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특허 상세정보

Guide system for nacelle assembly

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01B-025/02   
미국특허분류(USC) 415/144; 415/128; 415/145; 415/157; 415/196; 415/211.2
출원번호 US-0821364 (2010-06-23)
등록번호 US-8511973 (2013-08-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Snell & Wilmer L.L.P.
인용정보 피인용 횟수 : 10  인용 특허 : 27
초록

A guide system for translating components of an aircraft engine nacelle includes a track assembly and a slider assembly. The track assembly includes a track guide member having a track channel. The slider assembly translatably engages the track assembly. The slider assembly includes a slider body configured to be received within the track channel. The slider assembly further includes a slider arm member pivotably coupled to the slider body with a hinge joint disposed within the track channel. The slider arm member extends from the body portion and outwar...

대표
청구항

1. A guide system for translating components of an aircraft engine nacelle, the guide system comprising: a track assembly adapted to operably engage a first portion of a nacelle, the track assembly comprising a track guide member having a track channel; anda slider assembly configured to translatably engage the track assembly, the slider assembly comprising a slider body configured to be received within the track channel, the slider assembly further comprising a slider arm member pivotably coupled to the slider body with a hinge joint disposed within the...

이 특허에 인용된 특허 (27)

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  2. Timms Richard H. (San Diego County CA). Aircraft thrust reverser mechanism. USP1985054519561.
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  5. Nikkanen John P. (West Hartford CT). Compact thrust reverser. USP1996115575147.
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  7. Carimali Flix (Le Havre FRX) Legras Michel J. L. (Le Havre FRX). Deflector edge for a thrust reverser. USP1994035297387.
  8. Baudu Pierre Andre Marcel,FRX ; Gonidec Patrick,FRX ; Vauchel Guy Bernard,FRX. Electric control system for a turbojet engine thrust reverser including an electromechanical drive device and a locking. USP1999105960626.
  9. James Varnell L. (Auburn WA). Jet engine thrust reverser. USP1977054026105.
  10. Davies,Stephen Harlow; Guy,Mark Anthony; Somerfield,Michael Paul; Tucker,David Roy. Linear actuator. USP2007027174828.
  11. Jean Michel Christian Marie,FRX. Self-closing pivoting door thrust reverser. USP2000066079201.
  12. Richard G Stretton GB. Thrust reverser. USP2002116474059.
  13. Timms Richard H. (San Diego CA). Thrust reverser geared linkage. USP1983104407120.
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  16. Butler Lawrence (Cincinnati OH). Thrust reverser with variable nozzle. USP1997085655360.
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  18. Lair, Jean-Pierre. Toggle interlocked thrust reverser. USP2005126976352.
  19. Cariola Roy E.. Translating sleeve for cascade type thrust reversing system for fan gas turbine engine for an aircraft. USP2001016170254.
  20. Marshall, Richard M.; Gukeisen, Robert L.. Tri-body variable area fan nozzle and thrust reverser. USP2012018104261.
  21. Barbarin Jacques M. G. (Montivilliers FRX) Lecoutre Pascal B. G. (Le Havre FRX). Turbojet engine thrust reverser with variable exhaust cross-section. USP1990054922713.
  22. Johnston Everett A. (Mason OH). Variable area exhaust nozzle. USP1979014132068.
  23. 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.
  24. Gonidec Patrick,FRX ; Guy Bernard Vauchel,FRX. Variable cross-section turbofan exhaust duct with door type thrust reverser for aircraft. USP1999125996937.
  25. Cariola Roy E. ; Aten Michael R.. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser. USP1998095806302.
  26. Konarski Mieczyslaw (Lawrenceburg IN). Variable geometry exhaust nozzle. USP1983034375276.
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