Exhaust gas recirculation system with variable geometry turbine and bypass venturi assembly
    4.
    发明授权
    Exhaust gas recirculation system with variable geometry turbine and bypass venturi assembly 有权
    具有可变几何涡轮机和旁路文丘里管组件的废气再循环系统

    公开(公告)号:US06609373B2

    公开(公告)日:2003-08-26

    申请号:US10025655

    申请日:2001-12-19

    IPC分类号: F02B3344

    摘要: An internal combustion engine, particularly suitable for use in a work machine, is provided with an exhaust manifold, a turbocharger, and a bypass venturi assembly. The turbocharger includes a turbine and a compressor, with the turbine having a variable geometry inlet coupled with the exhaust manifold, and the compressor having an outlet. The bypass venturi assembly includes a housing having an outlet, a combustion air inlet and an exhaust gas inlet. The combustion air inlet is coupled with the compressor outlet. The exhaust gas inlet is coupled with the exhaust manifold. A center piece is positioned within the housing and is in communication with the combustion air inlet. The center piece defines a combustion air bypass section therein. A combustion air bypass valve is positioned in association with the combustion air bypass section. The exhaust gas valve is positioned in association with the exhaust gas inlet. The variable geometry inlet of the turbine allows the pressure ratio of the compressed combustion air to be varied, thereby improving the mixing efficiency of the exhaust gas with the combustion air.

    摘要翻译: 特别适用于作业机械的内燃机设置有排气歧管,涡轮增压器和旁路文氏管组件。 涡轮增压器包括涡轮机和压缩机,涡轮机具有与排气歧管连接的可变几何入口,并且压缩机具有出口。 旁路文氏管组件包括具有出口,燃烧空气入口和废气入口的壳体。 燃烧空气入口与压缩机出口连接。 排气入口与排气歧管连接。 中心件位于壳体内并与燃烧空气入口连通。 中心件在其中限定燃烧空气旁通部分。 燃烧空气旁通阀与燃烧空气旁路部分相关联地定位。 排气阀与排气入口相关联地定位。 涡轮机的可变几何形状入口允许压缩的燃烧空气的压力比改变,从而提高废气与燃烧空气的混合效率。