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6 条记录 (耗时 0.021 秒)

    SEALED SHAFT ASSEMBLY FOR EXHAUST TURBINES
    1.
    发明申请
    SEALED SHAFT ASSEMBLY FOR EXHAUST TURBINES 失效
    用于排气涡轮的密封轴组件

    公开(公告)号：US20110110767A1

    公开(公告)日：2011-05-12

    申请号：US12615981

    申请日：2009-11-10

    申请人： Joel Castan ,  Gerard Dieudonne ,  Arnaud Gerard ,  Lionel Toussaint

    发明人： Joel Castan ,  Gerard Dieudonne ,  Arnaud Gerard ,  Lionel Toussaint

    IPC分类号： F01D17/14 ,  F04D29/10 ,  B23P11/00

    CPC分类号： F01D17/165 ,  F02C6/12 ,  F05D2220/40

    摘要： An exemplary assembly includes a component of a turbocharger that includes a bore that extends between an inner, exhaust gas side of the component and an outer, ambient side of the component; a shaft that includes a pin portion and a head portion; a sleeve positioned on the pin portion of the shaft; and a bushing positioned over at least part of the sleeve and over at least part of the head portion of the shaft where the bushing seats the shaft and the sleeve in the bore. During operation of a turbocharger that includes such an assembly, the shaft, the sleeve and the bushing restrict flow of exhaust gas from the inner, exhaust gas side of the component to the outer, ambient side of the component. Various other exemplary devices, assemblies, methods, etc., are also disclosed.

    摘要翻译： 示例性组件包括涡轮增压器的部件，其包括在部件的内部排气侧和部件的外部空气侧之间延伸的孔; 轴，其包括销部和头部; 定位在所述轴的销部分上的套筒; 以及位于所述套筒的至少一部分上方并且在所述轴的头部部分的至少一部分上方的衬套，其中所述衬套将所述轴和所述套筒安置在所述孔中。 在包括这种组件的涡轮增压器的操作期间，轴，套筒和衬套限制排出气体从组件的内部排气侧到组件的外部环境侧的流动。 还公开了各种其它示例性装置，组件，方法等。

    Sealed shaft assembly for exhaust turbines
    2.
    发明授权
    Sealed shaft assembly for exhaust turbines 失效
    用于排气涡轮机的密封轴组件

    公开(公告)号：US08579579B2

    公开(公告)日：2013-11-12

    申请号：US12615981

    申请日：2009-11-10

    申请人： Joel Castan ,  Gerard Dieudonne ,  Arnaud Gerard ,  Lionel Toussaint

    发明人： Joel Castan ,  Gerard Dieudonne ,  Arnaud Gerard ,  Lionel Toussaint

    IPC分类号： F01D11/00

    CPC分类号： F01D17/165 ,  F02C6/12 ,  F05D2220/40

    摘要： An exemplary assembly includes a component of a turbocharger that includes a bore that extends between an inner, exhaust gas side of the component and an outer, ambient side of the component; a shaft that includes a pin portion and a head portion; a sleeve positioned on the pin portion of the shaft; and a bushing positioned over at least part of the sleeve and over at least part of the head portion of the shaft where the bushing seats the shaft and the sleeve in the bore. During operation of a turbocharger that includes such an assembly, the shaft, the sleeve and the bushing restrict flow of exhaust gas from the inner, exhaust gas side of the component to the outer, ambient side of the component. Various other exemplary devices, assemblies, methods, etc., are also disclosed.

    摘要翻译： 示例性组件包括涡轮增压器的部件，其包括在部件的内部排气侧和部件的外部空气侧之间延伸的孔; 轴，其包括销部和头部; 定位在所述轴的销部分上的套筒; 以及位于所述套筒的至少一部分上方并且在所述轴的头部部分的至少一部分上方的衬套，其中所述衬套将所述轴和所述套筒安置在所述孔中。 在包括这种组件的涡轮增压器的操作期间，轴，套筒和衬套限制排出气体从组件的内部排气侧到组件的外部环境侧的流动。 还公开了各种其它示例性装置，组件，方法等。

