发明名称 |
Fly by wire servos with internal loop closure |
摘要 |
Embodiments are directed to obtaining a first analog signal corresponding to a position error between a commanded gang output of a plurality of electro-mechanical actuators configured to be run in parallel with one another and a measured gang output of the plurality of electro-mechanical actuators, obtaining a second analog signal corresponding to an output torque, and processing, by a circuit, the first analog signal and the second analog signal to generate and output a discrete that indicates a status of the torque in terms of direction and magnitude. |
申请公布号 |
US9193455(B2) |
申请公布日期 |
2015.11.24 |
申请号 |
US201414184356 |
申请日期 |
2014.02.19 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
Cotton Bryan S.;Harrigan Matthew;Winslow Christopher L. |
分类号 |
B64C27/64;B64C27/57;B64C27/68 |
主分类号 |
B64C27/64 |
代理机构 |
Cantor Colburn LLP |
代理人 |
Cantor Colburn LLP |
主权项 |
1. A servo assembly comprising:
a hydraulic primary servo; a plurality of electro-mechanical actuators coupled to the primary servo and configured to drive the primary servo; at least one device configured to perform loop closure; and a summation bar coupled to a plurality of output arms associated with the plurality of electro-mechanical actuators and configured to perform a mechanical averaging of differences in outputs of the electro-mechanical actuators. |
地址 |
Stratford CT US |