发明名称 Compressor blade monitoring system
摘要 A system 2 including: at least one computing device 120 configured to monitor a compressor blade 10 in a turbomachine 5 by: extracting time of arrival (TOA) data about the compressor blade 10 at a defined interval; correlating turbomachine operating conditions with the TOA data; extracting resonance data about the compressor blade 10 during startup or shutdown of the turbomachine 5, and extracting static deflection and tip clearance data about the compressor blade 10 during steady state operation of the turbomachine 5; creating a baseline compressor blade comparison level based upon the extracted resonance data, extracted static deflection and tip clearance data, and correlation between the turbomachine operating conditions and the TOA data; and iteratively extracting updated TOA data and performing the correlating, the extracting of the resonance data, static deflection and tip clearance data using the updated TOA data at the defined interval to create an updated baseline compressor blade comparison level. Corresponding computer program product with a program code executed by such a computing device.
申请公布号 EP2848776(A3) 申请公布日期 2015.03.25
申请号 EP20140184199 申请日期 2014.09.10
申请人 GENERAL ELECTRIC COMPANY 发明人 YU, LIJIE;ANSARI, ADIL;BADAMI, VIVEK VENUGOPAL;BLISS, JOHN THOMAS;CHADHA, RAHUL;GUPTA, RAJAN
分类号 F01D21/00;F01D17/00;F01D17/02;F01D17/04;F01D17/06;F01D17/08;F01D21/10;F01D21/14;F02C9/00;G05B23/02 主分类号 F01D21/00
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