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 into cover sealing its inlet. Fuel preparation and delivery system is made in form of electrolyzer with supply of direct current to guide and working blades of compressor. Pumping device and nozzle with cavitator of fuel preparation and delivery system are made to feed and atomize water solution of electrolyte in electrolyzer. Compressor is made for building vacuum in seal part of housing and decomposition of water into hydrogen and oxygen under action of direct current passing through electrolyte.

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

2 cl, 2 dwg