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Variable cross-section turbofan exhaust duct with door type thrust reverser for aircraft 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-001/09
  • F02C-003/02
출원번호 US-0096525 (1998-06-12)
우선권정보 FR-0007278 (1997-06-12)
발명자 / 주소
  • Gonidec Patrick,FRX
  • Guy Bernard Vauchel,FRX
출원인 / 주소
  • Societe Hispano Suiza Aerostructures, FRX
대리인 / 주소
    Bacon & Thomas, PLLC
인용정보 피인용 횟수 : 34  인용 특허 : 4

초록

A variable turbofan bypass cowling includes a movable cowling assembly (12) with pivoting door type thrust reversers (20) connected to a fixed upstream cowling structure (11). The movable assembly may be translated between an upstream position whereat an upstream portion of the reverser and cowling

대표청구항

[ We claim:] [1.] A variable fan exhaust duct and thrust reverser arrangement for a turbofan-type aircraft engine comprising:a fan and engine outer cowling including pivoted thrust reverser doors, said cowling defining, with an outer surface of an inner primary engine cowling, a fan exhaust duct, sa

이 특허에 인용된 특허 (4)

  1. Prior Barry W. (San Diego CA) Halkola John T. (La Jolla CA), Fan cascade thrust reverser.
  2. Newton Arnold C. (Derby GB2), Thrust reverser.
  3. Standish Robert R.,FRX ; Laboure Bernard,FRX, Thrust reverser with adjustable section nozzle for aircraft jet engine.
  4. Duesler Paul W. ; Loffredo Constantino V. ; Prosser ; Jr. Harold T. ; Jones Christopher W., Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems.

이 특허를 인용한 특허 (34)

  1. Ramlaoui, Jihad I.; Pinto, Geoffrey; Shetzer, Daniel; Amkraut, Daniel M.; Hawksworth, Andrew Robert; Harvey, John; Evans, Alan K.; Chandarana, Vikram; Moorhouse, Roger, Actuation system for a translating variable area fan nozzle.
  2. Ramlaoui, Jihad I.; Pinto, Geoffrey; Shetzer, Daniel; Amkraut, Daniel M.; Hawksworth, Andrew Robert; Harvey, John; Evans, Alan K.; Chandarana, Vikram; Moorhouse, Roger, Actuation system for a translating variable area fan nozzle.
  3. Vauchel, Guy; Joret, Jean-Philippe; Baudu, Pierre; Guenadou, Christophe, Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator.
  4. Baker, Von David, Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle.
  5. James, Norman J., Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle.
  6. Chanez, Philippe Gerard; Zeggai, Kamel, Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl.
  7. Langston, Todd A.; Johnson, Andrew T.; Ahrendt, Terry J., Gearless electric thrust reverser actuators and actuation system incorporating same.
  8. Ramlaoui, Jihad I.; Roberts, Stephen Michael; Forsey, David, Guide system for nacelle assembly.
  9. Roberts, Stephen Michael, Guide system for nacelle assembly.
  10. Ahrendt, Terry, Method for controlling the deployment of jet engine thrust reversers.
  11. Lair, Jean-Pierre, Pivoting door thrust reverser for a turbofan gas turbine engine.
  12. Ahrendt, Terry, System and method for controlling the deployment of jet engine thrust reversers.
  13. Ahrendt, Terry J.; Johnson, Andrew T.; Chakkera, Kevin K., System and method for controlling the movement of an aircraft engine cowl door.
  14. Ahrendt, Terry, System and method for controlling the stowage of jet engine thrust reversers.
  15. Terry J. Ahrendt, System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system.
  16. Dehu, Michel Philippe; Lesbos, Damien Benoit Marie; Vauchel, Guy Bernard, System driving the displaceable fairing of a turbojet-engine thrust reverser.
  17. Lair, Jean-Pierre, Thrust reverser.
  18. Lair, Jean-Pierre, Thrust reverser door.
  19. Lair, Jean-Pierre, Thrust reverser door.
  20. Lair, Jean-Pierre, Thrust reverser for a turbofan gas turbine engine.
  21. Lair, Jean-Pierre, Thrust reverser nozzle for a turbofan gas turbine engine.
  22. Johnson, Andrew T., Thrust reverser position determination system and method.
  23. Amkraut, Daniel M.; Layland, Michael John; James, Norman John, Translating variable area fan nozzle providing an upstream bypass flow exit.
  24. Amkraut, Daniel M.; Layland, Michael John; James, Norman John, Translating variable area fan nozzle providing an upstream bypass flow exit.
  25. Wang, Shunshen Richard, Translating variable area fan nozzle with split beavertail fairings.
  26. Orlando, Robert Joseph; Moniz, Thomas Ory; Seda, Jorge Francisco, Turbofan engine cowl assembly and method of operating the same.
  27. Kemper, Paul D.; Moniz, Thomas Ory; Seda, Jorge Francisco, Turbofan engine nozzle assembly and method for operating the same.
  28. Kemper, Paul D.; Moniz, Thomas Ory; Seda, Jorge Francisco, Turbofan engine nozzle assembly and method of operating same.
  29. Gukeisen, Robert L.; Mercier, Claude; Malecki, Robert E., Turbomachine thrust reverser.
  30. Pero, Edward B.; Aceto, Leonard D., Variable area fan nozzle and thrust reverser.
  31. Pero, Edward B.; Aceto, Leonard D., Variable area fan nozzle and thrust reverser.
  32. Pero, Edward B.; Aceto, Leonard D., Variable area fan nozzle and thrust reverser.
  33. Chakkera, Kevin K.; Vaughan, Ron, Variable area fan nozzle systems with improved drive couplings.
  34. Frank, Joel Hudson; James, Norman John; Wang, Shunshen Richard; McKleny, Bryant Lynoel; Baer, David A.; Jones, Tony; Harvey, John H.; Bacon, Peter W.; Hubberstey, Mark; Wharton, Brett J.; Davies, Neil C.; Roberts, Stephen Michael; Wylie, Steven Andrew, Variable area fan nozzle with bypass flow.
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