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특허 상세정보

ATR axial V-groove

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-025/24    B64D-029/06    F01D-025/28    F01D-009/02   
출원번호 US-0187038 (2014-02-21)
등록번호 US-9611048 (2017-04-04)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 47
초록

A gas turbine engine nacelle includes a first annular portion that is stationary and adapted for partially surrounding an engine core. The first annular portion includes a fore pylon connecting portion. A rail is coupled to the fore pylon connecting portion and extends in the aft direction from the first annular portion. A second annular portion is positioned aft of the first portion and coupled to the rail. The second portion is movable along an engine core centerline between a closed position and at least one open position. The second annular portion i...

대표
청구항

1. A gas turbine engine nacelle comprising: a first annular portion that is stationary and adapted for partially surrounding an engine core, the first annular portion including a fore pylon connecting portion;a rail coupled to the fore pylon connecting portion and extending in the aft direction from the first annular portion;a second annular portion, aft of the first portion and coupled to the rail, the second portion being movable along an engine core centerline between a closed position and at least one open position, wherein the second annular portion...

이 특허에 인용된 특허 (47)

  1. Dunbar Donald K. (Sharonville OH) Delaney Bobby R. (Loveland OH). Aircraft bypass turbofan engine thrust reverser. USP1994055315821.
  2. McDonough, Michael Patrick; Brown, Keith Towers; Gilzean, Scott. Aircraft engine nacelle with translating inlet cowl. USP2012058181905.
  3. Marche, Herve. Aircraft pod and aircraft equipped with at least one such pod. USP2010087784735.
  4. Cole Derek (Bangor IEX) Sherry Philip D. (Larne IEX) Blair Alan J. (Holywood IEX). Aircraft propulsive power unit. USP1997035609313.
  5. Sherry Philip David,GBX ; Welsh Robert,GBX ; Johnson Kenneth Henry,GBX. Aircraft propulsive power unit assembly having a leading edge lipskin and intake barrel. USP1999085941061.
  6. Lair,Jean Pierre. Cascade reverser without blocker doors. USP2009027484356.
  7. Ramlaoui, Jihad I.; Seaver, Randall J.; James, Norman J.; Byrne, Stuart J.; Cornejo, Sheila. Cascadeless fan thrust reverser with plume control. USP2005116968675.
  8. Jannetta, Thomas J.; Peters, Frederick H.. Converging nozzle thrust reverser. USP2003056568172.
  9. Lair, Jean-Pierre. Duplex mixer exhaust nozzle. USP2004096786038.
  10. Journade, Frederic; Lafont, Laurent. Engine assembly for aircraft with sliding nacelle. USP2012078226027.
  11. Salice Luciano (Carimate ITX). Fastening element. USP1997075642960.
  12. Newton Arnold C. (Derby GB2). Gas turbine engine nacelle assembly. USP1996035497961.
  13. Legrand Paul J. (Vaux le Penil FRX) Hersen RenM. J. (Combs la Ville FRX). Guidance device for the moving fairing of a thrust reverser system. USP1984044442987.
  14. Beaufort, Jacques. Hinge device of a nacelle cowling of an aircraft engine on a supporting structure. USP2011067959107.
  15. Lair,Jean Pierre; Wolters,Gregory Thomas. Induction coupled variable nozzle. USP2006107127880.
  16. Guibert, Thibaud Jean-Baptiste; Lefort, Guillaume; Tesniere, Marc Patrick. Integrated propulsive system comprising a bypass turbojet engine. USP2011067959106.
  17. Wang Jwomin,TWX ; Lin Nick,TWX ; Yu Justin,TWX. Land grid package connector. USP2001106296495.
  18. Ichikawa, Kenji; Kasahara, Seiji. Mold, method for producing the same and magnetic recording medium. USP2010087784765.
  19. Lore Xavier R. Y. (Beuzeville la Grenier FRX). Multi-panel thrust reverser door. USP1991085039171.
  20. Calder, David P.; Howarth, Graham F.. Nacelle and method of assembling the same. USP2012078220738.
  21. Dubois Claude A. G. (Honfleur FRX). Pivoting door cascade thrust reverser. USP1992025090197.
  22. Cariola Roy E. (San Diego CA) Grace Thadeus N. (Chula Vista CA). Pivoting door thrust reverser. USP1992065117630.
  23. Lair, Jean-Pierre. Pivoting door thrust reverser for a turbofan gas turbine engine. USP2012058172175.
  24. Lardy Pascal,FRX ; Valleroy Laurent Georges,FRX. Pivoting door thrust reverser with sliding panel. USP1999105970704.
  25. Jean Michel Christian Marie,FRX. Self-closing pivoting door thrust reverser. USP2000066079201.
  26. Webb George (Cincinnati OH). Single pivot overwing thrust reverser. USP1992055110069.
  27. Sternberger, Joe E.. System for adjustment of thrust reverser pivot door. USP2011088002217.
  28. Fournier Alain M. (Clamart FRX) Kennedy John F. (Boulogne FRX). Thrust reversal device for air-craft turbojets. USP1984124485970.
  29. Lair, Jean-Pierre. Thrust reverser door. USP2012018091827.
  30. Kennedy John F. (Boulogne FRX) Fournier Alain (Clamart FRX). Thrust reverser for a jet engine, more especially for equipping an aircraft. USP1983104410152.
  31. Johnston Everett A. (Mason OH) Ryan Edward W. (Mason OH). Thrust reverser for a long duct fan engine. USP1981074278220.
  32. Bunel Serge P. (Le Havre FRX) Dubois Claude A. G. (Saint Pair FRX). Thrust reverser for a turbofan engine. USP1993125267438.
  33. Lair, Jean-Pierre. Thrust reverser for a turbofan gas turbine engine. USP2011118052085.
  34. Dubois Claude A. G. (Honfleur FRX) Lore Xavier R. Y. (Le Havre FRX). Thrust reverser for a turbojet engine. USP1990104960243.
  35. Standish Robert R.,FRX. Thrust reverser for high bypass fan engine. USP1999015863014.
  36. Lair, Jean-Pierre. Thrust reverser nozzle for a turbofan gas turbine engine. USP2011098015797.
  37. Dubois Claude A. G. (Honfleur FRX) Lore Xavier R. Y. (Le Havre FRX). Thrust reverser with movable deflector. USP1990014894985.
  38. Brian E. Barton. Translating independently mounted air inlet system for aircraft turbofan jet engine. USP2002016340135.
  39. Porte Alain,FRX. Turbofan with thrust reversal doors not submitted to bypass air in their inactive position. USP1998035722231.
  40. Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser door spoilers with motion controlling drive system. USP2000116151884.
  41. Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser having movable rear baffle pivattally connected by forward and rear linkrods which are. USP1999115974783.
  42. Canadas Marc,FRX. Turbojet pod with laminar flow. USP2001016179249.
  43. Gonidec Patrick,FRX ; Rouyer Pascal Gerard,FRX ; Vauchel Guy Bernard,FRX. Turbojet thrust reverser with downstream obstacles. USP2001016170255.
  44. Pero, Edward B.; Aceto, Leonard D.. Variable area fan nozzle and thrust reverser. USP2013048418436.
  45. Lair, Jean-Pierre. Variable area thrust reverser nozzle. USP2004026688099.
  46. James Varnell L. (Kent WA). Variable geometry convergent divergent exhaust nozzle. USP1980044196856.
  47. Bubello Robert (Meriden CT) Ream Jeffrey L. (Tollano CT). Ventilation system for a nacelle. USP1989054825644.