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Actuator control system and method for gas turbine engine

  • US 10,309,342 B2
  • Filed: 06/18/2015
  • Issued: 06/04/2019
  • Est. Priority Date: 06/18/2015
  • Status: Active Grant
First Claim
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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, wherein the plurality of actuator control modules include a power conditioning module, an actuator position module, and a drive module.

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