INTERNAL COMBUSTION TURBO ENGINE Russian patent published in 2019 - IPC F02B75/00 

Abstract RU 2677914 C1

FIELD: turbines or turbomachines.

SUBSTANCE: invention relates to rotary turbo engines. Combustion chamber passes into a conical working chamber, where the expanding gas, passing through it, contracts, picks up speed and, leaving a powerful, concentrated stream directed to the center of the blades, rotates the turbine and the engine shaft rigidly connected to it. Chambers uniformly installed in the zone of rotation of the turbine are filled with the combustible mixture under pressure created by the compressor, and then alternately opened by the turbine making a revolution with the simultaneous explosion of the combustible mixture. Thus, for one revolution of the turbine in the six-dimensional engine version, six working emissions occur, multiplying the engine's performance.

EFFECT: invention is aimed at improving the efficiency of the engine.

6 cl, 6 dwg

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RU 2 677 914 C1

Authors

Sofronov Anatolij Ivanovich

Dates

2019-01-22Published

2018-04-10Filed