发明名称 |
Control mean provided with a collective lever blade pitch control and with means for yaw control as well as an aircraft with such a control mean |
摘要 |
The controller (10) has a collective pitch lever (20) extending from an end (21) towards another end (22). A handle (30) controls a yaw movement control device, where the handle is secured to an inner crown (40) guided in rotation around an axis (AXLAC) by an outer crown (50) integral with the latter end of the lever. The inner crown is secured to the outer crown, where the lever is rotatable about another axis (AXCOL), so that elevational movement of a hand of a pilot causes rotation of the lever to generate a collective control command of collective pitch of blades. An independent claim is also included for a rotorcraft. |
申请公布号 |
EP2759473(A1) |
申请公布日期 |
2014.07.30 |
申请号 |
EP20140000191 |
申请日期 |
2014.01.20 |
申请人 |
AIRBUS HELICOPTERS |
发明人 |
KERDREUX, CHRISTELLE;COLAPRISCO, MARC;BARDET, DAVID |
分类号 |
B64C27/56;G05G9/047 |
主分类号 |
B64C27/56 |
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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