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http://dx.doi.org/10.5293/KFMA.2003.6.3.036

Performance degradation due to compressor fouling of an industrial gas turbine operating at design point condition  

Seo, J.S. (서울대학교 기계항공공학부 대학원)
Sohn, J.L. (서울대학교 기계항공공학부)
Kim, J.H. (한국항공우주연구원 터보기계연구그룹)
Kim, T.S. (인하대학교 기계공학부)
Ro, S.T. (서울대학교 기계항공공학부)
Publication Information
Abstract
Operating performance of industrial gas turbines in combined cycle power plants depends upon atmospheric conditions. Compressor fouling caused by airborne particles in the atmosphere and their adhesions on compressor blades is one of critical phenomena related to the performance degradation of industrial gas turbines. Compressor fouling provokes increase of pressure loss in inlet duct, decrease of mass flow rate of intake air and decrease of compressor stage efficiency. In this study, impacts of compressor fouling on the performance of an industrial gas turbine operating at design point condition are investigated analytically. As results, it is found that the reduction of produced power with decreased mass flow rate of intake air caused by narrowed flow area by the adhesion of airborne particles on compressor blades is the most dominant impact on the gas turbine performance by the compressor fouling phenomena.
Keywords
Gas turbine; Compressor; Fouling; Performance degradation; Mass flow rate; Stage efficiency; Power; Thermal efficiency;
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