发明名称 |
GAS TURBINE COMBUSTOR, CONTROL DEVICE FOR GAS TURBINE COMBUSTOR AND ABNORMALITY DETECTION METHOD FOR GAS TURBINE COMBUSTOR |
摘要 |
PROBLEM TO BE SOLVED: To provide a means for detecting an abnormality and protecting a combustor or a gas turbine with a simple means even when an abnormality occurs for example, a part of a plurality of fuel nozzles or a part of a plurality of fuel jetting ports which are provided in a gas turbine combustor, and a section where the plurality of fuel jetting ports or the like are branched at the downstream of a fuel flow rate control valve of one fuel system.SOLUTION: A means for detecting a difference pressure between fuel pressure at the downstream of a fuel flow rate control valve provided in a fuel system and pressure in a combustor is provided. A means for specifying a fuel flow rate flowing in the fuel system is also provided. A divider for calculating ratio of difference pressure signal of the fuel system and a fuel flow rate signal of the fuel system is provided. A comparator for determining a combustor abnormality based on a signal from the divider is included. |
申请公布号 |
JP2013241873(A) |
申请公布日期 |
2013.12.05 |
申请号 |
JP20120115181 |
申请日期 |
2012.05.21 |
申请人 |
HITACHI LTD |
发明人 |
KOGANEZAWA TOMOKI;ABE KAZUCHIKA;MIURA KEISUKE;SAITO TAKEO |
分类号 |
F02C9/00;F01D25/00;F02C7/00;F02C7/22;F02C9/26;F23R3/00;F23R3/28;F23R3/34 |
主分类号 |
F02C9/00 |
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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