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특허 상세정보

Auxiliary flaperon control for aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/06    B64C-009/12   
미국특허분류(USC) 244/75R ; 244/90R ; 244/215
출원번호 US-0833307 (1977-09-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 42  인용 특허 : 0
초록

An auxiliary flaperon control is pivotally mounted on the trailing edge of each wing of an aircraft between the outboard control surfaces and the fuselage and in close proximity to the tail of said aircraft; the auxiliary flaperon controls being operable relative to the outboard control surfaces to induce supplementary aerodynamic forces on the aircraft tail to thereby augment the effectiveness of aircraft lateral and directional control.

대표
청구항

In an aircraft which includes a fuselage, relatively thin right and left wings, outboard control surfaces mounted on the trailing edges of said wings, and a vertical tail: a. auxiliary control means pivotally mounted on each of said wings intermediate said outboard control surface and said fuselage forwardly of said vertical tail in close proximity thereto, said auxiliary control means being independently operable in opposition to movement of said outboard control surfaces to induce a supplementary aerodynamic forces on said vertical tail and thereby aug...

이 특허를 인용한 특허 피인용횟수: 42

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