发明名称 SYSTEME DE COMMANDE DE VOL REDONDANT
摘要 A flight control system utilizing pilot actuated flexible cables to selectively move a control quadrant and utilizing balanced, preloaded springs connected to the quadrant to be selectively automatically releasable in response to cable severance so that the quadrant can be pilot actuated through its full control regime despite the severance of one of the cables.
申请公布号 BE871502(A1) 申请公布日期 1979.02.15
申请号 BE19780191317 申请日期 1978.10.24
申请人 UNITED TECHNOLOGIES CORP. 发明人 R.A. DURNO;D.E. COOPER
分类号 B64C13/30;(IPC1-7):64D/ 主分类号 B64C13/30
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