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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0655620 (1976-02-05) |
발명자 / 주소 |
|
인용정보 | 피인용 횟수 : 3 인용 특허 : 0 |
Control system for aircraft wing spoilers in which the amount of centering moment provided by the downwardly moving or aerodynamically inactive spoiler is increased as the aircraft flaps are extended, the control system including a differential linkage mechanism interconnecting the flaps and the spo
In a control system for aircraft wing spoilers wherein said aircraft includes wings provided with flaps and also includes manual cockpit controls which are operatively connected to said spoilers and flaps, and wherein said spoilers are hingedly mounted in said wings forward of the wing flaps and are
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