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

FIELD: mechanical engineering; gas-turbine engines.

SUBSTANCE: proposed gas-turbine engine contains intake unit, axial-flow compressor with guide and working blades, combustion chamber, fuel feed system, igniter, turbine and exhaust unit. Intake unit and axial-flow compressor with guide and working blades are provided with electrolyzers. Electrodes of electrolyzers provide free passing of air flow and dissociation decomposition of water naturally present in air into hydrogen and oxygen and water of electrolyte (water solution of electrolyte) introduced additionally into air flow under action of electric current supplied by carry-on dc current source. They are installed in intake unit and are made on guide and working blades of axial-flow compressor.

EFFECT: improved operating efficiency of engine.

1 dwg