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특허 상세정보

Aileron for fixed wing aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/06   
미국특허분류(USC) 244/217
출원번호 US-0581951 (2000-09-20)
국제출원번호 PCT/US98/25199 (1998-12-03)
국제공개번호 WO99/30967 (1999-06-24)
발명자 / 주소
대리인 / 주소
    Burns, Doane, Swecker & Mathis, L.L.P.
인용정보 피인용 횟수 : 55  인용 특허 : 8
초록

An aircraft aileron system (10, 10) is comprised of two panels (12, 14, 28, 30, 62, 70) located at the rear portion of the wing (W24, 54), in a spanwise direction and aligned with the wing's trailing edge. The panels are independently hinged at their leading edges and rotate to make angular deflections with respect to the wing. The upper, aileron panel (12, 30, 62) is restricted to upward deflection only from its neutral position and in operation is deployed independently as an aileron. The lower, auxiliary flap panel (14, 28, 70) is capable of both upwa...

대표
청구항

An aircraft aileron system (10, 10) is comprised of two panels (12, 14, 28, 30, 62, 70) located at the rear portion of the wing (W24, 54), in a spanwise direction and aligned with the wing's trailing edge. The panels are independently hinged at their leading edges and rotate to make angular deflections with respect to the wing. The upper, aileron panel (12, 30, 62) is restricted to upward deflection only from its neutral position and in operation is deployed independently as an aileron. The lower, auxiliary flap panel (14, 28, 70) is capable of both upwa...

이 특허를 인용한 특허 피인용횟수: 55

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