发明申请
- 专利标题： HIGH INTEGRITY ROTARY ACTUATOR AND METHOD OF OPERATION
- 专利标题（中）： 高精度旋转执行器和操作方法
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申请号： US13424884申请日： 2012-03-20
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公开(公告)号： US20150105199A9公开(公告)日： 2015-04-16
- 发明人: Terence Ross Golding
- 申请人： Terence Ross Golding
- 优先权： GB1105478.0 20110331
- 主分类号： H02P5/695
- IPC分类号： H02P5/695 ; F16H3/72 ; B64C25/18 ; F16H61/12 ; B64C13/38 ; H02K7/116
摘要：
An actuator for an aircraft is provided. The actuator comprises a first motor, a second motor and an actuator output, which are interconnected by a gear assembly. The actuator output is driveable by the first motor independently of the second motor; the actuator output is driveable by the second motor independently of the first motor; and the actuator output is driveable by the first and second motors in combination.
公开/授权文献
- US20130249444A1 HIGH INTEGRITY ROTARY ACTUATOR AND METHOD OF OPERATION 公开/授权日：2013-09-26
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