SYSTEM FOR CONTROLLING A PLURALITY OF FUNCTIONS OF A TURBOJET ENGINE

摘要

The invention relates to a control system (1) for controlling a plurality of functions of a turbojet engine, each function being associated with one actuating device (10, 20). The control system according to the invention comprises: - an electric motor (30) designed to provide mechanical energy for each of the actuating devices; - an electronic control unit (60) for the electric motor; and - at least one switching device (50) interposed between the motor and the actuating devices, the switching device or devices allowing the mechanical energy provided by the electric motor to be distributed selectively to one of the actuating devices.