发明名称 GAS TURBINE SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a gas turbine system capable of effectively reducing NO<SB>X</SB>generated in a gas turbine without causing trouble in turbine cooling so as to achieve higher temperature, and improve plant efficiency. SOLUTION: High pressure air discharged from an air compressor 1 is supplied to a combustor 2, a turbine 3 is driven by high-temperature and high-pressure combustion gas generated by combustion in the combustor 2 with fuel that is separately supplied, and heat of exhaust gas discharged from the turbine 3 is recovered by an exhaust gas boiler 4 in this gas turbine system. An exhaust gas compressor 8 is provided to compress part of exhaust gas after heat recovering in the exhaust gas boiler 4. High-pressure exhaust gas discharged from the exhaust gas compressor 8 is supplied to the combustor 2. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004108147(A) 申请公布日期 2004.04.08
申请号 JP20020267704 申请日期 2002.09.13
申请人 MITSUBISHI HEAVY IND LTD 发明人 ISHIGURO TATSUO;BANDAI SHIGEMI;TANAKA KATSUNORI
分类号 F01K23/10;F02C3/30;F02C6/18;F02C7/16;F02C7/18;F02C7/32;F02C7/36;(IPC1-7):F02C3/30 主分类号 F01K23/10
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