| 发明名称 |
REDUNDANT FLIGHT CONTROL SYSTEM |
| 摘要 |
<p>REDUNDANT FLIGHT CONTROL SYSTEM 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.</p> |
| 申请公布号 |
CA1094037(A) |
申请公布日期 |
1981.01.20 |
| 申请号 |
CA19780312066 |
申请日期 |
1978.09.26 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DURNO, RONALD A.;COOPER, DEAN E. |
| 分类号 |
B64C13/30;(IPC1-7):16H21/44 |
主分类号 |
B64C13/30 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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