| 发明名称 |
Control device for a helicopter main rotor |
| 摘要 |
<p>For the control of a helicopter main rotor, each rotor blade (3) has at least one flap (19) on a pivot axis (18) parallel or coaxial to the longitudinal blade axis (5). It is deployed by an actuator (20) with the functions of the individual blade actuators (8).</p> |
| 申请公布号 |
EP1985536(A2) |
申请公布日期 |
2008.10.29 |
| 申请号 |
EP20080154292 |
申请日期 |
2008.04.10 |
| 申请人 |
ZF FRIEDRICHSHAFEN AG |
发明人 |
WINTJEN, CARSTEN;HAUSBERG, ANDRE;FUERST, DANIEL |
| 分类号 |
B64C27/605;B64C27/615;B64C27/72 |
主分类号 |
B64C27/605 |
| 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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