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Thrust reverser blocker door assembly 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/06
출원번호 US-0459903 (1982-09-29)
국제출원번호 PCT/US82/01355 (1982-09-29)
§371/§102 date 19820929 (19820929)
국제공개번호 WO-8401344 (1984-04-12)
발명자 / 주소
  • Vermilye Michael L. (Redmond WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 39  인용 특허 : 3

초록

A thrust reverser blocker door assembly for a fanjet engine (34) wherein a plurality of blocker doors (10) are disposed aerodynamically about a peripheral circumferential zone of a central fan duct (46) of the engine in a cruise configuration and are pivoted radially into an annular ring interruptin

대표청구항

A thrust reverser blocker door assembly for a fanjet engine wherein a plurality of blocker doors are disposed aerodynamically about a peripheral circumferential zone of a central fan duct of the engine in a cruise configuration and are pivoted radially inward into an annular ring interrupting said f

이 특허에 인용된 특허 (3)

  1. Montgomery Ronald (Belfast IEX), Actuating mechanism for the thrust reversal doors of a gas turbine engine.
  2. Lardellier Alain Marie Joseph (Melun FR), Device for boosting and bleeding a gas turbine engine.
  3. Johnston Everett A. (Mason OH) Ryan Edward W. (Mason OH), Thrust reverser for a long duct fan engine.

이 특허를 인용한 특허 (39)

  1. Redding, Charles E.; Beimgraben, Herbert W.; Hartmann, Charles; Patterson, Douglas, Acoustic isolator for well logging system.
  2. Redding, Charles E.; Beimgraben, Herbert W.; Hartmann, Charles; Patterson, Douglas, Acoustic isolator for well logging system.
  3. Beardsley, Peter K; Knight, Glenn A, Aeroengine thrust reverser.
  4. Dubois Claude A. G. (Honfleur FRX) Gely Jean-Marie L. (Le Havre FRX) Vauchel Guy B. (Le Havre FRX), Air deflector for a turbofan engine thrust reverser.
  5. Marche, Jacques Herve, Aircraft nacelle which includes thrust reverser system and aircraft incorporating at least one such nacelle.
  6. Fournier Alain (Clamart FRX) Kennedy John F. (Walmer GBX), Aircraft power unit of the type with faired blower equipped with a thrust reverser wth doors.
  7. Vauchel, Guy Bernard; Segat, Peter, Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle.
  8. Glancy Jerry L. (Wichita KS), Automatic deflector for a jet engine bleed air exhaust system.
  9. Masters Abbott R. ; Garcia Ruben ; James Norman J., Blocker door frame pressure structure for translating cowl of cascade thrust reverser for aircraft jet engine.
  10. Zysman, Steven H.; Migliaro, Jr., Edward F., Bypass duct with angled drag links.
  11. Gormley, Timothy, Drag link assembly for a thrust reverser.
  12. Welch John M. ; Popp Thomas D. ; Wikstrom Robert F. ; Stratton Terry W. ; Kitt Brian R., Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring.
  13. Welch John M. ; Benton William E. ; Lobsinger Michael R., Engine nacelle outer cowl panel with integral track fairings.
  14. Cazuc, Xavier; Joret, Jean-Philippe, Front frame for a cascade thrust reverser structure.
  15. Gormley, Timothy, Linear actuator with multi-degree of freedom mounting structure.
  16. Sawyers-Abbott, Nigel David; Exner, Matthew, Link arm drag reducing device.
  17. Welch John M. ; Popp Thomas D. ; Baca Leonard L., Method for forming a composite acoustic panel.
  18. Howe, Mark E., Method of varying a fan duct nozzle throat area of a gas turbine engine.
  19. Metezeau, Fabrice; Valleroy, Laurent, Mobile thrust reverser cowl and thrust reverser provided with such a cowl.
  20. Andre, Robert; Letay, Benoit; Saget, Benjamin; Inghelbrecht, Eric, Nacelle for aircraft comprising means of reversing thrust and aircraft comprising at least one such nacelle.
  21. Howe, Mark E., Pivoting fan nozzle nacelle.
  22. Hercock, Henry, Plastic core blocker door.
  23. Welch John M. ; Popp Thomas D. ; Wikstrom Robert F. ; Stratton Terry W. ; Kitt Brian R., Reinforcing structure for engine nacelle acoustic panel.
  24. Bean,Jason A.; Nakamura,Koichi, Splicing tape with separating portions.
  25. Allen, Damian, Spoiler deployment mechanism.
  26. Hogie, Jean-Paul, Spring for a cascade-type thrust reverser shutter for an aircraft jet engine.
  27. Bellanger, Alexandre; Dubois, Laurent; Bouillon, Florent; Bardin, Stephane, Stub frame for a cascade thrust reverser structure.
  28. Foutch, David W., Thrust reverser apparatus and method.
  29. Murphy, Michael Joseph, Thrust reverser assembly with shaped drag links.
  30. Aten, Michael Ray; Crawford, Sara Christine, Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion.
  31. Aten, Michael Ray; Crawford, Sara Christine, Thrust reverser cascade assembly with flow deflection shelf.
  32. Stuart, Alan Roy; Cosgrove, James Michael, Thrust reverser system with translating-rotating blocker doors and method of operation.
  33. Teia Dos Santos Mendes Gomes, Luis Daniel, Thrust reverser unit having both nested cascades translating linearly and only one cascade rotational.
  34. Gormley, Timothy, Thrust reverser with hidden linkage blocker doors.
  35. Stern, Alfred M., Thrust reversing variable area nozzle.
  36. Stern, Alfred M., Thrust reversing variable area nozzle.
  37. Gormley, Timothy, Translating cascade hidden blocker door thrust reverser.
  38. Schwark, Jr., Fred W.; Atassi, Oliver V.; Owen, William D., Variable area fan nozzle bearing track.
  39. Papa, Federico; Vivar, Pilar Del Carmen, Ventilation system using thrust reverser linkages.
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