发明名称 |
BURNER AND GAS TURBINE COMBUSTOR |
摘要 |
A burner is provided that has high flame stability and reduces NOx emissions. In the burner, air holes of an air hole member have a central axis inclined relative to a burner central axis. The leading end portion of a first fuel nozzle is configured to be able to suppress turbulence of air-flow flowing on the outer circumference side of the first fuel nozzle. The tip of the first fuel nozzle is located on a fuel jetting-out directional downstream side of the inlet of the fuel hole. The tip of the second fuel nozzle is located on a fuel jetting-out directional downstream side of the air hole inlet.
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申请公布号 |
US2009173075(A1) |
申请公布日期 |
2009.07.09 |
申请号 |
US20080323654 |
申请日期 |
2008.11.26 |
申请人 |
MIURA KEISUKE;INOUE HIROSHI;KOYAMA KAZUHITO;SAITO TAKEO;DODO SATOSHI |
发明人 |
MIURA KEISUKE;INOUE HIROSHI;KOYAMA KAZUHITO;SAITO TAKEO;DODO SATOSHI |
分类号 |
F23D14/02;F02C7/22 |
主分类号 |
F23D14/02 |
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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