GAS-TURBINE ENGINE Russian patent published in 2008 - IPC F02K3/00 

FIELD: mechanical engineering; gas-turbine engines.

SUBSTANCE: proposed gas-turbine engine has body with sealed compressor suction, combustion chamber with fire tube with burning zone, mixing zone, system of delivery and spraying of electrolyte (water solution of electrolyte) through nozzle with cavitator to compressor suction, igniter and turbine. Igniter is made in form of arc electrodes installed in combustion chamber with possibility of supplying direct current, striking and blowing out of arc, dissociating, ionization, igniting and turning vapors of electrolyte passing through zone of arc burning into plasma. One electrodes is made for displacement at striking of arc, and the other is made conical and provided with conical channel.

EFFECT: increased efficiency of engine.

2 cl, 1 dwg