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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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