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특허 상세정보

Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-007/00    B64C-009/02   
출원번호 US-0001832 (2016-01-20)
등록번호 US-10150557 (2018-12-11)
우선권정보 DE-10 2013 012 169 (2013-07-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lerner, David, Littenberg, Krumholz & Mentlik, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

A transition piece, which can be mounted in a recess, and which can form a continuous surface from a structural component of an airplane to a control surface, which is connected to the structural component in a pivotable manner is described. The transition piece can be mounted between an edge of the structural component and a lateral edge of the control surface such that the transition piece is fastened in a pivotable manner both to the edge of the structural component and to the lateral edge of the control surface. According to an example, the transitio...

대표
청구항

1. A transition piece for forming a continuous surface from a structural component of an aircraft to a control surface, wherein the control surface has a front edge, a rear edge and two lateral edges, wherein the front edge or the rear edge of the control surface is pivotally connected to the structural component, wherein the transition piece is configured to be mounted in a recess formed between an edge of the structural component and one of the lateral edges of the control surface,wherein the transition piece is configured to be pivotally mounted on th...

이 특허에 인용된 특허 (13)

  1. Kunz Rdiger (Munich DEX). Apparatus for closing an air gap between a flap and an aircraft. USP1984094471925.
  2. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223. Continuous moldline technology system. USP1998095810291.
  3. 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.
  4. 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.
  5. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP2000116145791.
  6. Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
  7. Wille Robert Henry. Hinge line skin system for an aircraft. USP1999085941480.
  8. Young Kendall Gardner ; Pauletti Steven Louis. Low density flexible edge transition. USP2001016173924.
  9. Turner, Travis L.; Khorrami, Mehdi R.; Lockard, David P.; McKenney, Martin J.; Atherley, Raymond D.; Kidd, Reggie T.. Multi-element airfoil system. USP2014078763958.
  10. Jasklowski, Christopher T.. Shape memory alloy actuation system for variable area fan nozzle. USP2017029581145.
  11. Madsen, Casey Lyn. Shape memory alloy rods for actuation of continuous surfaces. USP2015119174723.
  12. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA). Variable camber aircraft wing tip. USP1984024429844.
  13. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.