发明名称 Gas turbine output learning circuit and combustion control device for gas turbine having the same
摘要 A gas turbine output learning circuit is configured to compute a current combustion gas temperature TIT at an inlet of a gas turbine by linear interpolation by use of two characteristic curves A and B respectively representing relations between a pressure ratio and an exhaust gas temperature in the cases of the combustion gas temperature at the inlet of the gas turbine at 1400° C. and 1500° C., then to compute ideal MW corresponding to this combustion gas temperature TIT at the inlet of the gas turbine by linear interpolation according to 1400° C.MW and 1500° C.MW (temperature controlled MW), and then to correct the 1400° C.MW and the 1500° C.MW so as to match the ideal MW with a measured gas turbine output (a power generator output).
申请公布号 US2007271024(A1) 申请公布日期 2007.11.22
申请号 US20070657132 申请日期 2007.01.24
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 FUJII KENTARO;TOYAMA KOZO
分类号 F02D28/00 主分类号 F02D28/00
代理机构 代理人
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