FIELD: engines and pumps.
SUBSTANCE: invention relates to area aviation engine engineering and can be used in electronic-hydro mechanical systems of automatic control (ACS) of gas turbine engines (GTE). The invention consists in that the fuel system incorporates a high-pressure electrically-driven centrifugal pump, while the metering mechanism is made in the form of electrically-driven throttling unit.
EFFECT: higher reliability of the engine.
1 dwg
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