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특허 상세정보

Extendible leading edge flap

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/44   
미국특허분류(USC) 244/219 ; 244/214 ; 244/218 ; 244/076R
출원번호 US-0936631 (1997-09-25)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 39  인용 특허 : 9
초록

A flight control system comprises trailing edge airfoil members pivotally mounted at the trailing edge of each wing of an aircraft and selectively movable on a laterally extending axis between raised and lowered positions for imparting rolling motion to the aircraft. Leading edge airfoil members mounted adjacent the leading edge on each of the wings are movable transversely of the leading edge between a retracted position generally coextensive with the leading edge and an extended position protruding from the leading edge for imparting countervailing aer...

대표
청구항

[ What is claimed is:] [1.] A flight control system for an aircraft including a fuselage having a longitudinal axis and fixed wings supported on and extending laterally from said fuselage, said wings having leading and trailing edges, respectively, said flight control system comprising:trailing edge airfoil means pivotally mounted at said trailing edge of each of said wings and selectively movable on a laterally extending axis between raised and lowered positions for imparting roll movement to said aircraft;trailing edge actuating means operable for movi...

이 특허를 인용한 특허 피인용횟수: 39

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  14. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
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