TWO-SHAFT GAS-COMPRESSOR UNIT FOR BOOSTER COMPRESSOR STATIONS Russian patent published in 2015 - IPC F04D25/00 

Abstract RU 2554670 C1

FIELD: oil and gas industry.

SUBSTANCE: gas-compressor unit includes a gas-turbine engine, a multiplier connected to it, having two power takeoff shafts and two compression stages in the form of a low pressure compressor and a high pressure compressor, which are connected with a process loop and each of which is connected to the corresponding power takeoff shaft.

EFFECT: improving vibration characteristics and efficiency of unit operation, simplifying a process flow diagram and excluding the need for use of additional equipment; providing symmetric load distribution to the multiplier.

3 cl, 1 dwg

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RU 2 554 670 C1

Authors

Minigulov Rafail' Minigulovich

Vasin Oleg Evgen'Evich

Bodnaruk Vasilij Vsevolodovich

Dates

2015-06-27Published

2014-05-30Filed