发明名称 ガスタービン設備、及びその燃料温度管理方法
摘要 <p><P>PROBLEM TO BE SOLVED: To prevent liquefaction of gas fuel, even when gas composition of the gas fuel varies which is supplied to a combustor of a gas turbine. <P>SOLUTION: A facility includes: an auxiliary fuel heater 15 for heating the gas fuel flowing in a fuel pipe 10; a thermometer 25 for detecting a temperature of the gas fuel; a densitometer 26 for detecting the density of the gas fuel; and a heat controller 20 for driving and controlling the auxiliary fuel heater 15 so that a temperature detected by the thermometer 25 is higher than a dew point temperature, which is determined in accordance with the density detected by the densitometer 26, of the gas fuel under the environment of an inlet of the combustor 3. <P>COPYRIGHT: (C)2013,JPO&INPIT</p>
申请公布号 JP5787651(B2) 申请公布日期 2015.09.30
申请号 JP20110154783 申请日期 2011.07.13
申请人 发明人
分类号 F02C7/224;F02C7/22 主分类号 F02C7/224
代理机构 代理人
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