发明名称 |
MULTI-FUEL-CAPABLE GAS TURBINE COMBUSTOR |
摘要 |
A multi-fuel-capable gas turbine combustor is provided which is able to sufficiently utilize various fuels having a characteristic deviating from a premixing characteristic range suitable for generating a premixed gas, even while maintaining favorable low-emission performance by premixed combustion. The gas turbine combustor includes: a main burner configured to supply a premixed gas containing a first fuel for premixing, to a first combustion region within a combustion chamber to cause premixed combustion; and a supplemental burner configured to supply a second fuel for reheating having a different composition from that of the first fuel, to a second combustion region at a location downstream of the first combustion region within the combustion chamber, to cause diffusion combustion. The first fuel has a premixing characteristic range suitable for generating a premixed gas. The second fuel has a characteristic deviating from the premixing characteristic range. |
申请公布号 |
EP2933561(A4) |
申请公布日期 |
2016.08.24 |
申请号 |
EP20130862678 |
申请日期 |
2013.12.13 |
申请人 |
KAWASAKI JUKOGYO KABUSHIKI KAISHA |
发明人 |
OGATA, MASAHIRO;ODA, TAKEO;KINOSHITA, YASUHIRO |
分类号 |
F23R3/36;F02C3/22;F02C3/24;F02C7/22;F02C7/228;F23R3/28;F23R3/34 |
主分类号 |
F23R3/36 |
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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