FIELD: engines and pumps.
SUBSTANCE: turbojet two nacelle control system comprises two power supply control units. Each of the latter can convert electric power. Every said unit comprises means to high-voltage power to electromechanical drive of at least one drive input for every power supply control unit. System incorporates also one control unit to supply control instructions to power supply control units that differs in design and separated from the latter. Said separate unit comprises at least one control input to receive data from engine controllers and at least two drive outputs to be connected to drive inputs of power supply control units.
EFFECT: simplified certification of controller.
14 cl, 2 dwg
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