发明名称 ACTUATOR CONTROL SYSTEM AND METHOD FOR GAS TURBINE ENGINE
摘要 A system for controlling actuators within a gas turbine engine according to an exemplary aspect of the present disclosure includes an electronic engine controller, a plurality of actuators, and a central control unit. The central control unit includes an actuator control unit electrically coupled to the electronic engine controller and a plurality of actuator control modules. Each of the actuator control modules is electrically coupled to each of the plurality of actuators. A method is also disclosed.
申请公布号 US2016369745(A1) 申请公布日期 2016.12.22
申请号 US201514743148 申请日期 2015.06.18
申请人 Hamilton Sundstrand Corporation 发明人 Mueller Carl F.;Veilleux, JR. Leo J.
分类号 F02K1/76 主分类号 F02K1/76
代理机构 代理人
主权项 1. A system for controlling actuators within a gas turbine engine, comprising: an electronic engine controller; a plurality of actuators; and a central control unit, wherein the central control unit includes an actuator control unit electrically coupled to the electronic engine controller and a plurality of actuator control modules, each of the actuator control modules electrically coupled to each of the plurality of actuators.
地址 Charlotte NC US
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