TURBOJET ENGINE Russian patent published in 2000 - IPC

FIELD: power engineering, aircraft industry, transport. SUBSTANCE: engine has stator, hollow shaft, compressor with gas turbine and combustion chambers installed before compressor, fuel system including fuel and compressed air supply channels, exhaust branch pipes and spark contacts. Exhaust branch pipes are furnished with valves and are installed on stator at pitch equal to combustion chamber angular pitch. Spark contacts are installed at places of butt joining of internal combustion chambers with exhaust branch pipes. Fuel system is furnished with injector and methane bottle. EFFECT: increased efficiency. 2 dwg