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
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