INTERNAL COMBUSTION GAS TURBINE Russian patent published in 2000 - IPC

FIELD: power engineering; gas industry; transport engineering. SUBSTANCE: turbine has housing, rotor with hollow hub and shaft, internal combustion chambers limited by inner surfaces of gas nozzles with valves, and ignition system. Combustion chambers communicate with hub space and with branch pipe for delivery of fuel mixture thus forming a common channel at the end of which slotted header is installed. Header has fixed disk with through holes in form of Maltese cross and movable disk with similar through holes. Disks are installed for periodical alignment of holes. Movable disk has one spark contact, and fixed disk, four spark contacts arranged relative to each other at angular interval equal to 90 degrees. EFFECT: increased efficiency of turbine. 5 dwg