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특허 상세정보

Aircraft wings with aileron-supported ground speed spoilers and trailing edge flaps

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/34   
미국특허분류(USC) 244/217 ; 244/215 ; 244/90R ; 244/90A
출원번호 US-0835804 (1986-03-03)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 57  인용 특허 : 2
초록

Aileron-supported split flaps and ground speed spoilers (collectively referred to as “aerodynamic lifting or braking devices”) for reducing aircraft approach speeds and reducing the length of the runway needed to land the aircraft. The actuating mechanism for the aerodynamic lifting or braking device allows the latter to rotate with the supporting aileron as the latter is moved up and down when the lifting or braking device is in its stowed position. When the lifting or braking device is in its extended position, up and down aileron movements will cause ...

대표
청구항

The combination of: an aircraft wing; an aileron extending along said wing at the rear edge thereof; stationary aileron support means fixed to said wing; pivot means fixing said aileron to said support means for pivotable movement about an axis extending spanwise of said wing; an aerodynamic lifting or braking means adapted to be displaced from a stowed position in which said lifting or braking means is butted against said aileron to an extended position in which the lifting or braking means is oriented at an angle relative to the chord plane of said win...

이 특허를 인용한 특허 피인용횟수: 57

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