GAS-TURBINE ENGINE

A power gas-turbine engine with two-support rotor realizing Braiton cycle and including compressor 1, combustion chamber 2, turbine 3 driving the compressor 1, and through reducer 4 û electric generator, where the drive of the electric generator is performed from the side of the compressor and the gas outlet from turbine is axial additionally comprises a reducer 4 and a power body. The compressor 1 is arranged centrifugal, the outlet branch pipe of the diffuser of this one is turned to the side from the mixers of the fire pipes, the rotor of the turbo-compressor is assembled, of drum-disc type, is comprises a console drum section 5, a drum-disc section 6, a disc of centrifugal section 7, a drum-disc section of the turbine 8. Strength of the stator is provided by the body of the compressor 2 and the turbine 3, and the outer power body 9 comprising of connected to each other front cone 10, cylindrical insert 1, back cone 12 surrounding the compressor 1 and the turbine 3, in the upper part it is connected to the body of external two-pipe combustion chamber 2.