GAS COMPRESSOR UNIT Russian patent published in 2017 - IPC F02C3/20 F02C6/18 

Abstract RU 2610631 C1

FIELD: power industry.

SUBSTANCE: gas compressor unit comprising an air path comprising, in turn, an air intake, a compressor, a combustin chamber, a gas turbine, a shaft connecting the compressor and the gas turbine, a free turbine connected to the gas compressor and a fuel gas supply system to the combustion chamber with a fuel line. The fuel gas supply system comprises a water electrolyzer and a mixer of hydrogen, oxygen and fuel gas, located in front of the combustion chamber. A water supply system is connected to the mixer.

EFFECT: increase fuel combustion efficiency in the gas turbine engine used as the drive of the gas compressor unit, improvement of its specific characteristics and reducing the emission of harmful substances.

18 cl, 24 dwg

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RU 2 610 631 C1

Authors

Bolotin Nikolaj Borisovich

Dates

2017-02-14Published

2015-12-14Filed