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특허 상세정보

Auxiliary wing tips for an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-005/08   
미국특허분류(USC) 244/199 ; 244/91 ; 244/45R
출원번호 US-0839431 (1986-03-13)
우선권정보 DE-3242584 (1982-11-18)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 61  인용 특허 : 1
초록

Auxiliary winglets or control surfaces for aircraft wings are tiltable about an axis extending in the flight direction and about an axis extending substantially perpendicularly to the flight direction. The auxiliary wing tips have a configuration which assure a wing surface continuity, especially when the tips are in their normal wing extending position, but also in any other position of the winglets. Additionally, at least the leading auxiliary winglets are located upstream of the elastic wing axis, as viewed in the flight direction and they have a forw...

대표
청구항

An aircraft wing construction, comprising wings, each wing including a leading edge, a trailing edge, an elastic axis, an outer wing end, and auxiliary winglet means at said outer wing end, said auxiliary winglet means including first hinging means securing said auxiliary winglet means to said outer wing end, said first hinging means having a first hinging axis extending substantially perpendicularly to a flight direction, and first drive means arranged for tilting said auxiliary winglet means about said first hinging axis of said first hinging means, sa...

이 특허를 인용한 특허 피인용횟수: 61

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