ACTUATOR CONTROL SYSTEM AND METHOD FOR GAS TURBINE ENGINE

摘要

A system for controlling actuators within a gas turbine engine includes an electronic engine controller (22), a plurality of actuators (24A - 24N), and a central control unit (26). The central control unit includes an actuator control unit (28) electrically coupled to the electronic engine controller and a plurality of actuator control modules (30, 32, 34). Each of the actuator control modules is electrically coupled to each of the plurality of actuators. A method is also disclosed.