FIELD: engines and pumps.
SUBSTANCE: invention relates to system for control over turbojet multiple various functions. Every said functions is associated with definite actuator. Said system comprises motor designed to feed mechanical power to every actuator, motor electronic control unit, and switch arranged between motor and actuators. Said switch serves to effect distribution mechanical power supplied by motor to one of actuators in selective manner.
EFFECT: lower costs, simplified design.
3 dwg
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