发明名称 |
Fuel nozzle for a turbomachine |
摘要 |
A turbomachine includes a compressor, a turbine, and a combustor operatively connected to the turbine. The turbomachine further includes a cap member mounted to the combustor. The cap member includes a first surface and a second surface. A combustion chamber is defined within the combustor. An injection nozzle is supported at the second surface of the cap member. The injection nozzle includes a first end that extends through an inner flow path to a second end. The first end is configured to receive an amount of a first fluid and the second end is configured to receive an amount of a second fluid. A mixture of the first and second fluids is discharged from the second end of the injection nozzle. |
申请公布号 |
US8161750(B2) |
申请公布日期 |
2012.04.24 |
申请号 |
US20090355263 |
申请日期 |
2009.01.16 |
申请人 |
SIMMONS SCOTT ROBERT;THOMAS STEPHEN ROBERT;GENERAL ELECTRIC COMPANY |
发明人 |
SIMMONS SCOTT ROBERT;THOMAS STEPHEN ROBERT |
分类号 |
F02C1/00 |
主分类号 |
F02C1/00 |
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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