System for controlling a plurality of functions of a turbojet engine

摘要

A control system for controlling a plurality of distinct functions of a turbojet engine, each function being associated with a respective actuation device. The system includes: an electric motor adapted to supply mechanical energy to each of the actuation devices; an electronic control unit for the electric motor; and at least one switching device interposed between the motor and the actuation devices, the switching device(s) serving to distribute the mechanical energy supplied by the electric motor selectively to one of the actuation devices.

主权项

1. A control system for controlling a plurality of distinct functions of a turbojet engine that are not to be operated simultaneously, each function being associated with a respective actuation device, the system comprising:
an electric motor adapted to supply mechanical energy to each of the actuation devices; at least one switching device interposed between the motor and the actuation devices; and an electronic control unit for the at least one switching device and the electric motor wherein the electronic control unit controls the at least one switching device to selectively distribute the mechanical energy supplied by the electric motor to one of the actuation devices based on the function to be operated by the one of the actuation devices, and controls the at least one switching device such that the other actuation devices that are not operated simultaneously with the one of the operating devices are not supplied in mechanical energy by the electric motor.