GAS-TURBINE ENGINE Russian patent published in 2007 - IPC F02K3/00 

FIELD: mechanical engineering.

SUBSTANCE: proposed gas-turbine engine has compressor, combustion chamber, turbine and fuel supply system. said fuel supply system is made for delivery of fuel into combustion chamber and delivery of electrolyte (water solution) of electrolyte through nozzle with cavitator to compressor suction. Combustion chamber is connected with electrolyzer whose electrodes are made for decomposition of water at passing of direct current through electrolyte and enrichment of fuel-air mixture with hydrogen and oxygen and they are installed in separate housing. compressor is made for delivery of air enriched by electrolyte through electrolyzer into combustion chamber.

EFFECT: increased economy and improved ecological efficiency.

2 cl, 1 dwg