发明名称 GAS TURBINE COMBUSTION SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a gas turbine combustion system capable of reducing the consumption of the existing fuel while preventing the fusion of a turbine. SOLUTION: In this gas turbine combustion system wherein the fuel is supplied to a combustor 9 to be combusted, and a turbine 4 is rotated by a high temperature gas current to drive a generator 21 and to obtain a specific power generation output, the combustor 9 is provided with a combustion burner A to which the fuel is supplied, a steam torch B to which the steam is supplied, and a blown gas burner C to which the blown gas is supplied, and the amount of steam of the steam torch B and the combustion of the combustion burner A are adjusted in combusting the blown gas to inhibit the rise of a temperature at a turbine inlet.
申请公布号 JP2003027964(A) 申请公布日期 2003.01.29
申请号 JP20010210920 申请日期 2001.07.11
申请人 KOMOSU:KK 发明人 MUNEYUKI ISATO
分类号 F01K23/10;C10L1/32;F01K25/00;F02C3/22;F02C3/30;F02C7/08;F02C9/28;F02C9/40;(IPC1-7):F02C9/40 主分类号 F01K23/10
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