发明名称 NOZZLE FOR A TURBOMACHINE
摘要 A turbomachine includes a compressor, a combustor operatively connected to the compressor, and an injection nozzle operatively connected to the combustor. The injection nozzle includes a main body having a first end section that extends to a second end section to define an inner flow path. The injection nozzle further includes an outlet arranged at the second end section of the main body, at least one passage that extends within the main body and is fluidly connected to the outlet, and at least one conduit extending between the inner flow path and the at least one passage.
申请公布号 US2010180600(A1) 申请公布日期 2010.07.22
申请号 US20090357638 申请日期 2009.01.22
申请人 GENERAL ELECTRIC COMPANY 发明人 LACY BENJAMIN PAUL;KRAEMER GILBERT OTTO;YILMAZ ERTAN;MELTON PATRICK BENEDICT
分类号 F02C7/22;B05B7/04 主分类号 F02C7/22
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