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Turbomachine blade 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F01D-005/10
출원번호 US-0020315 (2001-12-18)
우선권정보 GB-20010000695 (2001-01-11)
발명자 / 주소
  • Norris, Jennifer M
  • Knott, David S
  • Jones, Adrian M
  • Midgelow, David R
  • Hall, Robert M
출원인 / 주소
  • Rolls-Royce plc
대리인 / 주소
    Taltavull, W. WarrenManelli, Denison & Selter PLLC
인용정보 피인용 횟수 : 56  인용 특허 : 6

초록

A gas turbine engine fan blade (26) comprises a root portion (40) and an aerofoil portion (42). The aerofoil portion (42) has a leading edge (44), a trailing edge (46), a concave metal wall portion (50) extending from the leading edge (44) to the trailing edge (46) and a convex metal wall portion (5

대표청구항

A gas turbine engine fan blade (26) comprises a root portion (40) and an aerofoil portion (42). The aerofoil portion (42) has a leading edge (44), a trailing edge (46), a concave metal wall portion (50) extending from the leading edge (44) to the trailing edge (46) and a convex metal wall portion (5

이 특허에 인용된 특허 (6)

  1. Stoker Eric ; Pollitt Stan ; Morris Terry ; Chen Bob ; Doshi Ramish, Damped blade having a single coating of vibration-damping material.
  2. Mercer Gary D. (Palm Beach FL) Hildebrand Kurt T. (Mariemont OH), Damper assembly for a strut in a jet propulsion engine.
  3. Ress ; Jr. Robert Anthony ; Ewing Bruce Allan ; King Brian Paul, High stiffness airoil and method of manufacture.
  4. Calle Gilles Michel Georges Louis,FRX ; Klein Gilles Charles,FRX, Method of manufacturing a hollow blade for a turbomachine.
  5. Schilling Jan C. ; Cornell Jay L. ; Stevenson Joseph T., Panel damped hybrid blade.
  6. Panovsky Josef ; Stevenson Joseph T., Striated hybrid blade.

이 특허를 인용한 특허 (56)

