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특허 상세정보

Systems and methods for controlling aircraft flaps and spoilers

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/06    B64C-009/00    B64C-009/18    B64C-009/32   
미국특허분류(USC) 244/215; 244/099.2
출원번호 US-0051738 (2005-02-04)
등록번호 US-7338018 (2008-03-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 27  인용 특허 : 204
초록

Systems and methods for controlling aircraft flaps and spoilers. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned proximate to the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position by operation of a first actuator. A spoiler can be positioned at least proximate to the trailing edge and can be movable among at least three positions, including a first spoiler position in which the spoiler forms a generally continuous contour with an...

대표
청구항

We claim: 1. An aircraft wing system, comprising: a wing having a trailing edge; a flap positioned proximate to the wing trailing edge and being deployable relative to the wing between a first flap position and a second flap position; a first actuator operatively coupled to the flap to move the flap between the first flap position and the second flap position; a spoiler positioned at least proximate to the flap, the spoiler being movable among at least three positions including a first spoiler position in which the spoiler forms a generally continuous c...

이 특허에 인용된 특허 (204)

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