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Rotary adjustable exhaust nozzle 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
출원번호 US-0838623 (2004-05-04)
발명자 / 주소
  • Lair, Jean-Pierre
출원인 / 주소
  • The NORDAM Group, Inc.
인용정보 피인용 횟수 : 22  인용 특허 : 23

초록

An exhaust nozzle includes an exhaust duct with an outlet and a row of radial apertures upstream therefrom. A radial frame surrounds the duct upstream from the apertures. A row of flaps are hinged to the frame to selectively cover and uncover the apertures for controlling exhaust flow discharged the

대표청구항

1. A gas turbine engine exhaust nozzle comprising:an exhaust duct having an outlet at an aft end thereof for discharging exhaust flow, and including a row of radial apertures spaced upstream from said outlet;a radial frame extending circumferentially around said duct and spaced forward from said ape

이 특허에 인용된 특허 (23)

  1. Davies Stephen Harlow,GBX, Actuator.
  2. Lymons Dennis E. ; Aten Michael R., Actuator and safety lock system for pivoting door thrust reverser for aircraft jet engine.
  3. Lair, Jean-Pierre, Confluent variable exhaust nozzle.
  4. Newton Arnold C,GBX, Ducted fan gas turbine engine with variable area fan duct nozzle.
  5. Fournier Alain M.,FRX, Electro/hydraulic system for a 2 door thrust reverser.
  6. Gonidec Patrick,FRX ; Rouyer Pascal Gerard,FRX ; Vauchel Guy Bernard,FRX, Gas flow guide for an aircraft thrust reverser.
  7. Johnson, Andrew T.; Chakkera, Kevin K., Jet engine thrust reverser system having torque limited synchronization.
  8. Markstein David J. (Hamilton OH) Kemme Paul B. (West Chester OH), Lock for nozzle control in the event of hydraulic failure.
  9. Moe Jeffrey W. ; Cariola Roy E. ; Lymons Dennis E., Pivoting door type thrust reverser with deployable members for efflux control and flow separation.
  10. Standish Robert R.,FRX ; Fournier Alain,FRX, Sealing for a pivoting door reverser.
  11. Klees Garry W. (Mercer Island WA), Simplified method and apparatus for hot-shield jet noise suppression.
  12. Baudu Pierre Andre Marcel,FRX ; Gonidec Patrick,FRX ; Rouyer Pascal Gerard,FRX ; Vauchel Guy Bernard,FRX, Synchronizing control system for aircraft jet engine thrust reversers.
  13. Standish Robert R.,FRX, Thrust reverser for high bypass fan engine.
  14. Matta Ram K. (Loveland OH) Bhutiani Pupinder K. (Cincinnati OH), Thrust reverser for high bypass turbofan engine.
  15. Lair Jean-Pierre (8023 Vantage ; Suite 1450 San Antonio TX 78230), Thrust reverser integrating a variable exhaust area nozzle.
  16. Standish Robert R.,FRX ; Laboure Bernard,FRX, Thrust reverser with adjustable section nozzle for aircraft jet engine.
  17. Metezeau Emile Fabrice Henri,FRX ; Portal Marcel Jean-Fabrice,FRX, Thrust reverser with improved forward thrust efficiency.
  18. Butler Lawrence (Cincinnati OH), Thrust reverser with variable nozzle.
  19. Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX, Turbojet engine thrust reverser having hinged doors.
  20. Barbarin Jacques M. G. (Montivilliers FRX) Lecoutre Pascal B. G. (Le Havre FRX), Turbojet engine thrust reverser with variable exhaust cross-section.
  21. Lair Jean-Pierre (100 W. El Prado ; Suite 308 San Antonio TX 78212), Variable area exhaust nozzle.
  22. 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.
  23. Vdoviak John William (Marblehead MA) McHugh Donald Patrick (Cincinnati OH), Variable slot bypass injector system.

이 특허를 인용한 특허 (22)

  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. Hocking, Barry N, Adjustment assembly.
  4. Alhatim, Omair M., Exhaust nozzle of a gas turbine engine.
  5. Baran, Kenneth C., Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system.
  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. Suciu, Gabriel L.; Epstein, Alan H.; Lord, Wesley K.; Chandler, Jesse M.; Pixton, Stephen G., Gas turbine engine with embedded distributed fans.
  8. Do, Logan H.; Krystowski, Edward A., Gas turbine engine with variable area fan nozzle.
  9. Lair, Jean-Pierre, Pivoting door thrust reverser for a turbofan gas turbine engine.
  10. Lair,Jean Pierre, Spider actuated thrust reverser.
  11. Alhatim, Omair M., System of support thrust from wasted exhaust.
  12. Lair, Jean-Pierre, Thrust reverser.
  13. Lair, Jean-Pierre, Thrust reverser door.
  14. Lair, Jean-Pierre, Thrust reverser door.
  15. Lair, Jean-Pierre, Thrust reverser for a turbofan gas turbine engine.
  16. Lair, Jean-Pierre; Weaver, Paul, Thrust reverser for a turbofan gas turbine engine.
  17. Lair, Jean-Pierre, Thrust reverser nozzle for a turbofan gas turbine engine.
  18. Amkraut, Daniel M.; Layland, Michael John; James, Norman John, Translating variable area fan nozzle providing an upstream bypass flow exit.
  19. Amkraut, Daniel M.; Layland, Michael John; James, Norman John, Translating variable area fan nozzle providing an upstream bypass flow exit.
  20. Wang, Shunshen Richard, Translating variable area fan nozzle with split beavertail fairings.
  21. Kemper, Paul D.; Moniz, Thomas Ory; Seda, Jorge Francisco, Turbofan engine nozzle assembly and method of operating same.
  22. 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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