发明名称 CONTROL DEVICE FOR GAS TURBINE, GAS TURBINE, AND CONTROL METHOD FOR GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To shorten starting time while maintaining safety.SOLUTION: A gas turbine comprises a compressor for producing compressed air by compressing air taken from an air inlet, a combustor for producing a combustion gas by burning fuel with the compressed air, and a turbine driven by the combustion gas. The control device 40 for a gas turbine comprises a rotational acceleration determining part 48 for determining the maximum rotational acceleration feasible by the turbine based on a safety index showing the relationship between damage of the appliances comprising the gas turbine and the rotational acceleration of the turbine, and an acceleration fuel-air ratio determining part 50 for determining the fuel-air ratio of the combustor for accelerating the turbine by the rotational acceleration determined by the rotational acceleration determining part 48.
申请公布号 JP2013221423(A) 申请公布日期 2013.10.28
申请号 JP20120091871 申请日期 2012.04.13
申请人 MITSUBISHI HEAVY IND LTD 发明人 YAMAMOTO KEISUKE;AZUMA KAZUYA;SONODA TAKASHI
分类号 F02C9/28;F01D17/00;F02C7/26 主分类号 F02C9/28
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