发明名称 |
MULTIFUEL GAS TURBINE COMBUSTOR |
摘要 |
To provide a multifuel gas turbine combustor capable of combusting gases containing hydrogen in a high concentration with a low NOx while maintaining a low emission performance brought about by the pre-mixture combustion in the main burner, the gas turbine combustor includes a main burner (12) for supplying to and combusting a premixed gas (M), containing a first fuel (F1), within a first combustion region (S1) of a combustion chamber (10), and a supplemental burner (20) for supplying to and combusting a second fuel (F2) of a composition different from that of the first fuel (F1) within a second combustion region (S2) defined downstream of the first combustion region (S1) within the combustion chamber (10). The first fuel (F1) is of a hydrocarbon system and the second fuel (F2) is a gas containing hydrogen in a concentration exceeding the stable combustion limiting concentration of the hydrogen. |
申请公布号 |
US2016033131(A1) |
申请公布日期 |
2016.02.04 |
申请号 |
US201414421065 |
申请日期 |
2014.06.12 |
申请人 |
KAWASAKI JUKOGYO KABUSHIKI KAISHA |
发明人 |
OGATA Masahiro;ODA Takeo;KINOSHITA Yasuhiro |
分类号 |
F23R3/28;F23R3/36;F02C3/22;F23R3/34 |
主分类号 |
F23R3/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
Hyogo JP |