发明名称 |
AN ELECTROMECHANICAL ACTUATOR FOR AN AIRCRAFT CONTROL SURFACE, AND AN AIRCRAFT PROVIDED WITH SUCH AN ACTUATOR |
摘要 |
An electromechanical actuator for a movable flight control surface of an aircraft, the actuator comprising an electric motor (2) having an outlet shaft (20) with first and second directions of rotation, a movement transmission (1) arranged to connect the outlet shaft of the motor to the movable flight control surface, and a control unit (3) for controlling the motor. The transmission incorporates a pawl device (18) arranged to oppose the transmission of movement in the first direction of rotation, and the control unit is connected to a pawl declutching member (19) for declutching the pawl and enabling movement to be transmitted in the first direction of rotation. |
申请公布号 |
CA2854239(C) |
申请公布日期 |
2016.06.14 |
申请号 |
CA20122854239 |
申请日期 |
2012.11.21 |
申请人 |
SAGEM DEFENSE SECURITE |
发明人 |
SENEGAS, DAVID;MEHEZ, JEROME;JESTIN, MAXIME;SEVAGEN, BERTRAND |
分类号 |
F16H31/00;B64C13/24;F16H35/00 |
主分类号 |
F16H31/00 |
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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