INTERNAL COMBUSTION GAS TURBINE Russian patent published in 1995 - IPC

FIELD: engine engineering. SUBSTANCE: rotor 3 with combustion chambers 4 is mounted inside the housing of the gas turbine provided with branch pipes for discharging exhaust gases 2. The rotor is mounted on shaft 5. Shaft 5 is hollow. Gas distributing collector 7 is mounted with a spaced relation inside hollow shaft 5. The collector is provided with passageways 8 and 9 for supplying gasify fuel components. Openings 6 for supplying fuel components to the combustion chamber from the supplying passageways are opposite to the combustion chambers inside the hollow shaft. Combustion chambers 4 are rigidly secured to shaft 5 and made up as vanes of axial compressor. The branch pipes for discharging exhaust gases are arranged inside housing 1 uniformly with an angle step being equal to the step of combustion chambers 4 mounted on the rotor of housings. Electric contacts of the ignition system are arranged on the branch pipes for discharging exhaust gases in faces abutting against the faces of the combustion chambers. One-half number of supplying branch pipes 8 is in communication with the fuel supplying system (hydrogen, methane). The remainder passageways 9 are in communication with the branch pipes for supplying working fluid (oxygen, air). Shaft 5 is rigidly secured to the shaft of the electric generator which energizes the transmission engine of a vehicle. EFFECT: enhanced efficiency. 1 dwg