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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Aerospace vehicle leading edge slat devices and corresponding methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50    B64C-003/00   
미국특허분류(USC) 244/214
출원번호 US-0048320 (2005-01-31)
등록번호 US-7322547 (2008-01-29)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 18  인용 특허 : 196

Aerospace vehicle leading edge slat devices and corresponding methods are generally disclosed herein. One aspect of the invention is directed toward an aerospace vehicle system that includes an airfoil having a leading edge. The system further includes a first flow body fixedly coupled to the airfoil to form at least one gap between the leading edge of the airfoil and the first flow body. A second flow body can be coupled to the airfoil and can be movable between at least a retracted position where the second flow body is positioned to at least approxima...


I claim: 1. An aerospace vehicle system, comprising: an airfoil having a leading edge; a first flow body fixedly coupled to the airfoil to form at least one gap between the leading edge of the airfoil and the first flow body; and a second flow body having a recess, an upper trailing edge, and a lower trailing edge, the second flow body being movably coupled to the airfoil to move between: a retracted position wherein the second flow body is positioned to at least approximately aerodynamically seal the at least one gap, and wherein the first flow body is...

이 특허에 인용된 특허 (196)

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