TURBINE SHAFT AND TURBOCHARGER
    1.
    发明申请

    公开(公告)号:US20180355723A1

    公开(公告)日:2018-12-13

    申请号:US16104194

    申请日:2018-08-17

    申请人: IHI Corporation

    IPC分类号: F01D5/02 F01D11/02

    摘要: A turbine shaft includes: a turbine impeller having a protruding portion provided on a back surface of a main body portion thereof and a welded surface provided on the back surface of the main body portion in a radially outer side of the protruding portion; and a shaft having an end hole provided on the one end surface thereof, the end hole in which the protruding portion is inserted, a welding surface provided in a radially outer side of the end hole and welded to the welded surface, a second seal groove provided in another end side with respect to the welding surface, and an enlarged diameter portion formed between the welding surface and the second seal groove, a diameter of the enlarged diameter portion expanding radially outward from the welding surface side toward the second seal groove side.

    VARIABLE NOZZLE UNIT AND VARIABLE GEOMETRY TURBOCHARGER
    2.
    发明申请
    VARIABLE NOZZLE UNIT AND VARIABLE GEOMETRY TURBOCHARGER 审中-公开
    可变的喷嘴单元和可变几何涡轮机

    公开(公告)号:US20170058764A1

    公开(公告)日:2017-03-02

    申请号:US15348602

    申请日:2016-11-10

    申请人: IHI Corporation

    IPC分类号: F02B37/22 F02B37/24

    摘要: In a variable nozzle unit, at a position located away from and opposed to a first nozzle ring in a right-left direction, a second nozzle ring is provided integrally with the first nozzle ring through multiple connecting pins arranged in a circumferential direction. An inner edge portion of a support ring is connected to the first nozzle ring by riveting of one end portions of the multiple connecting pins. Each pin hole in the support ring is formed into such a shape extending in a radial direction of the support ring. A washer is provided between a rim of each pin hole in the support ring and a rivet head brought about by joining of the end portion of the corresponding connecting pin.

    摘要翻译: 在可变喷嘴单元中,在位于左右方向上与第一喷嘴环相离并相对的位置处,通过沿圆周方向布置的多个连接销与第一喷嘴环一体地设置第二喷嘴环。 支撑环的内缘部分通过铆接多个连接销的一个端部而连接到第一喷嘴环。 支撑环中的每个销孔形成为在支撑环的径向方向上延伸的形状。 在支撑环中的每个销孔的边缘和通过相应的连接销的端部的接合而带来的铆钉头之间设置有垫圈。

    VARIABLE DISPLACEMENT TURBOCHARGER
    3.
    发明申请

    公开(公告)号:US20200300162A1

    公开(公告)日:2020-09-24

    申请号:US16899404

    申请日:2020-06-11

    申请人: IHI Corporation

    IPC分类号: F02C6/12 F01D17/16 F02B37/24

    摘要: Provided is a variable capacity turbocharger, including: a drive ring including a main body portion having an annular shape; a first projection portion and a second projection portion, which are formed on the main body portion, and are arranged apart from one another in a circumferential direction of the main body portion so as to sandwich a link plate to which a nozzle vane is mounted; and a cutout portion, which is formed in a portion of the main body portion between the first projection portion and the second projection portion.

    TURBOCHARGER
    4.
    发明申请
    TURBOCHARGER 审中-公开

    公开(公告)号:US20190032515A1

    公开(公告)日:2019-01-31

    申请号:US16126087

    申请日:2018-09-10

    申请人: IHI Corporation

    摘要: A turbocharger includes: a bearing housing (housing); a bearing disposed in the housing and having a thrust bearing surface; and a partition wall portion assembled to the housing, the partition wall portion including an inclined surface positioned on an outer side in a radial direction of the thrust bearing surface, extending at least vertically above the thrust bearing surface, and inclined with respect to a direction perpendicular to the axial direction of a shaft.

    VARIABLE DISPLACEMENT TURBOCHARGER
    8.
    发明申请

    公开(公告)号:US20190153943A1

    公开(公告)日:2019-05-23

    申请号:US16242035

    申请日:2019-01-08

    申请人: IHI Corporation

    IPC分类号: F02C6/12 F01D17/16 F02B37/24

    摘要: Provided is a variable capacity turbocharger, including: a drive ring including a main body portion having an annular shape; a first projection portion and a second projection portion, which are formed on the main body portion, and are arranged apart from one another in a circumferential direction of the main body portion so as to sandwich a link plate to which a nozzle vane is mounted; and a cutout portion, which is formed in a portion of the main body portion between the first projection portion and the second projection portion.

    VARIABLE DISPLACEMENT TURBOCHARGER
    9.
    发明申请

    公开(公告)号:US20190145274A1

    公开(公告)日:2019-05-16

    申请号:US16244254

    申请日:2019-01-10

    申请人: IHI Corporation

    IPC分类号: F01D17/16 F02B37/24

    摘要: A projecting portion is formed on a nozzle ring, projects to a radially outer side with respect to a cylindrical portion, extends in a circumferential direction, and is held in abutment against a housing from a side of a link plate. A plate is faced to the nozzle ring on a side of a nozzle vane, and is configured to form a flow passage in a clearance to the nozzle ring. A pin is inserted into a first insertion portion formed in the nozzle ring and a second insertion portion formed in the plate, and to which the nozzle ring and the plate are mounted while the clearance is maintained. A counter bore groove is formed in the first insertion portion of the nozzle ring on the side of the link plate, and cut out the projecting portion.

    BEARING STRUCTURE AND TURBOCHARGER
    10.
    发明申请

    公开(公告)号:US20180231053A1

    公开(公告)日:2018-08-16

    申请号:US15955833

    申请日:2018-04-18

    申请人: IHI Corporation

    摘要: A bearing structure S includes: a bearing hole formed in a housing; a main body portion of a bearing provided in the bearing hole and inserted with a shaft therethrough; damper surface and provided on an outer circumferential surface of the main body portion, the damper surface facing an inner circumferential surface of the bearing hole; thrust surface provided at end portions of the main body portion in an axial direction of the shaft; and thrust back surface portions provided in the main body portion and having an outer diameter larger than those of the damper surface, the thrust back surface portions spaced apart from the damper surface by a distance farther than a distance between each of the damper surface and the inner circumferential surface of the bearing hole and positioned on back sides of the thrust surface.