发明名称 |
GAS TURBINE SYSTEM CONTROL DEVICE AND METHOD |
摘要 |
<p>PROBLEM TO BE SOLVED: To provide a gas turbine system control device and a gas turbine system control method which detect performance deterioration of a plant due to aged deterioration and automatically correct the performance deterioration.SOLUTION: The gas turbine system control device supplies exhaust of a gas turbine combusting fuel with compressed air to a device located at a downstream side thereof through an exhaust duct and controls a fuel amount in a manner that adjusts a gas turbine outlet exhaust temperature to a predetermined value. The gas turbine system control device comprises: an adjustment function section which controls the gas turbine outlet exhaust temperature to the predetermined value; an exhaust temperature correction section which corrects the gas turbine outlet exhaust temperature to be input to the adjustment function section; and a correction condition confirmation section which detects that a temperature difference between the gas turbine outlet exhaust temperature and an inlet exhaust temperature of a downstream device exceeds a predetermined temperature difference. The gas turbine system control device corrects the gas turbine outlet exhaust temperature in a manner that curbs an increase therein to be input to the adjustment function section when the temperature difference exceeds the predetermined temperature difference.</p> |
申请公布号 |
JP2015001215(A) |
申请公布日期 |
2015.01.05 |
申请号 |
JP20130127270 |
申请日期 |
2013.06.18 |
申请人 |
MITSUBISHI HITACHI POWER SYSTEMS LTD |
发明人 |
SASAKI SHOHEI;MISONO KOICHI |
分类号 |
F02C9/28;F02C9/00 |
主分类号 |
F02C9/28 |
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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