Turbocharger
    33.
    发明授权
    Turbocharger 有权
    涡轮增压器

    公开(公告)号:US08096774B2

    公开(公告)日:2012-01-17

    申请号:US12091123

    申请日:2006-05-23

    CPC classification number: F04D29/057

    Abstract: The invention relates to a turbocharger (15) comprising a bearing housing (7) which mounts a rotor shaft (12) and has a bearing-housing oil space (13); comprising a compressor housing which is connected to the bearing housing (7) and has a compressor space (14); and comprising a sealing device (20) which is provided for sealing the bearing-housing oil space (13) relative to the compressor space (14) and which has a sealing ring (1) which is arranged in a fixed position in the bearing housing (7) and has two end faces (17, 17′) which interact with associated end faces (10) and (11) of a disc (9) and a sealing bush (16) which are fastened to the rotor shaft (12), wherein the sealing ring (1) is arranged with axial play on the rotor shaft (12) between the disc (9) and the sealing bush (16); and air-delivery devices (2, 3) oriented in opposition are arranged in the end faces (17, 17′) of the sealing ring (1).

    Abstract translation: 本发明涉及一种涡轮增压器(15),其包括安装转子轴(12)并具有轴承壳体油空间(13)的轴承壳体(7)。 包括压缩机壳体,其连接到所述轴承壳体(7)并具有压缩机空间(14); 并且包括密封装置(20),所述密封装置(20)被设置用于相对于所述压缩机空间(14)密封所述轴承壳体油空间(13),并且具有密封环(1),所述密封环设置在所述轴承壳体 (7)并且具有与盘(9)的相关联的端面(10)和(11)以及紧固到转子轴(12)的密封衬套(16)相互作用的两个端面(17,17'), ,其中所述密封环(1)在所述盘(9)和所述密封衬套(16)之间的转子轴(12)上以轴向方式布置; 并且在密封环(1)的端面(17,17')中布置相对定向的空气输送装置(2,3)。

    Turbocharger of variable turbine geometry
    39.
    发明授权
    Turbocharger of variable turbine geometry 有权
    涡轮机几何形状的涡轮增压器

    公开(公告)号:US07507067B2

    公开(公告)日:2009-03-24

    申请号:US11321300

    申请日:2005-12-28

    CPC classification number: F01D17/165 F05D2220/40 F05D2230/30 F05D2260/231

    Abstract: A turbocharger of variable turbine geometry, comprising: a vane bearing ring assembly including a vane bearing ring and a disk which can be fixed to the vane bearing ring for creating a flow channel; and at least one support pin which is connected with a first end to the vane bearing ring and which is welded with a second end to the disk which comprises recesses for the support pin end to be welded, the recesses being surrounded by a heat throttle.

    Abstract translation: 一种可变涡轮机几何形状的涡轮增压器,包括:叶片轴承环组件,其包括叶片轴承环和盘,所述叶片轴承环和盘可以固定到叶片轴承环以产生流动通道; 以及至少一个支撑销,其与第一端连接到叶片轴承环,并且其第二端被焊接到盘,该盘包括用于待焊接的支撑销端部的凹部,所述凹部被热节流阀包围。

    Turbocharger of variable turbine geometry
    40.
    发明申请
    Turbocharger of variable turbine geometry 有权
    涡轮机几何形状的涡轮增压器

    公开(公告)号:US20060140751A1

    公开(公告)日:2006-06-29

    申请号:US11321300

    申请日:2005-12-28

    CPC classification number: F01D17/165 F05D2220/40 F05D2230/30 F05D2260/231

    Abstract: A turbocharger of variable turbine geometry, comprising: a vane bearing ring assembly including a vane bearing ring and a disk which can be fixed to the vane bearing ring for creating a flow channel; and at least one support pin which is connected with a first end to the vane bearing ring and which is welded with a second end to the disk which comprises recesses for the support pin end to be welded, said recesses being surrounded by a heat throttle.

    Abstract translation: 一种可变涡轮机几何形状的涡轮增压器,包括:叶片轴承环组件,其包括叶片轴承环和盘,所述叶片轴承环和盘可以固定到叶片轴承环以产生流动通道; 以及至少一个支撑销,其与第一端连接到叶片轴承环,并且其第二端被焊接到盘,该盘包括用于待焊接的支撑销端部的凹部,所述凹部被热节流阀包围。

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