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Mounting arrangement for a gas turbine engine 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/20
  • B64C-001/16
출원번호 US-0036847 (1993-03-25)
우선권정보 GB-0008398 (1992-04-15)
발명자 / 주소
  • Carlin Robert N. (Nottingham GB2) Deighton Andrew W. (Derby GB2)
출원인 / 주소
  • Rolls-Royce plc (London GB2 03)
인용정보 피인용 횟수 : 43  인용 특허 : 0

초록

A nacelle of a gas turbine engine is attached via a pylon to an aircraft wing from which the engine is to be mounted. The nacelle is split to form a pair of opposing arcuate doors which are moveable between an open position and a closed position. When the doors are closed a ring on the fan casing lo

대표청구항

A mounting arrangement for a gas turbine engine comprising a nacelle surrounding the casing of a gas turbine engine, the nacelle being attached via a support member to an aircraft structure from which the engine is to be mounted, at least a part of the nacelle being split to form a pair of opposing

이 특허를 인용한 특허 (43)

  1. Crone James,CAX, Aircraft construction.
  2. Klamka Andrew ; Parham Dean Leon, Aircraft engine and associated aircraft engine cowl.
  3. Roche, Frederic; Martinou, Jean-Marc, Aircraft engine assembly comprising a fan cowl-supporting cradle mounted on two separate elements.
  4. Shutrump, Jeffrey D., Aircraft engine inlet having zone of deformation.
  5. Shutrump, Jeffrey D., Aircraft engine inlet having zone of deformation.
  6. Stretton,Richard G; Beardsley,Peter K; Beaven,David M, Aircraft engine mounting assembly.
  7. Sherry Philip David,GBX ; Welsh Robert,GBX ; Johnson Kenneth Henry,GBX, Aircraft propulsive power unit assembly having a leading edge lipskin and intake barrel.
  8. Mayes,Harold G, Closure panel arrangement.
  9. Porte Alain,FRX ; Lasserre Jean-Louis,FRX, Device for fixing an air intake to a jet engine and jet engine incorporating such a device.
  10. Marche, Herve, Device for mounting an aircraft turboprop engine comprising hydraulic attachments.
  11. El Hamel,Karim; Newton,Arnold C, Engine arrangement.
  12. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B., Engine mount system for a turbofan gas turbine engine.
  13. Suciu, Gabriel L.; Marx, Jon A.; Merry, Brian D.; Nordeen, Craig A.; Dye, Christopher M., Engine mounting configuration for a turbofan gas turbine engine.
  14. Eleftheriou, Andreas; Denis, David; Leclair, Denis; Roussel, Yves, Gas turbine engine case and method of making.
  15. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine compressor arrangement.
  16. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine compressor arrangement.
  17. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  18. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  19. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  20. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.; Schwarz, Frederick M., Gas turbine engine with low stage count low pressure turbine.
  21. Layland, Michael J.; James, Norman J.; Forsey, David; Soria, Christian, Hybrid hinge and latch beam.
  22. Marche, Jacques Hervé, Hydraulic system for transmission of forces between an aircraft turboprop and an attachment device.
  23. Williams,Nicholas A., Integrated mount duct for use with airborne auxiliary power units and other turbomachines.
  24. Bourdon, Gilles, Jet engine nacelle intended to equip an aircraft.
  25. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M., Mounting system for a gas turbine engine.
  26. Suciu, Gabriel L.; Merry, Brian D.; Franklin, David W. J.; Dye, Christopher M., Mounting system for a gas turbine engine.
  27. Suciu, Gabriel L.; Merry, Brian D.; Marx, Jon A.; Dye, Christopher M., Mounting system for a gas turbine engine.
  28. James, Norman John, Nacelle with longitudinal translating cowling and rotatable sleeves.
  29. Porte Alain,FRX, Opening device common to two adjacent aircraft engine nacelle covers.
  30. Garric, Stéphane; Vigneau, Philippe, Substitution device for aircraft engine.
  31. Soria, Christian; Chiou, Song; Layland, Michael J.; Hubert, Claude, Thrust reverser-integrated track beam and inner fixed structure.
  32. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M., Turbine section of high bypass turbofan.
  33. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  34. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph B.; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  35. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph Brent; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  36. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  37. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  38. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  39. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  40. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  41. Eleftheriou,Andreas; Lobo,Kevin Walter; Weinberg,Maurice; Liu,Quantai, Turbofan case and method of making.
  42. Derenes, Jacky Raphael Michel; Dijoud Lambert, Delphine; Nouhaud, Christophe Claude Philippe, Turbojet nacelle.
  43. Royer Wilson M. ; Gucker Mark J., Vent valve with pressure relief.
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