发明名称 GAS TURBINE FUEL GAS SYSTEM
摘要 PURPOSE:To improve reliability on control of a flow rate, by a method wherein, in a title fuel gas system using multiple fuel, a heat generating amount of fuel gas is detected, and in case there is a low heat generating amount, the fuel gas system is switched to a fuel feed system on the low flow rate side, and if a high heat generating amount, it is switched to a fuel feed system on the high flow rate side. CONSTITUTION:A heat generating amount detector 11, a switching valve 10, pressure regulating valves 1, flow rate control valves 2, and fuel gas manifolds 7 of 2 system rows, and a fuel nozzle 8 having two orifices different in size are located on a fuel gas feed system. In case mixture gas of gas C and gas D is used as the fuel gas, in a first system A, the fuel gas is set controllably in the range of the gas C of 100-50% and the gas D of 0-50%, and in a second system B, it is set controllably in a range of the gas C of 0-50% and the gas D of 50-100%. In case a heat generating amount detected by the heat generating detector 11 is low, the first system A is selectively switched by the switching valve 10, and in case high, the second system B is selectively switched by the switching valve 10.
申请公布号 JPS61210234(A) 申请公布日期 1986.09.18
申请号 JP19850050469 申请日期 1985.03.15
申请人 HITACHI LTD;HITACHI ENG CO LTD 发明人 USE SHINJI;HORI MICHIO
分类号 F02C9/40 主分类号 F02C9/40
代理机构 代理人
主权项
地址
您可能感兴趣的专利