Radial compressor, particularly for an exhaust gas turbocharger of an internal combustion engine
    49.
    发明授权
    Radial compressor, particularly for an exhaust gas turbocharger of an internal combustion engine 有权
    径向压缩机,特别是用于内燃机的废气涡轮增压器

    公开(公告)号:US08522549B2

    公开(公告)日:2013-09-03

    申请号:US12927869

    申请日:2010-11-27

    IPC分类号: F01D1/12 F04D29/44 F02B33/44

    摘要: In a radial compressor, particularly of an exhaust gas turbocharger of an internal combustion engine, having a compressor housing within which a compressor wheel is disposed for compressing air from an inflow channel of the compressor housing and directing the air to an outflow channel of the compressor housing, the compressor housing comprising a bypass channel having a first flow opening upstream of an axial compressor wheel inlet and a second flow opening downstream of the compressor wheel inlet, the compressor housing is configured at least in a flow region upstream of the second flow opening in an asymmetric manner with regard to a rotational axis of the compressor wheel.

    摘要翻译: 在径向压缩机,特别是内燃机的排气涡轮增压器的径向压缩机中,具有压缩机壳体,压缩机叶轮设置在该压缩机壳体内,用于压缩来自压缩机壳体的流入通道的空气并将空气引导到压缩机的流出通道 所述压缩机壳体包括具有在轴向压缩机叶轮入口上游的第一流动开口和在所述压缩机叶轮入口下游的第二流动开口的旁通通道,所述压缩机壳体构造成至少在所述第二流动开口 相对于压缩机叶轮的旋转轴线以不对称的方式。

    Internal combustion engine comprising an exhaust gas turbocharger
    50.
    发明授权
    Internal combustion engine comprising an exhaust gas turbocharger 有权
    内燃机包括排气涡轮增压器

    公开(公告)号:US07934379B2

    公开(公告)日:2011-05-03

    申请号:US11651405

    申请日:2007-01-09

    IPC分类号: F02D23/00

    摘要: In an internal combustion engine comprising an exhaust gas turbocharger, including a turbine with at least two inlet passages arranged in the exhaust gas tract of the internal combustion engine, via which exhaust gas from the internal combustion engine can be supplied to a turbine wheel of the turbine, and a valve arrangement being arranged in to the exhaust gas tract to the turbocharger to control the supply of exhaust gas to the inlet passages of the turbine, a valve and turbine inlet passage configuration is selectable providing for a maximum braking power with low thermal load.

    摘要翻译: 在包括排气涡轮增压器的内燃机中,包括具有设置在内燃机的排气管道中的至少两个入口通道的涡轮机,通过该内燃机可以将来自内燃机的废气供应到涡轮机的涡轮机叶轮 涡轮机,以及阀装置,其布置在排气管道中,以连接到涡轮增压器,以控制向涡轮机的入口通道供应排气,阀和涡轮机入口通道配置可选择,提供具有低热能的最大制动功率 加载。