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公开(公告)号：US09051848B2
公开(公告)日：2015-06-09
申请号：US13291390
申请日：2011-11-08
CPC分类号： F01D25/162 , F01D25/166 , F01D25/18 , F05D2220/40 , F05D2260/37 , F16C17/10 , F16C27/02 , F16C33/08 , F16C2360/24 , Y10T29/49243 , Y10T403/54
摘要： A turbocharger assembly includes: a housing with a through-bore and a cross-bore that intersects the through-bore to define an upper portion of the cross-bore with a first diameter and a lower portion of the cross-bore with a second diameter where the first diameter exceeds the second diameter; a bearing disposed in the through-bore of the housing where the bearing includes a through-bore configured to support a shaft and a cross-bore that intersects the through-bore; and a locating pin with a diameter that exceeds the second diameter of the lower portion of the cross-bore of the housing, the locating pin press-fit at least partially into the lower portion of the cross-bore of the housing and disposed at least partially in the lower portion of the cross-bore of the bearing to locate the bearing in the through-bore of the housing. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译： 涡轮增压器组件包括：具有通孔的壳体和与所述通孔相交的横孔，以限定所述横孔的上部，所述横孔的第一直径和下部具有第二直径 其中第一直径超过第二直径; 设置在所述壳体的所述通孔中的轴承，其中所述轴承包括构造成支撑轴的通孔和与所述通孔相交的横向孔; 以及定位销，其直径超过所述壳体的所述十字孔的下部的第二直径，所述定位销至少部分地压配合到所述壳体的所述交叉孔的下部并且至少设置 部分地位于轴承的横孔的下部，以将轴承定位在壳体的通孔中。 还公开了装置，组件，系统，方法等的各种其它示例。
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公开(公告)号：US10465698B2
公开(公告)日：2019-11-05
申请号：US13291466
申请日：2011-11-08
IPC分类号： F04D29/28 , F04D29/054 , F04D29/26 , F04D25/02 , F01D5/02
摘要： A turbocharger assembly includes a compressor wheel with a base surface, a nose surface, a z-plane disposed between the base surface and the nose surface and a bore extending from the base surface to the nose surface and a shaft that includes a first pilot surface disposed in the bore of the compressor wheel at a position between the z-plane and the nose surface, a second pilot surface disposed in the bore of the compressor wheel at a position between the z-plane and the base surface, and a recessed surface disposed between the first pilot surface and the second pilot surface. A nut adjustably disposed on the shaft adjacent to the nose surface can tension the shaft to apply a compressive load between the base surface and the nose surface of the compressor wheel. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
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公开(公告)号：US20130115088A1
公开(公告)日：2013-05-09
申请号：US13291466
申请日：2011-11-08
CPC分类号： F04D29/284 , F01D5/025 , F04D25/024 , F04D29/054 , F04D29/266 , F05D2220/40 , Y10T29/49321
摘要： A turbocharger assembly includes a compressor wheel with a base surface, a nose surface, a z-plane disposed between the base surface and the nose surface and a bore extending from the base surface to the nose surface and a shaft that includes a first pilot surface disposed in the bore of the compressor wheel at a position between the z-plane and the nose surface, a second pilot surface disposed in the bore of the compressor wheel at a position between the z-plane and the base surface, and a recessed surface disposed between the first pilot surface and the second pilot surface. A nut adjustably disposed on the shaft adjacent to the nose surface can tension the shaft to apply a compressive load between the base surface and the nose surface of the compressor wheel. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译： 涡轮增压器组件包括具有基座表面的压缩机叶轮，鼻部表面，设置在基部表面和鼻部表面之间的z平面以及从基部表面延伸到鼻子表面的孔，以及包括第一引导表面 设置在z平面和鼻部表面之间的位置处的压缩机叶轮的孔中，在z平面和基面之间的位置处设置在压缩机叶轮的孔中的第二引导表面， 设置在第一导频面和第二导频面之间。 可靠地设置在与鼻子表面相邻的轴上的螺母可以张紧轴以在压缩机叶轮的基面和鼻表面之间施加压缩载荷。 还公开了装置，组件，系统，方法等的各种其它示例。
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公开(公告)号：US20130115080A1
公开(公告)日：2013-05-09
申请号：US13291390
申请日：2011-11-08
CPC分类号： F01D25/162 , F01D25/166 , F01D25/18 , F05D2220/40 , F05D2260/37 , F16C17/10 , F16C27/02 , F16C33/08 , F16C2360/24 , Y10T29/49243 , Y10T403/54
摘要： A turbocharger assembly includes: a housing with a through-bore and a cross-bore that intersects the through-bore to define an upper portion of the cross-bore with a first diameter and a lower portion of the cross-bore with a second diameter where the first diameter exceeds the second diameter; a bearing disposed in the through-bore of the housing where the bearing includes a through-bore configured to support a shaft and a cross-bore that intersects the through-bore; and a locating pin with a diameter that exceeds the second diameter of the lower portion of the cross-bore of the housing, the locating pin press-fit at least partially into the lower portion of the cross-bore of the housing and disposed at least partially in the lower portion of the cross-bore of the bearing to locate the bearing in the through-bore of the housing. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译： 涡轮增压器组件包括：具有通孔的壳体和与所述通孔相交的横孔，以限定所述横孔的上部，所述横孔的第一直径和下部具有第二直径 其中第一直径超过第二直径; 设置在所述壳体的所述通孔中的轴承，其中所述轴承包括构造成支撑轴的通孔和与所述通孔相交的横向孔; 以及定位销，其直径超过所述壳体的所述十字孔的下部的第二直径，所述定位销至少部分地压配合到所述壳体的所述交叉孔的下部并且至少设置 部分地位于轴承的横孔的下部，以将轴承定位在壳体的通孔中。 还公开了装置，组件，系统，方法等的各种其它示例。
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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
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。
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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。
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公开(公告)号：US20110120125A1
公开(公告)日：2011-05-26
申请号：US12625493
申请日：2009-11-24
CPC分类号： F02C6/12 , F05D2220/40 , F05D2230/64 , F05D2240/53 , F16C17/10 , F16C17/18 , F16C27/02 , F16C33/08 , F16C33/1065 , F16C35/02 , F16C2226/50 , F16C2360/24
摘要： An exemplary semi-floating bearing for a turbocharger has a central axis defining a cylindrical coordinate system with an axial direction, a radial direction and an angular direction; a turbine end; a compressor end; journal surfaces between the turbine end and the compressor end, the surfaces configured to support a turbocharger shaft; and an opening disposed between the turbine end and the compressor end, the opening having a radial dimension that exceeds an axial dimension to, upon receipt of a locating pin, provide for movement of the bearing in the angular direction about its central axis and to provide for lesser movement of the bearing in the axial direction. Other exemplary bearings, arrangements and methods are also disclosed.
