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특허 상세정보

Aerial vehicle with variable aspect ratio deployable wings

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/40   
미국특허분류(USC) 244/046; 244/049; 244/219
출원번호 UP-0707088 (2007-02-16)
등록번호 US-7841559 (2011-01-31)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kaye Scholer LLP
인용정보 피인용 횟수 : 7  인용 특허 : 54
초록

Embodiments of the present invention relate a wing arrangement for an aerial vehicle configured to adjust the vehicles aspect ratio in response to flight mission parameters. The wing arrangement may include a pair of wing assemblies capable of deploying to a first winged position defining a first aspect ratio. Each wing assembly may have a forward inboard wing pivotally connected to the fuselage and an aft inboard wing pivotally connected to the carriage. The forward inboard wing and aft inboard wing of each assembly may be connected, forming a bi-plane ...

대표
청구항

What is claimed is: 1. A wing arrangement for an aerial vehicle, comprising: a deployment mechanism configured to attach to a first side of a fuselage and configured to move from a first position to a second position; a first wing configured to be rotationally coupled to a second side of the fuselage; a second wing configured to be rotationally coupled to the deployment mechanism and rotationally coupled to the first wing; a third wing configured to be rotationally coupled to the second side of the fuselage; and a fourth wing configured to be rotational...

이 특허에 인용된 특허 (54)

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