GAS TURBINE ENGINE Russian patent published in 2015 - IPC F02C3/20 F02C3/34 

FIELD: engines and pumps.

SUBSTANCE: this engine comprises housing, cover sealing the engine inlet, electrolyte feed system composed of the nozzle with cavitator, compressor and turbine shaft arranged in said housing, electrolyser-cavitator and local channel contraction with central body. Said electrolyser-cavitator is sealed in separate case connected with combustion chamber to feed pressurized gas mix downstream of compressor via electrolyser-cavitator with central; body to combustion chamber with igniter. Combustion chamber outlet is provided with gas flow separator including supersonic nozzle, outer and inner coaxial tubes and channel to return subsonic flow back, into combustion chamber.

EFFECT: higher efficiency.

2 dwg