Abstract
The design scheme of the turboimpact high pressure fuel gas separator for gas turbine units has been developed. The experimental investigations of the efficiency of the compressed gases separators for gas turbine units with turboimpact and coagulating purification stages are carried out. The hydrodynamic separator characteristics at an air flow rate of 30 – 150 m3/h are obtained. The experiments confirmed the high values of the total purification efficiency coefficients of the studied separators which reach 90,0 – 99,8 %. On the basis of results of investigations, the recommendations for designing the flow area of compressed gases turboimpact separators for gas turbine units are developed.
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