GAS-TURBINE ENGINE Russian patent published in 2006 - IPC F02C3/28 

FIELD: mechanical engineering; gas-turbine engines.

SUBSTANCE: proposed gas-turbine engine contains housing with fitted-in shaft, compressor, combustion chamber, turbine and fuel preparation and delivery system. Housing is provided with cover sealing its inlet. Fuel preparation and delivery system is made in form of electrolyzer consisting of electrodes to which direct current is supplied and installed before compressor in sealed part of housing and of electrodes formed by delivery of direct current to guide and working blades of compressor. Pumping device of fuel preparation and delivery system provides delivery and atomizing of electrolyte (water solution of electrolyte) through nozzle furnished with cavitator, in electrolyzer where electrolysis of water takes place under action of direct current passing through electrolyte. Compressor is made for building vacuum in sealed part of housing and compression and delivery of gas mixture into combustion chamber.

EFFECT: reduced consumption of fuel, no adverse effect on environment.

2 cl, 1 dwg