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특허 상세정보

Variable camber aircraft wing tip

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/48   
미국특허분류(USC) 244/219
출원번호 US-0451216 (1982-09-29)
국제출원번호 PCT/US82/01354
§371/§102 date 19820929 (19820929)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 43  인용 특허 : 1
초록

A variable wing tip (18) for securing to a variable camber leading edge portion (12) of an aircraft wing (10). The wing tip has a normal fore and aft camber in an upper position and is adapted to have an increased camber curvature in a deflected down position. In the down position, the wing tip has a compound curvature, is shortened in the fore and aft direction ad is generally thickened in depth in a substantial portion of the wing tip. By operation of an actuator (96) in the leading edge (21), a multiple of generally parallel scissor plates (30,32) are...

대표
청구항

In an aircraft wing, a variable camber wing tip forming an outboard and forward portion of said wing, said wing tip comprising: an inboard generally fore and aft extending end of the wing tip being secured along a complementary outer end of a variable camber leading edge portion of the wing; a trailing edge of the wing tip extending along a fixed outboard forwardly facing edge of the wing; said wing tip having a normal camber on its upper surface in an upper position and being adapted to have an increased camber curvature in a deflected down position; sa...

이 특허를 인용한 특허 피인용횟수: 43

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