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    Turbine end heatsink
    2.
    发明授权
    Turbine end heatsink 有权
    涡轮端头散热器

    公开(公告)号：US09097264B1

    公开(公告)日：2015-08-04

    申请号：US14573586

    申请日：2014-12-17

    Applicant: BorgWarner Inc.

    Inventor： Donald Michael Kennedy

    IPC: F01D25/08 ,  F04D29/58 ,  F04D29/056 ,  F04D17/10

    CPC classification number: F04D29/582 ,  F01D9/026 ,  F01D25/14 ,  F04D17/10 ,  F04D29/0563 ,  F05D2220/40 ,  F05D2260/2214 ,  F05D2260/22141

    Abstract: A product is disclosed for use with a turbocharging system. The product may include a bearing housing configured to house a bearing and having a flange. A shaft may extend through the bearing and a turbine wheel may be connected to one end of the shaft. A turbine housing may be disposed around the turbine wheel and may include an annular wall adapted to mate with the flange of the bearing housing. A cooling plate may comprise a washer shaped body and may be disposed around, and spaced apart from, the bearing housing. The cooling plate may be connected to the turbine housing to transfer heat from the turbine housing and away from the bearing housing.

    Abstract translation: 公开了一种用于涡轮增压系统的产品。 产品可以包括构造成容纳轴承并具有凸缘的轴承壳体。 轴可以延伸穿过轴承，并且涡轮机叶轮可以连接到轴的一端。 涡轮机壳体可以设置在涡轮机叶轮周围，并且可以包括适于与轴承壳体的凸缘配合的环形壁。 冷却板可以包括垫圈形体，并且可以布置在轴承壳体周围并与其间隔开。 冷却板可以连接到涡轮机壳体以从涡轮壳体传递热量并远离轴承壳体。

    Adjustment ring damper
    3.
    发明授权
    Adjustment ring damper 有权

    公开(公告)号：US10385722B2

    公开(公告)日：2019-08-20

    申请号：US15103047

    申请日：2014-12-12

    Applicant: BorgWarner Inc.

    Inventor： Donald Michael Kennedy

    IPC: F01D17/16 ,  F02B37/24 ,  F01D9/04

    Abstract: A variable turbine geometry turbocharger (100) with an adjustment ring assembly (45) having an adjustment ring (50) and a series of pivotable guide vanes (30) that are operably connected to the adjustment ring (50). A spring-biased retention clip (60) is between adjacent vane levers (36) and is attached to the adjustment ring (50). The retention clip (60) applies a force against the adjacent vane levers (36) and dampens and reduces movement of corresponding components.

    Asymmetric actuator pivot shaft bushing for VTG turbocharger
    4.
    发明授权
    Asymmetric actuator pivot shaft bushing for VTG turbocharger 有权

    公开(公告)号：US09945287B2

    公开(公告)日：2018-04-17

    申请号：US14654000

    申请日：2013-12-05

    Applicant: BorgWarner Inc.

    Inventor： Donald Michael Kennedy

    IPC: F01D17/16 ,  F02B37/24

    CPC classification number: F02B37/24 ,  F01D17/16 ,  F01D17/165 ,  F05D2220/40 ,  Y02T10/144

    Abstract: A turbocharger (10) includes a housing (12, 14, 16) and an actuating mechanism (46) for actuating a device (40) within the housing (12, 14, 16). A pivot shaft (42) has an inside end (48) inside the housing (12, 14, 16) and an outside end (82) outside the housing (12, 14, 16). The pivot shaft (42) is rotatably mounted in a bore (64) in the housing (12, 14, 16) for transmitting an actuating movement from outside the housing (12, 14, 16) to the actuating mechanism (46). A bushing (62) is disposed in the bore (64). The bushing (62) includes an asymmetric portion (68) that extends inside the housing (12, 14, 16) to support the inside end (48) of the pivot shaft (42).

    Vane ring thermal strain relief cuts
    7.
    发明授权
    Vane ring thermal strain relief cuts 有权
    叶片环热应变减压

    公开(公告)号：US09353645B1

    公开(公告)日：2016-05-31

    申请号：US14623256

    申请日：2015-02-16

    Applicant: BorgWarner Inc.

    Inventor： Donald Michael Kennedy

    IPC: F01D25/14 ,  F01D9/02 ,  F01D17/16 ,  F01D9/04

    CPC classification number: F01D25/14 ,  F01D9/041 ,  F01D17/16 ,  F01D17/165 ,  F05D2220/40 ,  F05D2240/12 ,  F05D2260/30 ,  F05D2260/941

    Abstract: A product for a turbocharger assembly is disclosed. A turbine wheel assembly may be adapted to rotate when exposed to a flow of gas. A vane ring may be disposed in the turbine wheel assembly. A plurality of vanes may be mounted to the vane ring. The flow of gas may meet the plurality of vanes at an angle of incidence. The plurality of vanes may be adjustable to selectively change the angle of incidence. The vane ring may have at least one slot adapted to direct a thermal deformation of the vane ring in a selected direction when exposed to the flow of gas.

