FIELD: turbines or turbomachines.
SUBSTANCE: twin-shaft gas turbine engine is made of two parts of the body. In the first part of the housing are located the input device, the combustion chamber, the shaft with the rotors of the turbine and the centrifugal compressor, in the second part – the second shaft with the rotor of the traction turbine and exhaust pipes according to the number of nozzle windows of the combustion chambers. Between the turbines is located guide apparatus.
EFFECT: invention is aimed at improving efficiency and power.
1 cl, 1 dwg
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