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