摘要翻译： 用于涡轮增压器的示例性半浮动轴承具有限定具有轴向方向，径向方向和角度方向的圆柱形坐标系的中心轴线; 涡轮机端; 压缩机端; 在涡轮机端部和压缩机端部之间的轴颈表面，构造成支撑涡轮增压器轴的表面; 以及设置在所述涡轮机端部和所述压缩机端部之间的开口，所述开口具有超过轴向尺寸的径向尺寸，以在接收到定位销时提供所述轴承围绕其中心轴线在角度方向上的运动，并且提供 用于轴承在轴向上较小的运动。 还公开了其它示例性轴承，布置和方法。
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公开(公告)号：US09140185B2
公开(公告)日：2015-09-22
申请号：US12625493
申请日：2009-11-24
CPC分类号： F02C6/12 , F05D2220/40 , F05D2230/64 , F05D2240/53 , F16C17/10 , F16C17/18 , F16C27/02 , F16C33/08 , F16C33/1065 , F16C35/02 , F16C2226/50 , F16C2360/24
摘要： An exemplary semi-floating bearing for a turbocharger has a central axis defining a cylindrical coordinate system with an axial direction, a radial direction and an angular direction; a turbine end; a compressor end; journal surfaces between the turbine end and the compressor end, the surfaces configured to support a turbocharger shaft; and an opening disposed between the turbine end and the compressor end, the opening having a radial dimension that exceeds an axial dimension to, upon receipt of a locating pin, provide for movement of the bearing in the angular direction about its central axis and to provide for lesser movement of the bearing in the axial direction. Other exemplary bearings, arrangements and methods are also disclosed.
摘要翻译： 用于涡轮增压器的示例性半浮动轴承具有限定具有轴向方向，径向方向和角度方向的圆柱形坐标系的中心轴线; 涡轮机端; 压缩机端; 在涡轮机端部和压缩机端部之间的轴颈表面，构造成支撑涡轮增压器轴的表面; 以及设置在所述涡轮机端部和所述压缩机端部之间的开口，所述开口具有超过轴向尺寸的径向尺寸，以在接收到定位销时提供所述轴承围绕其中心轴线在角度方向上的运动，并且提供 用于轴承在轴向上较小的运动。 还公开了其它示例性轴承，布置和方法。
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公开(公告)号：US09163668B2
公开(公告)日：2015-10-20
申请号：US13479688
申请日：2012-05-24
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： F16C35/02 , F16C33/08 , F16B19/02 , F16B35/00 , F04D29/046 , F04D29/056 , F16D1/10
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： A method can include providing a multi-piece locating pin, inserting a pin piece of the multi-piece locating pin into an opening in a wall of a bearing positioned in a bore of a housing of a turbocharger assembly, and securing a screw piece of the multi-piece locating pin in an opening of the housing to thereby secure the pin piece and axially locate the bearing in the bore of the housing of the turbocharger assembly. Other exemplary pins, arrangements and methods are also disclosed.
摘要翻译： 一种方法可以包括提供多件定位销，将多片定位销的销件插入定位在涡轮增压器组件的壳体的孔中的轴承的壁中的开口中，并且固定螺钉片 多件定位销在壳体的开口中，从而固定销件并将轴承轴向定位在涡轮增压器组件的壳体的孔中。 还公开了其它示例性引脚，布置和方法。
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公开(公告)号：US20120246905A1
公开(公告)日：2012-10-04
申请号：US13479688
申请日：2012-05-24
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： B23P11/00
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： A method can include providing a multi-piece locating pin, inserting a pin piece of the multi-piece locating pin into an opening in a wall of a bearing positioned in a bore of a housing of a turbocharger assembly, and securing a screw piece of the multi-piece locating pin in an opening of the housing to thereby secure the pin piece and axially locate the bearing in the bore of the housing of the turbocharger assembly. Other exemplary pins, arrangements and methods are also disclosed.
摘要翻译： 一种方法可以包括提供多件定位销，将多片定位销的销件插入定位在涡轮增压器组件的壳体的孔中的轴承的壁中的开口中，并且固定螺钉片 多件定位销在壳体的开口中，从而固定销件并将轴承轴向定位在涡轮增压器组件的壳体的孔中。 还公开了其它示例性引脚，布置和方法。
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