发明名称 |
Method and apparatus for monitoring the performance of a gas turbine system |
摘要 |
A method for monitoring performance of a gas turbine system comprises providing a plurality of combustor cans; placing a plurality of temperature sensors circumferentially around an exhaust plane of the plurality of combustor cans; operating the plurality of combustor cans while varying a plurality of gas turbine operating parameters, where exhaust gas issues from each combustor can of the plurality of combustor cans during operation; measuring temperature of the exhaust gas in the exhaust plane using the plurality of temperature sensors to obtain a plurality of individual temperature measurements; determining a correlation of the individual temperature measurements of exhaust gas temperature with corresponding individual combustor cans of the plurality of combustor cans issuing the exhaust gas; and developing a swirl model, where the model uses the correlation to predict swirl values in the exhaust plane as a function of the operating parameters.
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申请公布号 |
US2004148940(A1) |
申请公布日期 |
2004.08.05 |
申请号 |
US20030354824 |
申请日期 |
2003.01.30 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
VENKATESWARAN NARAYANAN;ASHOK SHAH MINESH;NORMAN BRUCE GORDON |
分类号 |
F02C9/00;F01D17/08;F02C9/20;F02C9/28;(IPC1-7):F02C1/00 |
主分类号 |
F02C9/00 |
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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