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특허 상세정보

Aircraft provided with thrust reversers

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02    F02K-003/00   
미국특허분류(USC) 060/226.2; 060/224; 244/075.R
출원번호 US-0932342 (2004-09-02)
우선권정보 FR-03 10417(2003-09-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Stevens, Davis, Miller &
인용정보 피인용 횟수 : 1  인용 특허 : 24
초록

Some but not all engines of an aircraft are provided with thrust reversers. A safety device disables, at least from the position corresponding to idling, the action of the throttles corresponding to the engines devoid of thrust reversers when the thrust reversers are controlled to deployment.

대표
청구항

The invention claimed is: 1. An aircraft provided with a plurality of engines whose speeds are controlled individually, between idling and full speed, by throttles respectively associated with said engines, wherein: certain of said engines of said plurality are equipped with thrust reversers that are operable to be controlled so as to be able to go from an inactive retracted position to an active deployed position and, conversely, from said active deployed position to said inactive retracted position; other engines of said plurality are devoid of thrust...

이 특허에 인용된 특허 (24)

  1. O\Brien Michael T. (Cincinnati OH) Bobo ; deceased Melvin (late of Cincinnati OH by Beatrice L. Bobo ; executor). Aircraft gas turbine engine sideways mount. USP1995085443229.
  2. Albero, Jose; Bruno, Louis J.; Dussault, Richard; Lents, Charles E.; Thresher, Wayne A.; Sahm, Michael K.; Thompson, Robert G.. Aircraft system architecture. USP2003106634596.
  3. Lawson Dale W. R. (Bonita CA). Aircraft turbine engine thrust reverser. USP1993075230213.
  4. Presz ; Jr. Walter M. ; Reynolds Gary. Contoured thrust reverser and lobed nozzle noise suppressor for gas turbine engines. USP2001056233920.
  5. Howe, Mark E.; Loss, Kevin L.; Sheahan, B. Kelly. Flammable fluid line shroud. USP2004106802479.
  6. Standish Robert R. (Gazeran FRX). Forward mounted pivoting door reverser with efflux control device. USP1997095671598.
  7. Marx Alan D. (Seattle WA) Renzelmann Michael E. (Woodinville WA) Smith Mark H. (Vashon Island WA). Hydraulic actuator with mechanical lock and installation. USP1995015379969.
  8. Archung Ralph (Issaquah WA). Hydraulic power supplies. USP1992035100082.
  9. Dacosta John,KNX. Inflight aircraft visual monitoring apparatus. USP2001076264135.
  10. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  11. Presz ; Jr. Walter M. ; Butler Maurice C. ; Anderson Jack H.. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor. USP2001116311928.
  12. Baudu Pierre Andre Marcel,FRX ; Gonidec Patrick,FRX ; Rouyer Pascal Gerard,FRX ; Vauchel Guy Bernard,FRX. Locking system for an aircraft jet engine thrust reverser door including a plurality of locking devices arranged to prevent deformation of the thrust reverser door. USP2000046044641.
  13. Van De Kreeke, Marc; Cassein, Guillaume. Method and system for controlling an aircraft control surface. USP2005036863242.
  14. Mathieu Gerard,FRX. Method for controlling an aeroplane control surfaces to counter ground lateral drift. USP2001066241183.
  15. Dun, Roy. Methods and apparatuses for controlling airflow proximate to engine/airfoil systems. USP2005126978971.
  16. Finch Thomas (San Antonio TX). Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies. USP1982014311289.
  17. Moss William Gregory (Centerville OH) Roberts Kenneth Dale (Xenia OH) Briggs Charles Whitford (Waynesville OH). Pod mounted refueling system. USP1997095667170.
  18. Rivron Vincent (Toulouse FRX) Vollard Ccile (Toulouse FRX). Process for the control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviatio. USP1994125375793.
  19. Rudolph Peter K. C. (Seattle WA). Supersonic airplane with subsonic boost engine means and method of operating the same. USP1996065529263.
  20. 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. USP2000086094908.
  21. Wagenfeld Robert E. (New York NY). System for reducing aircraft noise and hush kit. USP1989064836469.
  22. Rouyer, Pascal Gerard; Gonidec, Patrick. System for the synchronized locking of the doors of a thrust reverser. USP2003096622964.
  23. Lair, Jean-Pierre. Toggle interlocked thrust reverser. USP2005126976352.
  24. Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser door spoilers with motion controlling drive system. USP2000116151884.