发明名称 |
TURBOMACHINE COMBUSTOR ASSEMBLY AND METHOD OF OPERATING A TURBOMACHINE |
摘要 |
<p>A turbomachine combustor assembly includes a combustor body having a combustor outlet, and a combustion liner arranged within the combustor body. The combustion liner defines a combustion chamber. An injection nozzle is arranged within the combustor body upstream from the combustion chamber. The injection nozzle is configured and disposed to deliver a first fluid toward the combustion chamber. A fluid module is mounted to the combustor body downstream from the combustion chamber. The fluid module includes a fluid module body that defines a fluid zone, a first injector member mounted to the fluid module body and configured to deliver a second fluid into the fluid zone at a first orientation, and a second injector member mounted to the fluid module body and configured to deliver a third fluid into the fluid zone at a second orientation that is distinct from the first orientation.</p> |
申请公布号 |
EP2780636(A1) |
申请公布日期 |
2014.09.24 |
申请号 |
EP20110855268 |
申请日期 |
2011.11.17 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SLOBODYANSKIY, LLYA ALEKSANDROVICH;STRYAPUNIN, SERGEY ALEKSANDROVICH;TRETYAKOV, DMITRY VLADLENOVICH |
分类号 |
F23R3/34 |
主分类号 |
F23R3/34 |
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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