (8)

  1. Ellis ; Delmar H., Composite reinforcement of metallic airfoils.
  2. Finn Scott Roger ; Pandey Ravindra Kumar ; Fitzgerald John James ; Bachrach William Elliot, Gas turbine blade having areas of different densities.
  3. Schilling Jan Christopher (Middletown OH), Hybrid blade for a gas turbine.
  4. Wang Weiping ; Bachrach William Elliot ; Lin Wendy Wen-Ling ; Finn Scott Roger, Multi-component blade for a gas turbine.
  5. Howard Walter D. (Cincinnati OH) Ingling Theodore R. (Loveland OH) Bachrach William E. (Bennington VT), Partially-metallic blade for a gas turbine.
  6. El-Aini Yehia M. (Jupiter FL) Burge Joseph C. (Palm Beach Gardens FL) Meece Carl E. (Jupiter FL), Turbine engine rotor blade vibration damping device.
  7. Daguet Alain P. M. (Bondoufle FRX), Turbomachine flow-straightener blade.
  8. Murphy Guy C. (Fairfield OH) Fuhrmann Barrett J. (Cincinnati OH), Wide chord fan blade.

이 특허를 인용한 특허 (56)

  1. Charles R. Evans ; Douglas D. Ward ; Joseph T. Begovich, Jr. ; Wendy W. Lin ; Herbert S. Chao, Adhesion enhancers to promote bonds of improved strength between elastomers metals in lightweight aircraft fan blades.
  2. Evans, Dale E; Care, Ian C D, Aerofoil assembly.
  3. Goldfinch, Keith C.; Strother, Oliver M., Aerofoil sub-assembly, an aerofoil and a method of making an aerofoil.
  4. Reba, Ramons A.; Morin, Bruce L.; Morford, Stephen A.; Lord, Wesley K., Airfoil acoustic impedance control.
  5. Hui, Kwan; Weisse, Michael A., Airfoil cover system.
  6. Foster, Larry, Airfoil with an integrally stiffened composite cover.
  7. von Flotow, Andreas H., Apparatus for passive damping of flexural blade vibration in turbo-machinery.
  8. Deakin, Martin J.; Gent, John T.; Shipton, Mark H.; Shipton, legal representative, Joanne M., Article having a vibration damping coating and a method of applying a vibration damping coating to an article.
  9. Deakin,Martin J; Gent,John T; Shipton, legal representative,Joanne M; Shipton,Mark H, Article having a vibration damping coating and a method of applying a vibration damping coating to an article.
  10. Strother, Oliver M., Article with an internal structure.
  11. De Moura, Raul Fernando; Jean, Pierrick Bernard; Le Hong, Son; Lombard, Jean-Pierre Francois, Blade made of composite material comprising a damping device.
  12. Harrison, John M.; Goldfinch, Keith C., Bladed rotor balancing.
  13. Strother, Oliver Michael, Component structure.
  14. Goldfinch, Keith C.; Strother, Oliver M.; Mackechnie-Jarvis, Julian, Component with a damping filler.
  15. Goldfinch, Keith C.; Strother, Oliver M.; Mackechnie-Jarvis, Julian, Component with a damping filler and method.
  16. Goldfinch, Keith C.; Strother, Oliver M.; Mackechnie-Jarvis, Julian, Component with a damping filler and method.
  17. Vetters,Daniel K., Composite filled gas turbine engine blade with gas film damper.
  18. El-Aini, Yehia M.; Davis, Gary A., Damper for an integrally bladed rotor.
  19. El-Aini, Yehia M.; Davis, Gary A., Damper for an integrally bladed rotor.
  20. Evans Charles R. ; Ward Douglas D. ; Lin Wendy W. ; Chao Herbert S. ; Begovich ; Jr. Joseph T., Elastomeric formulation used in the construction of lightweight aircraft engine fan blades.
  21. McKaveney, Christopher S.; Murdock, James R., Fan blade channel termination.
  22. Hui, Kwan; Weisse, Michael A.; Foster, Larry, Fan blade composite cover with tapered edges.
  23. Rosenau, Knut, Fan blade for an aircraft engine.
