ON THE POSSIBILITY OF IMPROVING THE DESIGN OF A GAS TURBINE DRIVEN COMPRESSOR UNIT BASED ON AN INDEPTH THERMODYNAMIC ANALYSIS OF ITS WORKING PROCESS
Abstract
In-depth thermodynamic analysis of the gas turbine compressor unit of hydrocarbon gas and analysis of possible ways to improve its efficiency. The potential for reducing existing exergy losses in the elements has been determined. Possible design improvements are proposed for individual unit systems and operating modes, and their effect on the efficiency of the unit is shown.
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