发明名称 OPERATING METHOD OF COMPOSITE CYCLE-GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To lower the NOx emitting material so as to improve the efficiency and output by using a multi-stage compressor having a specified pressure ratio so as to compress the inlet air, and supplying the nearly all compressed air to a combustion device so as to generate the gaseous combustion product, and supplying this gaseous combustion product to a turbine for discharge. SOLUTION: Air from a compressor 12' is discharged to several combustors 36 provided around a gas turbine rotor 14' in the circumferential direction. After the combustion, the gas obtained through the combustion is used so as to drive a turbine 20'. The turbine 20' has hour wheels 38, 40, 42, 44, and these are set on a gas turbine rotor 14', and each wheel includes buckets or vanes 54, 56, 58, 60. As an operation parameter, instead of raising the exhaust temperature of the turbine, a higher pressure ratio of the compressor, namely, the pressure ratio at about 23:1 is selected so as to restrict the temperature effect, and the NOx emitting material is reduced so as to improve the efficiency and the output.
申请公布号 JPH094466(A) 申请公布日期 1997.01.07
申请号 JP19960078607 申请日期 1996.04.01
申请人 GENERAL ELECTRIC CO <GE> 发明人 ROJIYAA UIRIAMU SUKONUORUDO;YAIRAI RAMACHIYANDORAN;JIYOOJI DABURIYUU SUKIPAA JIYUNIA
分类号 F01K23/10;F02C6/00;F02C6/18;F02C7/16;(IPC1-7):F02C7/16 主分类号 F01K23/10
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