发明名称 Combustors for use in turbine engine assemblies
摘要 An engine assembly includes a scroll assembly including an inlet, an outlet, an inner section, and an outer section. Each of the inner section and the outer section extend between the inlet and the outlet with the outer section being longer than the inner section. The engine assembly further includes a combustor having an entrance for receiving fuel to be mixed with air and combusted in the combustor, an exit coupled to the inlet of the scroll assembly for delivering the combusted air-fuel mixture, including a hot stream, thereto, and a wall coupled between the entrance and the exit and including a plurality of dilution holes therethrough for deflecting the hot stream toward the outer section of the scroll assembly.
申请公布号 US7984615(B2) 申请公布日期 2011.07.26
申请号 US20070769077 申请日期 2007.06.27
申请人 HONEYWELL INTERNATIONAL INC. 发明人 WOODCOCK GREGORY O.;CRITCHLEY IAN L.
分类号 F02C1/00;F02G3/00 主分类号 F02C1/00
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