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특허 상세정보

Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/00    B64C-009/02    B64C-007/00   
출원번호 US-0831066 (2015-08-20)
등록번호 US-10000274 (2018-06-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Duft Bornsen & Fettig LLP
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

Embodiments provide a transitional element that bridges a gap between an edge of a flight control surface and an edge of a non-movable portion of an airframe. In one embodiment, a transitional element bridges a gap between an edge of a flight control surface and an edge of a non-movable portion of an airframe. The transitional element includes a plurality of ribs that span the gap. Each of the plurality of ribs has a contour that corresponds to the flight control surface and is configured to pivot a portion of a rotated angle of the flight control surfac...

대표
청구항

1. An apparatus, comprising: a transitional element that is configured to bridge a gap between an edge of a flight control surface and an edge of a non-movable portion of an airframe, the transitional element including: a member that spans the gap and has a first end fixed proximate to the edge of the flight control surface and a second end fixed proximate to the edge of the non-movable portion of the airframe, wherein the member defines an axis extending from the edge of the flight control surface to the edge of the non-movable portion of the airframe; ...

이 특허에 인용된 특허 (13)

  1. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2010057708231.
  2. Kunz Rdiger (Munich DEX). Apparatus for closing an air gap between a flap and an aircraft. USP1984094471925.
  3. Kruse, John Scott; Fogarty, John Hershey. Attachment of aircraft ribs to spars having variable geometry. USP2016059346533.
  4. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223. Continuous moldline technology system. USP1998095810291.
  5. Caton John Harold ; Hobey Michael James ; Groeneveld John David ; Jacobs Jack Howard ; Wille Robert Henry ; Brase ; Jr. Lawrence Otto. Control surface for an aircraft. USP2001046209824.
  6. Khorrami, Mehdi R.; Lockard, David P.; Moore, James B.; Su, Ji; Turner, Travis L.; Lin, John C.; Taminger, Karen M.; Kahng, Seun K.; Verden, Scott A.. Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction. USP2014048695925.
  7. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP2000116145791.
  8. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  9. Young Kendall Gardner ; Pauletti Steven Louis. Low density flexible edge transition. USP2001016173924.
  10. Etling, Keith A.. Morphing control surface transition. USP2013018342447.
  11. Hamilton Terry W. (Box 49 Bulverde TX 78163). Over-lap rib joint. USP1988044739954.
  12. Young Kendall Gardner ; Pauletti Steven Louis. Rotor driven edge. USP2001066244542.
  13. Orazi Paul. Wing assemblies for aircraft. USP1999115984230.