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특허 상세정보

Thrust reverser door

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/54   
미국특허분류(USC) 244/110B; 060/226.2
출원번호 US-0941360 (2007-11-16)
등록번호 US-8091827 (2012-01-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Conte, Francis L.
인용정보 피인용 횟수 : 13  인용 특허 : 189
초록

A thrust reverser door provides in one aspect a separation of structural and aerodynamic functions through the provision of individual structures. In some embodiments, an aerodynamic element is adjustable in position, while in other embodiments, the relative positions are fixed. An exemplary aerodynamic element extends radially into the reverser flow to redirect the flow away from the door surface.

대표
청구항

1. A thrust reverser having at least one thrust reverser door pivotable between stowed closed and deployed open positions, the at least one door comprising a transverse leading edge having a first, second and third frames axially spaced apart from one another to define a radially open channel therebetween and disposed circumferentially adjacent said leading edge, the first, second and third frames projecting inwardly from an interior side of the at least one door, the third frame mounted to the first and second frames, the third frame extending inwardly ...

이 특허에 인용된 특허 (189)

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  168. 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.
  169. Gonidec Patrick,FRX ; Portal Jean Fabrice Marcel,FRX ; Studer Vincent Joseph Rodolphe,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser having scoop doors and movable upstream visors. USP2000066076347.
  170. Lardy Pascal,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser with asymmetrical doors. USP1998035727380.
  171. Lardy Pascal,FRX ; Valleroy Laurent Georges,FRX ; Vauchel Guy Bernard,FRX. Turbojet engine thrust reverser with biased baffles. USP1998075775097.
  172. Carimali Flix (Le Havre FRX) Legras Michel J. L. (Le Havre FRX). Turbojet engine thrust reverser with directional control. USP1994025284015.
  173. de Cambray Elisabeth L. F. C. (Le Havre FRX) Vicogne Laurent M. (Gonfreville L\Orcher FRX). Turbojet engine thrust reverser with rear support structure. USP1996085548954.
  174. Barbarin Jacques M. G. (Montivilliers FRX) Lecoutre Pascal B. G. (Le Havre FRX). Turbojet engine thrust reverser with variable exhaust cross-section. USP1990054922713.
  175. Gonidec Patrick,FRX ; Rouyer Pascal Gerard,FRX ; Vauchel Guy Bernard,FRX. Turbojet thrust reverser with downstream obstacles. USP2001016170255.
  176. Michel Christian Marie Jean FR; Laurent Marcel Vicogne FR. Turbojet-engine thrust reverser with doors mounted on centered pivots. USP2002066402092.
  177. Metezeau Fabrice Henri Emile,FRX ; Vauchel Bernard Guy,FRX. Turbojet-engine thrust reverser with internal clamshells. USP2000116151885.
  178. Gonidec Patrick,FRX ; Portal Jean Fabrice Marcel,FRX ; Studer Vincent Joseph Rodolphe,FRX ; Vauchel Guy Bernard,FRX. Turbojet-engine thrust reverser with scoop-doors of adjustable exhaust cross-section. USP2000126158211.
  179. Osman Medhat A. (1416 Ridgeback Rd. #D Chula Vista CA 91910). Ultra thrust reverser system. USP1997045615834.
  180. Lair Jean-Pierre (100 W. El Prado ; Suite 308 San Antonio TX 78212). Variable area exhaust nozzle. USP1993065221048.
  181. 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. USP1998075778659.
  182. Lair, Jean-Pierre. Variable area plug nozzle. USP2005016845607.
  183. Lair, Jean-Pierre. Variable area thrust reverser nozzle. USP2004026688099.
  184. Lair,Jean Pierre. Variable cam exhaust nozzle. USP2006087093793.
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  186. Cariola Roy E. ; Aten Michael R.. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser. USP1998095806302.
  187. Joyce, Nicolas J.. Vectorable variable area nozzle. USP2005066910328.
  188. Lair,Jean Pierre. Ventilated confluent exhaust nozzle. USP2006037010905.
  189. Herrick Paul W. (Jupiter FL) Thayer Edward B. (Jupiter FL) Stewart Jim D. (Jupiter FL). Yaw and pitch convergent-divergent thrust vectoring nozzle. USP1989064836451.