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특허 상세정보

Flaperon system for tilt rotor wings

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/02   
미국특허분류(USC) 244/214 ; 244/130 ; 244/219
출원번호 US-0417811 (1989-10-13)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 56  인용 특허 : 0
초록

The present invention provides an aircraft wing (10) having a main portion (20) with a trailing edge (20b) and a movable flaperon (22) hingedly secured at the trailing edge. A movable flaperon seal (40) is hingedly attached at its leading edge to the trailing edge of the main portion of the wing. Interconnecting structure is provided between the main portion of the wing and the flaperon seal. Such structure is operable to pivot the seal flap such that the opening between the trailing edge of the main wing portion (20b) and the leading edge of said movabl...

대표
청구항

An aircraft wing assembly comprising: (a) a main wing portion having a trailing edge; (b) a pivotal flaperon directly attached to said main wing portion; (c) a flaperon seal pivotally attached to said main wing portion; (d) control means for interconnecting said flaperon and said flaperon seal and for angularly positioning said flaperon seal relative to said flaperon as said flaperon is pivoted relative to said main wing portion, said control means comprising: (i) a rigid arm attached to said flaperon seal; (ii) a cam follower attached to said rigid arm;...

이 특허를 인용한 특허 피인용횟수: 56

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