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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Pivot thrust reverser surrounding inner surface of bypass duct

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/72    B64D-029/00    F02K-001/60    F02K-001/62    F02K-001/64    B23P-019/04    F02K-001/76   
출원번호 US-0184313 (2014-02-19)
등록번호 US-9631578 (2017-04-25)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kinney & Lange, P.A.
인용정보 피인용 횟수 : 0  인용 특허 : 51
초록
▼

A pivot thrust reverser includes a first pivot door forming a first portion of a nacelle when stowed and second pivot door forming a second portion of the nacelle when stowed. The first pivot door and second pivot door each form a portion of a surface of a bypass duct when in a stowed position. In the deployed position the first pivot door and the second pivot door circumferentially surround a portion of an inner surface of a bypass duct such that when the pivot thrust reverser is deployed during engine operation a fan bypass stream is redirected while b...

대표
청구항
▼

1. A pivot thrust reverser for use in a gas turbine engine assembly, the pivot thrust reverser comprising: a first pivot door forming a first portion of an outer surface of a nacelle when stowed;a second pivot door spaced from the first pivot door forming a second portion of the outer surface of the nacelle when stowed, wherein the first pivot door and the second pivot door are axially aligned and radially opposite along an axis of the gas turbine engine assembly and each form a portion of a surface of a bypass duct when stowed;an actuator configured to ...

이 특허에 인용된 특허 (51)

  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.
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  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. Calder, David P.; Howarth, Graham F.. Apparatus for facilitating access to a nacelle interior and method of assembling the same. USP2015119188026.
  7. Lair,Jean Pierre. Cascade reverser without blocker doors. USP2009027484356.
  8. Ramlaoui, Jihad I.; Seaver, Randall J.; James, Norman J.; Byrne, Stuart J.; Cornejo, Sheila. Cascadeless fan thrust reverser with plume control. USP2005116968675.
  9. Jannetta, Thomas J.; Peters, Frederick H.. Converging nozzle thrust reverser. USP2003056568172.
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  17. Lair,Jean Pierre; Wolters,Gregory Thomas. Induction coupled variable nozzle. USP2006107127880.
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  28. Lardy Pascal,FRX ; Valleroy Laurent Georges,FRX. Pivoting door thrust reverser with sliding panel. USP1999105970704.
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  30. Webb George (Cincinnati OH). Single pivot overwing thrust reverser. USP1992055110069.
  31. Sternberger, Joe E.. System for adjustment of thrust reverser pivot door. USP2011088002217.
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  33. Lair, Jean-Pierre. Thrust reverser door. USP2012018091827.
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  35. Johnston Everett A. (Mason OH) Ryan Edward W. (Mason OH). Thrust reverser for a long duct fan engine. USP1981074278220.
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  42. Brian E. Barton. Translating independently mounted air inlet system for aircraft turbofan jet engine. USP2002016340135.
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  44. Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser door spoilers with motion controlling drive system. USP2000116151884.
  45. 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.
  46. Canadas Marc,FRX. Turbojet pod with laminar flow. USP2001016179249.
  47. Gonidec Patrick,FRX ; Rouyer Pascal Gerard,FRX ; Vauchel Guy Bernard,FRX. Turbojet thrust reverser with downstream obstacles. USP2001016170255.
  48. Pero, Edward B.; Aceto, Leonard D.. Variable area fan nozzle and thrust reverser. USP2013048418436.
  49. Lair, Jean-Pierre. Variable area thrust reverser nozzle. USP2004026688099.
  50. James Varnell L. (Kent WA). Variable geometry convergent divergent exhaust nozzle. USP1980044196856.
  51. Bubello Robert (Meriden CT) Ream Jeffrey L. (Tollano CT). Ventilation system for a nacelle. USP1989054825644.

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