    MULTI-PIECE LOCATING PIN
    3.
    发明申请
    MULTI-PIECE LOCATING PIN 有权
    多个位置的PIN码

    公开(公告)号：US20090293257A1

    公开(公告)日：2009-12-03

    申请号：US12132123

    申请日：2008-06-03

    申请人： Joel Castan ,  Dominique Armand ,  Arnaud Gerard ,  Franck Blaise

    发明人： Joel Castan ,  Dominique Armand ,  Arnaud Gerard ,  Franck Blaise

    IPC分类号： B23Q3/00

    CPC分类号： F16C33/08 ,  F04D29/046 ,  F04D29/0563 ,  F16B19/02 ,  F16B35/005 ,  F16C17/10 ,  F16C27/02 ,  F16C35/02 ,  F16C2226/50 ,  F16C2360/24 ,  F16D2001/102 ,  Y10T29/4932 ,  Y10T29/49826 ,  Y10T29/49895 ,  Y10T29/49945

    摘要： An exemplary multi-piece locating pin for a turbocharger assembly includes a screw piece with a nub and a securing feature to secure the screw piece in a housing of a turbocharger assembly and a pin piece with a receptacle configured to receive the nub and a locating surface to locate a bearing in a bore of the housing. An exemplary turbocharger assembly includes a housing with a bore, a bearing positioned in the bore where the bearing has a wall opening and a multi-piece locating pin secured to the housing and inserted at least partially in the wall opening to axially locate the bearing in the bore. Other exemplary pins, arrangements and methods are also disclosed.

    摘要翻译： 用于涡轮增压器组件的示例性多件定位销包括具有凸块的螺纹件和用于将螺钉件固定在涡轮增压器组件的壳体中的固定特征，以及具有接收构造成接纳该凸块的定位表面的销件 以将轴承定位在壳体的孔中。 示例性的涡轮增压器组件包括具有孔的壳体，位于孔中的轴承，其中轴承具有壁开口，以及固定到壳体并且至少部分地插入到壁开口中的多片定位销，以将轴承定位在 孔。 还公开了其它示例性引脚，布置和方法。

    Multi-piece locating pin
    4.
    发明授权
    Multi-piece locating pin 有权
    多片定位销

    公开(公告)号：US08186922B2

    公开(公告)日：2012-05-29

    申请号：US12132123

    申请日：2008-06-03

    申请人： Joel Castan ,  Dominique Armand ,  Arnaud Gerard ,  Franck Blaise

    发明人： Joel Castan ,  Dominique Armand ,  Arnaud Gerard ,  Franck Blaise

    IPC分类号： F16B35/00

    CPC分类号： F16C33/08 ,  F04D29/046 ,  F04D29/0563 ,  F16B19/02 ,  F16B35/005 ,  F16C17/10 ,  F16C27/02 ,  F16C35/02 ,  F16C2226/50 ,  F16C2360/24 ,  F16D2001/102 ,  Y10T29/4932 ,  Y10T29/49826 ,  Y10T29/49895 ,  Y10T29/49945

    摘要： An exemplary multi-piece locating pin for a turbocharger assembly includes a screw piece with a nub and a securing feature to secure the screw piece in a housing of a turbocharger assembly and a pin piece with a receptacle configured to receive the nub and a locating surface to locate a bearing in a bore of the housing. An exemplary turbocharger assembly includes a housing with a bore, a bearing positioned in the bore where the bearing has a wall opening and a multi-piece locating pin secured to the housing and inserted at least partially in the wall opening to axially locate the bearing in the bore. Other exemplary pins, arrangements and methods are also disclosed.

    摘要翻译： 用于涡轮增压器组件的示例性多件定位销包括具有凸块的螺纹件和用于将螺钉件固定在涡轮增压器组件的壳体中的固定特征，以及具有接收构造成接纳该凸块的定位表面的销件 以将轴承定位在壳体的孔中。 示例性的涡轮增压器组件包括具有孔的壳体，位于孔中的轴承，其中轴承具有壁开口，以及固定到壳体并且至少部分地插入到壁开口中的多片定位销，以将轴承定位在 孔。 还公开了其它示例性引脚，布置和方法。