INTERNAL-COMBUSTION GAS ENGINE Russian patent published in 1998 - IPC

FIELD: engine manufacture. SUBSTANCE: gas turbine has casing, hollow-shaft rotor provided with fuel and working medium admission channels arranged in alternating manner, combustion chambers inserted between internal surfaces of gas nozzles and external surfaces made in the form of axial-flow compressor blades. Gas nozzles are mounted on casing at pitch equal to angular pitch of combustion chambers and carry valves and control gear. Electric contacts of combustion-chamber ignition system are provided at ends of propulsive nozzles. EFFECT: simplified design, reduced metal input, improved efficiency, facilitated maintenance in operation, provision for using environmentally friendly fuel. 1 dwg