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Integrated gas turbine engine-nacelle 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/20
  • F02K-003/04
출원번호 US-0628221 (1975-11-03)
발명자 / 주소
  • Adamson Arthur P. (Cincinnati OH) Sargisson Donald F. (Cincinnati OH) Stotler
  • Jr. Charles L. (Fairfield OH)
출원인 / 주소
  • The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (Washington DC 06)
인용정보 피인용 횟수 : 41  인용 특허 : 0

초록

A nacelle for use with a gas turbine engine is provided with an integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine. The nacelle is entirely supported in its spacial relationship with the engine by means of the webbed structure. The inner surface of

대표청구항

An integrated propulsion system comprising: a pylon; a gas turbofan engine including a core engine for rotatably driving a fan stage to pressurize a motive fluid, a fan bypass flow annulus generally circumscribing said core engine, a core engine inlet duct communicating with said bypass duct, a flow

이 특허를 인용한 특허 (41)

  1. Thies, Robert; Buchholz, Carsten; Staudte, Andreas, Accessory mounting for a gas turbine.
  2. Beier, Jürgen, Accessory mounting for a gas turbine engine.
  3. Marche, Jacques Herve; Raison, Fabien, Aircraft engine attachment pylon comprising a box with a circular or elliptical shaped section.
  4. Dunstan Kent W., Aircraft engine thrust mount.
  5. Hey Kenneth E., Aircraft engine thrust mount.
  6. Stretton,Richard G; Moore,Alastair D, Aircraft wing and aeroengine arrangement for attenuating engine noise.
  7. Stewart, David Mark, Apparatus for attachment of wing panels.
  8. Okapuu lo (309 Place Valencay St. Lambert ; Quebec CAX J4S 1S3) Patel Kiritkumar V. (4176 Trellis Crescent Mississauga ; Ontari CAX L5L 2M2), Circumferentially grooved shroud liner.
  9. Murphy Patrick (Bellevue WA) Roundy Bertan J. (Bellevue WA) Wood Stuart K. (Seattle WA), Collapsible cowl structure for gas-turbine engine strut.
  10. Garcia Alain (Aussonne FRX) Tchavdarov Jean-Claude (Castelmaurou FRX) Porte Alain (Colomiers FRX), Ducted fan turbine engine.
  11. Chee Wan T. (Bellevue WA), Engine mounting assembly.
  12. Hey Kenneth E. (Seattle WA), Fail-safe engine mount system.
  13. Lenk, Olaf, Flow divider having breaking points for a fan engine.
  14. Eleftheriou, Andreas; Denis, David; Leclair, Denis; Roussel, Yves, Gas turbine engine case and method of making.
  15. Winter, Michael, Gas turbine engine with pylon mounted accessory drive.
  16. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  17. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A., Isentropic compression inlet for supersonic aircraft.
  18. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  19. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  20. Conners, Timothy R., Low shock strength inlet.
  21. Conners, Timothy R., Low shock strength inlet.
  22. Conners, Timothy R., Low shock strength propulsion system.
  23. Conners, Timothy R., Low shock strength propulsion system.
  24. Conners, Timothy R., Low shock strength propulsion system.
  25. Alain Porte FR; Robert Andre FR, Method for making a composite panel and resulting panel.
  26. MacGee Andrew (Cincinnati OH), Sliding duct seal.
  27. Naud Henry (Verrieres Le Buisson FRX), Structural cowlings of twin flow turbo jet engines.
  28. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Supersonic aircraft jet engine installation.
  29. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L., Supersonic aircraft with spike for controlling and reducing sonic boom.
  30. Anderson, William Carl, Systems and methods for designing threads of turbine engine connectors.
  31. Dunstan Kent W. ; Hey Kenneth E., Three link failsafe engine mount.
  32. Hey Kenneth E. (Seattle WA), Three link failsafe engine mount.
  33. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  34. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  35. Eleftheriou, Andreas; Lobo, Kevin Walter; Weinberg, Maurice; Liu, Quantai, Turbofan case and method of making.
  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. Adamson Arthur P. (Cincinnati OH), Turbofan engine having a split cowl.
  40. Brown, Dewain Ray, Turbofan jet engine.
  41. Lardellier Alain M. J. (Melun FRX), Wing mounting nacelle for a very high by-pass ratio turbojet aero-engine.
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