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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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