发明名称 |
ACTUATOR FOR CONTROLLING A FLIGHT CONTROL SURFACE |
摘要 |
<p>The invention relates to an actuator (4) for controlling a flight control surface (3) of an aircraft, comprising: - a primary route (5) comprising a first member (8) for generating a first torque, and a first drive shaft (10) having an end (18) able to be connected to the first member (8) and an end (19) able to be connected to the control surface (3), - a secondary route (6) comprising a second member (24) for generating a second torque and a second drive shaft (26) having an end (45) able to be connected to the second member (24) and an end (46) able to be connected to the control surface (3), in which actuator the second drive shaft (10) is hollow and extends around the first drive shaft (26).</p> |
申请公布号 |
WO2015177301(A1) |
申请公布日期 |
2015.11.26 |
申请号 |
WO2015EP61314 |
申请日期 |
2015.05.21 |
申请人 |
SAGEM DEFENSE SECURITE |
发明人 |
CHAVIGNIER, LOUIS;LEBRUN, MARC;VIENNOT, SEVERIN |
分类号 |
B64C13/50;B64C13/28;F16H1/28;F16H25/20 |
主分类号 |
B64C13/50 |
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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