发明名称 Fault-tolerant electromechanical actuator having a torque sensing control system
摘要 An electromechanical actuator (EMA) is provided. The EMA includes a threaded output ram connectable to a mechanical component and at least one motor module engageable with the output ram for controllably translating the output ram along a linear axis of the output ram. The actuator further includes a torque sensing adaptive control (TSAC) system for monitoring torque within the motor module. The TSAC generates a disengagement command signal when the TSAC system determines torque within the motor module is outside an allowable motor module torque range. The disengagement command signal initiates disengagement of the motor module from the output ram.
申请公布号 US2006113933(A1) 申请公布日期 2006.06.01
申请号 US20050291709 申请日期 2005.12.01
申请人 THE BOEING COMPANY 发明人 BLANDING DAVID E.;PECK JAMES L.
分类号 H02P7/00;B64C13/00;B64C13/24;F16H25/20;F16H27/02;H01L41/04;H02K7/06;H02K7/10;H02K16/00;H02K19/38;H02K41/00 主分类号 H02P7/00
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