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

FIELD: mechanical engineering; gas-turbine engines.

SUBSTANCE: proposed gas-turbine engine has body, turbine shaft fitted in body, combustion chamber with space formed by housing, fire tube with burning zone and mixing zone, igniter and fuel feed system. Space formed by housing and front part of fire tube are sealed. System to feed fuel is made for delivery and atomizing of water in housing space and for delivery and atomizing of mixture of electrolyte (water solution of electrolyte) and fuel through nozzle with cavitator into arc burning zone. Igniter is made in form of arc electrodes made for delivery of direct current, striking and extinction of arc and with possibility of dissociation, ionization, ignition and turning into plazma of vapor mixture passing through zone of arc burning. Electrodes are installed in fire tube. One of electrodes is made movable at arc striking, and the other is made conical and provided with conical channel.

EFFECT: increased economy and ecological efficiency of engine.

2 cl, 1 dwg