发明名称 GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To provide a gas turbine performing turndown operation with low emission by a simple system while ensuring reliability of the gas turbine. SOLUTION: This gas turbine 1 includes: a compressor 2 compressing air used for combustion; a combustion section 3 injecting fuel to the compressed air in order to perform combustion and generating high-temperature combustion gas; a turbine section 4 rotatively driven by the combustion gas; and a moving blade cooling system 6 bleeding a part of the compressed air as cooling air and introducing the cooling air to the insides of moving blades belonging to a plurality of stages composing the turbine section 4. The moving blade cooling system 6 is provided with an adjustment section 63 adjusting the flow rate of the cooling air flowing in the inside. The flow rate of the cooling air flowing in the moving blade cooling system 6 during operation at a load lower than the full load is higher than the flow rate of the cooling air during operation at the full load. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2011137390(A) 申请公布日期 2011.07.14
申请号 JP20090296157 申请日期 2009.12.25
申请人 MITSUBISHI HEAVY IND LTD 发明人 YOSHIOKA SHINICHI;IWASAKI YOSHIFUMI;HAGI NAOKI;TAKAHASHI TATSUJI
分类号 F02C7/18;F01D25/12;F02C9/18 主分类号 F02C7/18
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