发明授权
US08919096B2 System for controlling a plurality of functions of a turbojet engine 有权
用于控制涡轮喷气发动机的多个功能的系统

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.
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