GAS TURBINE ENGINE Russian patent published in 2008 - IPC F02C3/20 

FIELD: engines and pumps.

SUBSTANCE: gas turbine engine comprises case and cover to seal an inlet into the case, compressor, combustion chamber, system for electrolyte/electrolyte water solution supply/ through a sprayer with cavitator, inflaming device, turbine and electrolyzer. The case inlet sealing cover is designed to facilitate adjusting of air intake into the engine. The electrolyte supply system provides the possibility to supply electrolyte via the sprayer with cavitator into the flow of air intake to the engine and to supply fuel into the combustion chamber. The electrolyzer is designed as a cavitator with a central body where direct electrical current from power supply runs to cavitator components; the electrolyzer is installed in an isolated case and tight proof connected to the combustion chamber, thus a gas mixture under pressure behind a compressor is supplied to the combustion chamber via that eloctrolyser. The purpose of the invention is to increase efficiency of an engine.

EFFECT: increase efficiency output of an engine.

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