发明名称 |
Disengageable control column for a copilot of an aircraft |
摘要 |
The invention relates to a control column (2) for a copilot of an aircraft, coupled for control of roll and pitch by a linkage (5) to the pilot's control column (1). This linkage comprises two parallel rods (6,7) pivoted on the one hand to the column (1) and on the other hand to a member (13) connected to the column (2) by a double universal joint (14, 17). When operative, the column (2) is locked to the member (13) by a lock bolt (19). This control column can be put out of action by releasing the said bolt and can be secured by hooking to a fixed point, in which case the double universal joint (14, 17) ensures its disconnection from the column (1) and thus prevents any misoperation.
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申请公布号 |
US4473203(A) |
申请公布日期 |
1984.09.25 |
申请号 |
US19830482172 |
申请日期 |
1983.04.05 |
申请人 |
SOCIETE NATIONALE INDUSTRIELLE ET AEROSPATIALE |
发明人 |
BARNOIN, PIERRE;CAS, JACQUES M. |
分类号 |
B64C13/12;G05G9/047;G05G11/00;(IPC1-7):B64C13/12;B64C13/14 |
主分类号 |
B64C13/12 |
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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