发明名称 METHOD FOR DETERMINING THE OF THE GAS-DYNAMIC STABILITY FACTOR OF A GAS-TURBINE COMPRESSOR IN OPERATION CONDITIONS
摘要 The proposed method for determining the of the gas-dynamic stability factor of a gas-turbine compressor in operation conditions consists in determining the performance an the critical stability of the compressor by its rotation frequency and thermodynamic parameters, measuring the actual flow of air passing through the compressor and air pressure at the outlet of the compressor.
申请公布号 UA13488(U) 申请公布日期 2006.04.17
申请号 UA20050005246U 申请日期 2005.06.02
申请人 NATIONAL AVIATION UNIVERSITY 发明人 VOLIANSKA LARYSA HEORHIIVNA;KINASCHUK IHOR FEDOROVYCH;KIRCHU FEDIR IVANOVYCH;PANIN VLADYSLAV VADYMOVYCH
分类号 G01M15/14;(IPC1-7):G01M/14 主分类号 G01M15/14
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