FIELD: engines and pumps.
SUBSTANCE: proposed method consists in feeding carbon fuel to compressor inlet. Said feed is accompanied with fuel feed into main combustion chamber reduced by amount of fuel fed to compressor inlet. Fuel consumption at compressor inlet does not exceed three percent of air consumption. Fuel nozzles mounted at compressor inlet can be directed towards airflow.
EFFECT: improved thrust, reduced fuel consumption of high-rpm gas turbine engines.
2 cl, 3 dwg
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