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    • 4. 发明申请
    • Asymmetric Split-Inlet Turbine Housing
    • 不对称分体式进气涡轮机壳体
    • US20100229551A1
    • 2010-09-16
    • US12401762
    • 2009-03-11
    • Ko-Jen WuJian Jun ZhangJames C. Elmslie
    • Ko-Jen WuJian Jun ZhangJames C. Elmslie
    • F02B33/40F04D29/42
    • F01D9/026F02B37/00F02B37/025F02B75/22F05D2220/40F05D2240/40F05D2250/51Y02T10/144
    • A turbine housing for a turbocharger for use in a reciprocating internal combustion engine includes a housing having a housing axis and configured to house a rotatable shaft having a turbine wheel disposed thereon. The housing includes a volute having a volute chamber disposed around the housing axis for receiving the turbine wheel. The volute has a first volute inlet providing a first flow path in fluid communication with the volute chamber and second volute inlet providing a second flow path in fluid communication with the volute chamber. The first volute inlet is circumferentially spaced about the housing axis from the second volute inlet by a phase angle α. The first volute inlet is also radially spaced about the housing axis from the second volute inlet, and may also be axially spaced from the second volute inlet along the housing axis.
    • 用于在往复式内燃机中使用的涡轮增压器的涡轮机壳体包括壳体,该壳体具有壳体轴线并且构造成容纳其上设置有涡轮机叶轮的可旋转轴。 壳体包括具有围绕壳体轴线设置用于接收涡轮机叶轮的蜗壳的蜗壳。 蜗壳具有第一蜗壳入口,其提供与蜗壳腔流体连通的第一流路,第二蜗壳入口提供与蜗壳室流体连通的第二流动路径。 第一蜗壳入口围绕壳体轴线与第二蜗壳入口周向间隔开相位角α。 第一蜗壳入口也围绕壳体轴线与第二蜗壳入口径向间隔开,并且还可以沿着壳体轴线与第二蜗壳入口轴向间隔开。
    • 7. 发明授权
    • Asymmetric split-inlet turbine housing
    • 不对称分流式涡轮机壳体
    • US08266906B2
    • 2012-09-18
    • US12401762
    • 2009-03-11
    • Ko-Jen WuJian Jun ZhangJames C. Elmslie
    • Ko-Jen WuJian Jun ZhangJames C. Elmslie
    • F03B3/16F02D23/00F04D29/44
    • F01D9/026F02B37/00F02B37/025F02B75/22F05D2220/40F05D2240/40F05D2250/51Y02T10/144
    • A turbine housing for a turbocharger for use in a reciprocating internal combustion engine includes a housing having a housing axis and configured to house a rotatable shaft having a turbine wheel disposed thereon. The housing includes a volute having a volute chamber disposed around the housing axis for receiving the turbine wheel. The volute has a first volute inlet providing a first flow path in fluid communication with the volute chamber and second volute inlet providing a second flow path in fluid communication with the volute chamber. The first volute inlet is circumferentially spaced about the housing axis from the second volute inlet by a phase angle α. The first volute inlet is also radially spaced about the housing axis from the second volute inlet, and may also be axially spaced from the second volute inlet along the housing axis.
    • 用于在往复式内燃机中使用的涡轮增压器的涡轮机壳体包括壳体,该壳体具有壳体轴线并且构造成容纳其上设置有涡轮机叶轮的可旋转轴。 壳体包括具有围绕壳体轴线设置用于接收涡轮机叶轮的蜗壳的蜗壳。 蜗壳具有第一蜗壳入口,其提供与蜗壳腔流体连通的第一流路,第二蜗壳入口提供与蜗壳室流体连通的第二流动路径。 第一蜗壳入口围绕壳体轴线与第二蜗壳入口周向间隔开相位角α。 第一蜗壳入口也围绕壳体轴线与第二蜗壳入口径向间隔开,并且还可以沿着壳体轴线与第二蜗壳入口轴向间隔开。
    • 9. 发明授权
    • Compact turbocharged cylinder deactivation engine
    • 紧凑型涡轮增压汽缸停用发动机
    • US06786190B2
    • 2004-09-07
    • US10303242
    • 2002-11-25
    • Ko-Jen WuJack T. DoyleJames C. Elmslie
    • Ko-Jen WuJack T. DoyleJames C. Elmslie
    • F02B7700
    • F02D17/02F02D21/08F02M26/05F02M26/10F02M26/22F02M26/42F02M26/43
    • An automotive vehicle engine includes multiple power-producing cylinders including a first group of deactivation cylinders capable of being selectively deactivated during engine operation and a second group of cylinders capable of continued power production during deactivation of the first group. An air intake system includes a turbocharger compressor connected to intake valves of all the cylinders for supplying charge air to the cylinders. An exhaust system includes a turbine connected for driving the compressor, which includes twin scrolls with first and second exhaust flow passages separately connecting the turbine with exhaust valves of the first group of cylinders and with exhaust valves of the second group of cylinders. At high loads, the engine operates on all cylinders and is turbocharged for maximum power. At lower loads, the first group of cylinders may be deactivated and the engine may be driven by the second group of cylinders to obtain increased fuel efficiency.
    • 机动车辆发动机包括多个发电缸,其包括能够在发动机运行期间选择性地停用的第一组停用气缸,以及能够在停用第一组期间能够继续发电的第二组汽缸。 进气系统包括连接到用于向气缸供应增压空气的所有气缸的进气阀的涡轮增压器压缩机。 排气系统包括连接用于驱动压缩机的涡轮机,其包括双涡卷,其中第一和第二排气流通道将涡轮与第一组气缸的排气阀分别连接,并具有第二组气缸的排气阀。 在高负载下,发动机在所有气缸上运行,并且为了最大功率而涡轮增压。 在较低的负载下,第一组气缸可以停用并且发动机可以由第二组气缸驱动以获得增加的燃料效率。
    • 10. 发明授权
    • Compressor inlet duct
    • 压缩机入口管道
    • US07765993B2
    • 2010-08-03
    • US11696963
    • 2007-04-05
    • Ko-Jen WuJian Jun ZhangWilliam F. Spruit
    • Ko-Jen WuJian Jun ZhangWilliam F. Spruit
    • F02B33/00F01C1/24
    • F02M35/10255F02M35/10144F04C18/16F04C29/12Y10S138/11
    • An inlet for a compressor having a housing defining a generally C-shaped inlet opening and a rotor cavity configured to contain first and second rotors is provided. The inlet includes an inlet duct defining an inlet opening and a generally C-shaped outlet opening. The inlet duct has an inner wall defining a cavity operable to communicate airflow between the inlet opening and the generally C-shaped outlet opening. The generally C-shaped outlet opening of the inlet duct is substantially similar to the shape of the generally C-shaped inlet opening of the housing. The inner wall includes a floor portion and a roof portion. At least a portion of the floor portion is contoured to impart a velocity component to the airflow complementary to the tangential velocity of each of the first and second rotors during rotation of the first and second rotors.
    • 一种用于压缩机的入口,其具有限定大致C形入口的壳体和构造成容纳第一和第二转子的转子腔。 入口包括限定入口开口和大致C形出口的入口管。 入口管道具有限定可操作以在入口开口和大体上C形出口之间连通气流的空腔的内壁。 入口管的大致C形的出口开口基本上类似于壳体的大致C形入口的形状。 内壁包括地板部分和屋顶部分。 底板部分的至少一部分被轮廓化,以在第一和第二转子旋转期间将速度分量赋予与第一和第二转子中的每一个的切向速度互补的气流。