    Abstract translation: 公开了一种用于涡轮增压器组件的产品。 涡轮机叶轮组件可以适于在暴露于气体流时旋转。 叶轮环可以设置在涡轮机轮组件中。 多个叶片可以安装到叶片环上。 气体的流动可以以入射角与多个叶片相遇。 多个叶片可以是可调节的，以选择性地改变入射角。 叶片环可以具有至少一个适于在暴露于气体流时沿着选定方向引导叶片环的热变形的槽。

    Turbocharger including a sealing assembly
    8.
    发明授权
    Turbocharger including a sealing assembly 有权

    公开(公告)号：US11655721B2

    公开(公告)日：2023-05-23

    申请号：US17083446

    申请日：2020-10-29

    Applicant: BorgWarner Inc.

    Inventor： Augustine Cavagnaro ,  Donald Michael Kennedy ,  Erwin Perry Ellwood, III

    IPC: F01D11/00 ,  F01D25/16

    CPC classification number: F01D11/003 ,  F01D25/162 ,  F05D2220/40 ,  F05D2240/54 ,  F05D2240/55

    Abstract: A turbocharger includes a shaft extending between first and second shaft ends. A turbine wheel is coupled to the first shaft end, and a bearing housing defines a bearing housing interior and is disposed about the shaft. A turbine housing defines a turbine housing interior and is disposed about the turbine wheel. A sealing assembly includes a case disposed about the shaft and extending between a first case end proximate to the turbine wheel and a second case end distal from the turbine wheel. The sealing assembly also includes a ring disposed between the shaft and the case such that the ring is unobstructed by the case radially between the shaft and the ring. The sealing assembly further includes a deformable component coupled to the second case end and to the ring, and is moveable with the ring to seal the bearing housing interior and the turbine housing interior.

    Ball bearing turbocharger balancer
    9.
    发明授权
    Ball bearing turbocharger balancer 有权
    滚珠轴承涡轮增压器平衡器

    公开(公告)号：US09181804B1

    公开(公告)日：2015-11-10

    申请号：US14624140

    申请日：2015-02-17

    Applicant: BorgWarner Inc.

    Inventor： Donald Michael Kennedy

    IPC: G01M1/16 ,  G01M1/30 ,  F01D5/02 ,  F04D29/60 ,  B23P19/04

    CPC classification number: B23P19/04 ,  F01D5/027 ,  F04D25/024 ,  F04D29/059 ,  F04D29/601 ,  F04D29/662 ,  F05D2220/40 ,  F05D2230/80 ,  G01M1/22 ,  G01M1/30

    Abstract: A method of balancing a core assembly of a turbocharger. The core assembly may include a rotor assembly having a compressor wheel and a turbine wheel connected for common rotation by a shaft. A first bending critical speed of the rotor assembly may be determined. The core assembly may be mounted in a balancing machine. A drive source may be engaged with the core assembly to impart rotation. The rotor assembly may be rotated at an initial phase speed that is between approximately 5500 revolutions per minute and the first bending critical speed. A state of imbalance of the rotor assembly may be determined at the initial phase speed.

    Abstract translation: 一种平衡涡轮增压器的核心组件的方法。 芯组件可包括具有压缩机叶轮和涡轮机叶轮的转子组件，所述涡轮机叶片由轴连接用于共同转动。 可以确定转子组件的第一弯曲临界速度。 芯组件可以安装在平衡机中。 驱动源可以与芯组件接合以产生旋转。 转子组件可以以大约5500转/分钟和第一弯曲临界转速之间的初始相位速度旋转。 可以在初始相位速度下确定转子组件的不平衡状态。

    VARIABLE TURBINE GEOMETRY ASSEMBLY
    10.
    发明公开
    VARIABLE TURBINE GEOMETRY ASSEMBLY 审中-公开

    公开(公告)号：US20230175414A1

    公开(公告)日：2023-06-08

    申请号：US17542791

    申请日：2021-12-06

    Applicant: BorgWarner Inc.

    Inventor： Augustine Cavagnaro ,  Elias Morgan ,  Greg Williams ,  Donald Michael Kennedy ,  Sean Hastings ,  David George Grabowska ,  Matthew King

    IPC: F01D17/16 ,  F02B39/00

    CPC classification number: F01D17/16 ,  F02B39/00 ,  F05D2220/40

    Abstract: A variable turbine geometry assembly includes an adjustment ring extending along and rotatable about an axis, at least one vane lever coupled to the adjustment ring, and at least one vane coupled to the at least one vane lever. The variable turbine geometry assembly also includes a biasing member coupled to the adjustment ring at a first circumferential location on the adjustment ring and coupled to the adjustment ring at a second circumferential location on the adjustment ring. The biasing member extends from the first circumferential location to the second circumferential location. The biasing member is operably in contact with the at least one vane lever between the first circumferential location and the second circumferential location to bias the at least one vane lever toward the adjustment ring and to reduce vibration between the adjustment ring and the at least one vane lever.

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