发明名称 GAS TURBINE COMBUSTOR
摘要 PROBLEM TO BE SOLVED: To suppress discharge of unburned constituents and reduce NOx even if air and nitrogen are supplied to gasified gas in an operation load range of a gas turbine. SOLUTION: When the gasified gas 15 is jetted to a combustion chamber 8a from a fuel jet 24a, and combustion air 9a and nitrogen 13 in an air passage 9b are jetted to the combustion chamber 8a from a fluid swirling passage 24c, nitrogen is jetted out from a nitrogen jet 27a and a nitrogen jet 27b of a nitrogen jet nozzle 27 into the passage 9b, and the oxygen concentration in the air that passes through an air swirler 24 is raised, thereby, in a low loading condition, rendering the temperature of a flame 20b to be more than a given value and suppressing the unburned constituent concentration of the discharge gas. On the other hand, in a high loading condition, the temperature of the entire flame 20b can be lowered by mixing the nitrogen 13 supplied from a combustion air port 26a with combustion gas and thus generation of NOx is suppressed.
申请公布号 JP2002206741(A) 申请公布日期 2002.07.26
申请号 JP20010001364 申请日期 2001.01.09
申请人 HITACHI LTD;CENTRAL RES INST OF ELECTRIC POWER IND 发明人 KOIZUMI HIROMI;HAYASHI AKINORI;KOBAYASHI SHIGEYOSHI;HASEGAWA TAKEJI;HISAMATSU NOBORU
分类号 F23R3/06;F02C3/22;F02C3/30;F23R3/12;F23R3/26;F23R3/28;(IPC1-7):F23R3/06 主分类号 F23R3/06
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