| 发明名称 |
Helicopter flight control systems. |
| 摘要 |
<p>In a helicopter, signals representative of the rotor disc attitude of a main sustaining rotor (11) are fed into a flight control system (24) to modify an actuator demand signal (31) controlling a rotor blade actuation system (32) of the main sustaining rotor.</p> |
| 申请公布号 |
EP0272058(A2) |
申请公布日期 |
1988.06.22 |
| 申请号 |
EP19870310903 |
申请日期 |
1987.12.10 |
| 申请人 |
WESTLAND GROUP PLC |
发明人 |
THORPE, JANE MARGARET;TAYLOR, PAUL;GRAHAM, ALISTAIR CHARLES |
| 分类号 |
B64C27/72;G05D1/08 |
主分类号 |
B64C27/72 |
| 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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