发明名称 GAS TURBINE COMBUSTOR BYPASS VALVE CONTROLLING METHOD
摘要 PURPOSE:To contrive to decrease NOx producing as least as possible and perform the stable combustion by a method wherein an air pressure in the casing of a combustor and a generator output are measured and calculated, then a fuel-air ratio at the burning part in the gas turbine combustor is controlled. CONSTITUTION:The air pressure P2 in the casing of a gas turbine combustor and a generator output Lgen are measured. A factor F(P2) is calculated based on the air pressure P2. In a calculating device 17, alpha=Lgen/F(P2) is calculated based on the air pressure P2 and the generator output Lgen. In a factor setting device 18, a bypass valve open degree setting signal CSO is set for the alpha calculated by the calculating device 17. The bypass valve open degree is controlled by the signal CSO.
申请公布号 JPS6196333(A) 申请公布日期 1986.05.15
申请号 JP19840218886 申请日期 1984.10.18
申请人 MITSUBISHI HEAVY IND LTD 发明人 FUKUE ICHIRO;AOYAMA KUNIAKI
分类号 F02C9/18;F23R3/26;F23R3/42 主分类号 F02C9/18
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