  1. El-Wardany, Tahany Ibrahim; Smith, Peter G.; Reynolds, Warren; Ng, Eugene; Adams, Kay V., Abrasive waterjet machining and method to manufacture a curved rotor blade retention slot.
  2. Christofi, Costas; Hoang, Quynh; Gupta, Sanjay; Lemon, Angus; Vershaw, James T.; Nalla, Nandagopal; Abi-Habib, Emile, Acoustical vibration dampener for a rotatable blade.
  3. Read, Simon, Aerofoil and a method of manufacturing an aerofoil.
  4. Goldfinch, Keith C.; Strother, Oliver M., Aerofoil sub-assembly, an aerofoil and a method of making an aerofoil.
  5. Xu, JinQuan, Airfoil cooling enhancement and method of making the same.
  6. Propheter-Hinckley, Tracy A.; Loureiro, Sergio M.; Klucha, Agnes; Fisk, Benjamin T.; Tracy, Anita L., Airfoil having internal lattice network.
  7. Propheter-Hinckley, Tracy A.; Fisk, Benjamin T.; Taffet, Steven; Dolansky, Gregory M.; Tracy, Anita L., Airfoil having minimum distance ribs.
  8. Dolansky, Gregory M.; Fisk, Benjamin T.; Propheter-Hinckley, Tracy A.; Tracy, Anita L., Airfoil having tapered buttress.
  9. Dolansky, Gregory M.; Propheter-Hinckley, Tracy A.; Fisk, Benjamin T., Airfoil including damper member.
  10. Houston, David P.; Propheter-Hinckley, Tracy A.; Fisk, Benjamin T.; Tracy, Anita L., Airfoil including loose damper.
  11. Houston, David P.; Propheter-Hinckley, Tracy A.; Fisk, Benjamin T.; Tracy, Anita L., Airfoil including loose damper.
  12. Propheter-Hinckley, Tracy A.; Tracy, Anita L., Airfoil including member connected by articulated joint.
  13. O'Hearn, Jason L.; Aggarwala, Andrew S., Airfoil leading edge shape tailoring to reduce heat load.
  14. Propheter-Hinckley, Tracy A.; Houston, David P.; Tracy, Anita L., Airfoil support method and apparatus.
  15. Fisk, Benjamin T.; Propheter-Hinckley, Tracy A.; Dolansky, Gregory M.; Houston, David P.; Tracy, Anita L., Airfoil with break-way, free-floating damper member.
  16. Propheter-Hinckley, Tracy A.; Dolansky, Gregory M.; Fisk, Benjamin T.; Treen, Robert J., Airfoil with powder damper.
  17. Fisk, Benjamin T.; Propheter-Hinckley, Tracy A., Airfoils having porous abradable elements.
  18. Read, Simon; McMillan, Alison J.; Ravey, Eric, Apparatus for preventing ice accretion.
  19. Read, Simon; McMillan, Alison J; Ravey, Eric, Apparatus for preventing ice accretion.
  20. Strother, Oliver M., Article with an internal structure.
  21. McMillan,Alison J.; Read,Simon, Blade.
  22. Fisk, Benjamin T.; Propheter-Hinckley, Tracy A., Blade having porous, abradable element.
  23. Strother, Oliver Michael, Component structure.
  24. Goldfinch, Keith C.; Strother, Oliver M.; Mackechnie-Jarvis, Julian, Component with a damping filler.
  25. Goldfinch, Keith C.; Strother, Oliver M.; Mackechnie-Jarvis, Julian, Component with a damping filler and method.
  26. Goldfinch, Keith C.; Strother, Oliver M.; Mackechnie-Jarvis, Julian, Component with a damping filler and method.
  27. Powell,Christopher A., Component with internal damping.
  28. Cahill, Kevin; Strauss, Eric; Burchett, Doug; Didandeh, Hooshang; Shogren, Charles Mark, Composite fan.
  29. Vetters,Daniel K., Composite filled gas turbine engine blade with gas film damper.
  30. Schreiber, Karl, Fan blade for a gas-turbine engine.
  31. Propheter-Hinckley, Tracy A.; Zelesky, Mark F.; Mongillo, Jr., Dominic J.; Devore, Matthew A.; Gautschi, Steven Bruce; Fisk, Benjamin T., Gas turbine engine airfoil impingement cooling.
  32. Hui, Kwan; Weisse, Michael A.; Lussier, Darin S.; Huttenhower, Hillary Anne, Hollow airfoil with composite cover and foam filler.
  33. Motherwell, Andrew, Hollow component with internal damping.
  34. Eilert,Theodore J.; Harkins,Henry D.; Kornfeld,Roger E.; Breer,Marlin D., Method and apparatus for forming complex contour structural assemblies.
  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. Bray,Simon E; Throssell,Jonathan P, Method of making aerofoil blisks.
  38. Andrews, Ian J.; Rugg, David; Wallis, Michael J., Method of making and joining an aerofoil and root.
  39. Strother, Oliver M., Method of manufacturing a component.
  40. 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.
  41. Schilling,Jan Christopher, Methods and apparatus for gas turbine engines.
  42. Eilert, Theodore J.; Harkins, Henry D.; Kornfeld, Roger E.; Breer, Marlin D., Preform for forming complex contour structural assemblies.
  43. Halley, Jeremiah E.; Slattery, Kevin T., Preforms for forming machined structural assemblies.
  44. Hyatt, Thomas B.; Ganoe, Jr., William Richard, Retention of damping media.
  45. Strother, Oliver M., Rotationally balancing a rotating part.
  46. Weisse, Michael A., Rotor blade with bonded cover.
  47. Weisse, Michael A., Rotor blade with bonded cover.
  48. Christofi, Costas; Hoang, Quynh; Gupta, Sanjay; Lemon, Angus; Vershaw, James T.; Nalla, Nandagopal; Abi-Habib, Emile, Structural and acoustical vibration dampener for a rotatable blade.
  49. Slattery, Kevin T.; Young, Keith A., Structural assemblies and preforms therefor formed by friction welding.
  50. Slattery, Kevin T., Structural assemblies and preforms therefor formed by linear friction welding.
  51. Slattery,Kevin T., Structural assemblies and preforms therefor formed by linear friction welding.
  52. Sjogren,John F.; Eilert,Theodore J.; Harkins,Henry D., System and method for processing a preform vacuum vessel to produce a structural assembly.
  53. Clark, Daniel; Harvey, Richard C; Rongong, Jem A, Turbomachine blade.
  54. Rongong,Jem A; Tomlinson,Geoffrey R, Turbomachine blade.
  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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