FIELD: engines and pumps.
SUBSTANCE: system of an aircraft gas turbine start-up comprises a hydrogen-oxygen generator to produce superheated steam, which is either directly supplied into the gas turbine to spin it to a rotation speed, which will be sufficient to produce such an extent of air compression, which ensures the gas turbine operation on fuel, or the superheated steam is supplied into the compressed air generator to produce compressed air to be supplied into the compressed air system.
EFFECT: invention makes it possible to facilitate the gas turbine start-up.
4 cl, 1 dwg
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