INTERNAL COMBUSTION GAS TURBINE Russian patent published in 2001 - IPC

Abstract RU 2164610 C1

FIELD: power engineering; power generating turboplants. SUBSTANCE: turbine has housing, hollow shaft and axle with feed channels, ignition, system, fuel mixture preparation system with ejector and internal combustion chambers. Rotors with internal combustion chambers are installed on shaft. Internal combustion chambers are arranged at equal angles relative to each other. Fan impellers are placed between chambers. EFFECT: increased efficiency, smoothing down angular velocity fluctuations of turbine shaft. 3 dwg

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RU 2 164 610 C1

Authors

Jakovlev V.A.

Dates

2001-03-27Published

1999-06-23Filed