发明名称 |
Control device for helicopter tail rotor |
摘要 |
The device controls first the aerodynamic surface (D) of the mixed rotor so that it engenders a lift which is representative of a first control command able to be executed by the surface. It also controls the tail rotor (R2) so that the combined action of the surface and the rotor is representative of a yawing order of the helicopter. A rudder bar (3) and a collective handle control yawing.
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申请公布号 |
FR2769285(A1) |
申请公布日期 |
1999.04.09 |
申请号 |
FR19970012454 |
申请日期 |
1997.10.07 |
申请人 |
EUROCOPTER FRANCE |
发明人 |
DEQUIN ANDRE MICHEL LOUIS;DELISLE VALERY LIONEL |
分类号 |
B64C13/16;B64C27/82;G05D1/08;(IPC1-7):B64C27/82;B64C13/02 |
主分类号 |
B64C13/16 |
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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