发明名称 |
Method for controlling fuel splits to gas turbine combustor |
摘要 |
A method for determining a target exhaust temperature for a gas turbine including: determining a target exhaust temperature based on a compressor pressure condition; determining a temperature adjustment to the target exhaust temperature based on at least one parameter of a group of parameters consisting of specific humidity, compressor inlet pressure loss and turbine exhaust back pressure; and adjusting the target exhaust temperature by applying the temperature adjustment.
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申请公布号 |
US2005114010(A1) |
申请公布日期 |
2005.05.26 |
申请号 |
US20030716454 |
申请日期 |
2003.11.20 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
HEALY TIMOTHY A.;SIMONS DERRICK W. |
分类号 |
F02C9/00;F02C9/28;F23N1/00;F23R3/34;(IPC1-7):G06F19/00 |
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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