  24. McKaveney, Christopher S.; Murdock, James R., Fan blade having internal rib break-edge.
  25. Anderson, Carney R.; Graves, William R., Gas turbine engine airfoil structure.
  26. Schwarz, Frederick M.; Suciu, Gabriel L., Geared turbine engine with relatively lightweight propulsor module.
  27. Hui, Kwan; Weisse, Michael A.; Lussier, Darin S.; Huttenhower, Hillary Anne, Hollow airfoil with composite cover and foam filler.
  28. Motherwell, Andrew, Hollow component with internal damping.
  29. Weisse, Michael A.; McKaveney, Christopher S., Hollow fan blade channel configuration to reduce stress.
  30. Murdock, James R., Hollow fan blade tuning using distinct filler materials.
  31. Read, Simon, Hollow turbine blade.
  32. Burdgick,Steven Sebastian, Hybrid bucket and related method of pocket design.
  33. Viens, Daniel V.; Nardone, Vincent C.; Smith, Peter G.; Strife, James R.; Lamm, Foster P., Hybrid structure airfoil.
  34. Schwarz, Frederick M.; Weisse, Michael A.; Zysman, Steven H., Lightweight shrouded fan blade.
  35. Goldfinch, Keith C.; Strother, Oliver M.; MacKechnie-Jarvis, Julian, Method of forming an aerofoil with a damping filler.
  36. Jones, Richard M.; Strother, Oliver M., Method of joining plates of material to form a structure.
  37. Strother, Oliver M., Method of manufacturing a component.
  38. Chivers, Nigel J.D.; Goldfinch, Keith C., Method of manufacturing a rotor for a gas turbine engine that includes identifying the frequency response of the rotor and adjusting the frequency response by providing a pressure gradient within the rotor.
  39. David William Crall, Methods and apparatus for damping rotor assembly vibrations.
  40. Burdgick, Steven S.; Lanaud, Christophe; Makinde, Adegboyega; Lin, Wendy, Methods and apparatus for mechanical retainment of non-metallic fillers in pockets.
  41. Burdgick,Steven Sebastian; DeLeonardo,Guy W.; Lin,Wendy W.; Barb,Kevin Joseph, Mixed tuned hybrid blade related method.
  42. Barb, Kevin Joseph, Mixed tuned hybrid bucket and related method.
  43. Pope, Andrew, Modal tuning for vanes.
  44. Hyatt, Thomas B.; Ganoe, Jr., William Richard, Retention of damping media.
  45. McCaffrey, Michael G., Root region of a blade for a gas turbine engine.
  46. Strother, Oliver M., Rotationally balancing a rotating part.
  47. Weisse, Michael A., Rotor blade with bonded cover.
  48. Weisse, Michael A., Rotor blade with bonded cover.
  49. Hyatt, Thomas B.; Klinetob, Carl Brian, Structural guide vane leading edge.
  50. Joseph Timothy Stevenson ; Wendy Wen-Ling Lin, Submerged rib hybrid blade.
  51. Campbell, Christian X.; Messmann, Stephen J, Turbine blade with tuned damping structure.
  52. Papin, Thierry Georges Paul; Lacroix, Lise; Raulin, Dominique, Turbine engine vane plate seal.
  53. Norris, Jennifer M; Knott, David S; Jones, Adrian M; Midgelow, David R; Hall, Robert M, Turbomachine blade.
  54. Lin, Wendy Wen-Ling; Finn, Scott Roger; Flanagan, Kevin Warner; Stevenson, Joseph Timothy; Carnahan, James Claude, Use of high modulus, impact resistant foams for structural components.
  55. Klinetob, Carl Brian; Ganoe, Jr., William Richard; Hyatt, Thomas B.; Leroux, Jason; Morgan, Douglas J., Vibration damping assembly and method of damping vibration in a gas turbine engine.
  56. Klinetob, Carl Brian; Lindahl, Stephen J.; Klein, Myron L.; Pope, Andrew; Ganoe, Jr., William Richard; Kasprow, Thomas D.; Morgan, Douglas J., Vibration damping for structural guide vanes.
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