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특허 상세정보

Arrangement for effecting movement of a wing tip device between a flight configuration and a ground configuration

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/56    B64C-023/06   
출원번호 US-0045311 (2016-02-17)
등록번호 US-10137977 (2018-11-27)
우선권정보 GB-1502661 (2015-02-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Nixon & Vanderhye, PC
인용정보 피인용 횟수 : 0  인용 특허 : 29
초록

An aircraft comprises a wing, a wing tip device at the tip of the wing and an actuator. The actuator is arranged to effect movement of the wing tip device between a flight configuration for use during flight and a ground configuration in which the wing tip device is moved away from the flight configuration such that the span of the aircraft is reduced. The aircraft comprises a carriage guide, such as a track assembly, fixed relative to the wing, and a carriage arranged to move along the track assembly as the wing tip device moves between the flight and g...

대표
청구항

1. An aircraft comprising a wing having a span, a wing tip device at the tip of the wing and an actuator, wherein the actuator is arranged to effect movement of the wing tip device between: (i) a flight configuration for use during flight and(ii) a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved away from the flight configuration such that the span of the aircraft wing is reduced,characterised in that the aircraft comprises: a carriage guide, fixed relative to the wing, anda carriage...

이 특허에 인용된 특허 (29)

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  2. Guida, Nicholas R.. Active winglet. USP2017099764825.
  3. Harding, Matthew; Napier, Stefan; Marongiu, Nicola; Thompson, Robert Ian; Livings, Nick; Briancourt, Stephen Paul; Boye, Sylvain. Actuation assembly for moving a wing tip device on an aircraft wing. USP2018029889920.
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  5. Johnstone Edmund H. (82 Salzburg Blvd. Apt. G Columbus IN 47201). Aircraft wing vortex deflector. USP1976083974986.
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  7. Fong, Tony; Axford, Timothy. Braided composite spar. USP2018029896186.
  8. Paez Carlos A. (Northport NY). Folding wing assembly. USP1994125372336.
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  10. Smith Mark H. (Vashon Island WA) Renzelmann Michael E. (Woodinville WA) Marx Alan D. (Seattle WA). Folding wing-tip system. USP1995015381986.
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  15. Young Kendall Gardner ; Pauletti Steven Louis. Low density flexible edge transition. USP2001016173924.
  16. Parker, Simon John. Method of coupling aerofoil surface structures and an aerofoil assembly. USP2015089096304.
  17. Dasa Madhava (R.R. 1 - Box 549 Kula HI 96790). Multiple configuration model aircraft. USP1987104698041.
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  19. Renzelmann Michael E. (Woodinville WA). Self-monitoring latch pin lock for folding wing aircraft. USP1993045201479.
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  22. Ratony Alexander (2076 Shadybrook Thouand Oaks CA 91362). Tri-channel wing aircraft. USP198911D304821.
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  27. Veile Joseph R. (St. Louis MO). Wing fold push-pin locking assembly. USP1996095558299.
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  29. Krafka Herfried (Toulouse FRX) Jendrian Henry (Tournefeuille FRX). Wing with extendable flap and variable camber. USP1988024725026.