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특허 상세정보

Aileron segment control for a flaperon system

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-009/06    B64C-009/12   
미국특허분류(USC) 244/75R ; 74/25 ; 244/215 ; 244/90R
출원번호 US-0754823 (1976-12-27)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 47  인용 특허 : 0
초록

An improved control system for the aileron segment of a combined flap and aileron (flaperon) wherein the flaperon, supported, extended and retracted by conventional means, is described. It consists of a splined shaft rotatably mounted on an aircraft wing, its longitudinal axis being substantially aligned with the extension and retraction path of the flap. A transfer gear box slidably engages the splined shaft and is supported by a roller assembly engaging a support track which is mounted in the wing and runs substantially parallel to the splined shaft. T...

대표
청구항

In an aircraft wing flaperon system comprising a flap, flap power means and means driven thereby to extend and retract the flap, flap guide means mounted in the wing to support and guide the flap, and an aileron segment contained within, defining a portion of and attached to the flap for rotation relative to the flap about an axis of rotation, an improved aileron segment control system comprising: aileron segment rotation power means connected to receive pilot inputs; a first power transfer means having an output shaft for controlling the aileron segment...

이 특허를 인용한 특허 피인용횟수: 47

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