发明名称 |
GAS TURBINE COMBUSTOR |
摘要 |
Provided is a gas turbine combustor capable of reducing the size of a low-temperature air layer of pilot air formed between a pilot flame and a premixed flame and of improving the flame stability of the premixed flame. A gas turbine combustor 1A, which is provided with a pilot burner 3 that is provided at the center portion of a combustor main body formed in a cylindrical shape to form a pilot flame, and a plurality of main burners 10 arranged so as to surround the outer periphery of the pilot burner 3 to form a premixed flame, includes, as the ignition improving part, a channel blocking member 20 that reduces the size of the low-temperature air layer of the pilot air formed between the pilot flame and the premixed flame. |
申请公布号 |
EP2187127(A4) |
申请公布日期 |
2014.08.13 |
申请号 |
EP20080863965 |
申请日期 |
2008.12.19 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
INOUE, KEI;SAITO, KEIJIRO;MATSUMURA, YOSHIKAZU;NAKAMURA, SOSUKE |
分类号 |
F23R3/14;F23R3/30;F23R3/34 |
主分类号 |
F23R3/14 |
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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