发明名称 |
METHOD FOR DIAGNOSING A GAS TURBINE |
摘要 |
The method involves using an intake mass flow of a gas turbine (1) as a parameter during the prediction of the additional power. A combustion chamber pressure loss or the pressure loss between an environment and a compressor inlet is determined as the input parameters for determining the intake mass flow of a turbine inlet pressure. Independent claims are included for the following: (1) a gas turbine system with multiple components having a gas turbine and a control system; and (2) a prognosis module for use in a gas turbine system. |
申请公布号 |
EP2257933(A1) |
申请公布日期 |
2010.12.08 |
申请号 |
EP20090725928 |
申请日期 |
2009.03.24 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
GROSSE-LAXZEN, ROLF;WERNER, KLAUS |
分类号 |
G07C3/00;F01D21/00 |
主分类号 |
G07C3/00 |
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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