FIELD: gas-turbine engines. SUBSTANCE: transport two-shaft and three-shaft gas-turbine engines have an intake with an air cleaner made in the form of a gauze, stator with a coolant jacket, rotor of centrifugal compressor with a turbine and supports. The turbocompressor rotor is centrifugal, with one hub, on one disk, and the turbine is removed to the periphery. The power turbine is centrifugal, multistage, nozzle windows according to the number of engine combustion chambers are made on the stator in circumference. EFFECT: enhanced economical efficiency at manufacture. 4 cl, 6 dwg
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