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    HEAT ISOLATING ACTUATOR LINKAGE
    2.
    发明申请
    HEAT ISOLATING ACTUATOR LINKAGE 审中-公开
    热隔离执行器连接

    公开(公告)号：US20150098750A1

    公开(公告)日：2015-04-09

    申请号：US14400019

    申请日：2013-05-01

    Applicant: BorgWarner Inc.

    Inventor： Mathew King ,  Eli Morgan ,  Vahidin Alajbegovic

    IPC: F02B39/16

    CPC classification number: F02B39/16 ,  F02B37/186 ,  Y02T10/144 ,  Y10T29/49908 ,  Y10T403/32114

    Abstract: A heat isolating actuator linkage (805, 905) that includes a rod end housing (810, 910) including a bearing opening (814, 914) with a rod end ball (812, 912) disposed therein. A race insert (816, 916) is disposed between the rod end housing (810, 910) and the rod end ball (812, 912). A threaded portion (818, 918) extends from the rod end housing (810, 910) and may comprise male or female threads. A shield (830, 930) extends from the rod end housing (810, 910). The shield (830, 930) is integrally formed with the rod end housing (810, 910). The shield (830, 930) extends around a majority of the rod end housing (810, 910) and may extend to one side of the bearing opening (814, 914). Alternatively, a first portion (932) of the shield may extend towards one side of the bearing opening (914) and a second portion (932) of the shield may extend towards the other side.

    Abstract translation: 包括杆端壳体（810,910）的隔热致动器联动装置（805,905），其包括设置在其中的杆端球（812,912）的轴承开口（814,914）。 座杆插入件（816,916）设置在杆端壳体（810,910）和杆端球（812,912）之间。 螺纹部分（818,918）从杆端壳体（810,910）延伸并且可以包括阳螺纹或阴螺纹。 屏蔽（830,930）从杆端壳体（810,910）延伸。 屏蔽（830,930）与杆端壳体（810,910）一体地形成。 屏蔽件（830,930）围绕杆端壳体（810,910）的大部分延伸并且可以延伸到轴承开口（814,914）的一侧。 替代地，屏蔽件的第一部分（932）可以朝向轴承开口（914）的一侧延伸，并且屏蔽件的第二部分（932）可朝向另一侧延伸。

    DOUBLE FLOW TURBINE HOUSING TURBOCHARGER
    3.
    发明申请
    DOUBLE FLOW TURBINE HOUSING TURBOCHARGER 有权
    双流涡轮外壳涡轮增压器

    公开(公告)号：US20140093364A1

    公开(公告)日：2014-04-03

    申请号：US14119246

    申请日：2012-06-08

    Applicant: BORGWARNER INC.

    Inventor： Abraham C. Narehood ,  Vahidin Alajbegovic ,  John P. Watson

    IPC: F01D9/04

    CPC classification number: F01D9/041 ,  F01D9/026 ,  F01D17/165 ,  F02B37/025 ,  F02B37/24 ,  F02C6/12 ,  F05D2220/40 ,  F05D2250/51 ,  Y02T10/144 ,  Y10T29/4932

    Abstract: Implementations of the present disclosure are directed to turbine assemblies for turbocharger systems. In some implementations, turbine housings include a body that defines an inlet for fluid communication with a fluid source, and a wall, the wall dividing the inlet into an inner inlet and an outer inlet, and a fluid guide assembly disposed within the housing, the fluid guide assembly including a plurality of vanes that demarcate an inner volute and an outer volute within the housing, the inner volute being in fluid communication with the inner inlet and the outer volute being in fluid communication with the outer inlet, each vane of the plurality of vanes being fixed at a respective angle relative to a radial direction, the plurality of vanes guiding fluid flow from the outer volute to the inner volute.

    Abstract translation: 本公开的实施例涉及用于涡轮增压器系统的涡轮组件。 在一些实施方案中，涡轮机壳体包括限定用于与流体源流体连通的入口的主体和壁，将入口分成内部入口和外部入口的壁以及设置在壳体内的流体引导组件， 流体引导组件包括多个叶片，其划分在壳体内的内蜗壳和外蜗壳，内蜗壳与内入口和外蜗壳流体连通，与外进口流体连通，多个叶片中的每个叶片 所述叶片相对于径向方向以相应的角度固定，所述多个叶片将流体从所述外部蜗壳引导到所述内部涡卷。

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