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

Abstract RU 2305199 C1

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. Axial-flow compressor with guide and working blades is provided with electrolyzer. Electrodes of electrolyzer provide free passing of air flow and dissociation decomposition of water naturally present in air into hydrogen and oxygen and water electrolyte (water solution of electrolyte) introduced additionally into air flow under action of electric current. Electrolyzers are found on guide and working blades of axial-flow compressor.

EFFECT: improved operating efficiency of gas-turbine engine.

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RU 2 305 199 C1

Authors

Vesengiriev Mikhail Ivanovich

Dates

2007-08-27Published

2006-02-20Filed