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

Abstract RU 2280182 C1

FIELD: mechanical engineering; gas-turbine engines.

SUBSTANCE: proposed gas-turbine engine contains housing with fitted-in shaft, compressor, combustion chamber with igniter, 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 installed with possibility of supply of direct current to its electrodes, free passing of electrolyte (water solution of electrolyte) through electrolyzer and products of water decomposition formed under action of direct current passing through electrolyte. Electrolyzer is installed before compressor in sealed part of housing. Pumping device and nozzle serve to deliver and atomize water solution of electrolyte in electrolyzer. Nozzle is furnished with cavitator made in form of local contraction of channel.

EFFECT: reduced consumption of fuel, adverse effect on environment.

3 cl, 2 dwg

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RU 2 280 182 C1

Authors

Vesengiriev Mikhail Ivanovich

Dates

2006-07-20Published

2005-01-11Filed