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公开(公告)号：US20130084161A1
公开(公告)日：2013-04-04
申请号：US13250679
申请日：2011-09-30
申请人： Chris Groves , Lionel Toussaint , Peter Davies , Pierre Barthelet
发明人： Chris Groves , Lionel Toussaint , Peter Davies , Pierre Barthelet
CPC分类号： F01D17/165 , F01D11/001 , F01D11/003 , F02C6/12
摘要： A variable-nozzle turbocharger includes a turbine housing and a center housing, and a generally annular nozzle ring and an array of vanes rotatably mounted to the nozzle ring such that the vanes can be pivoted about their axes for regulating exhaust gas flow to the turbine wheel. The vanes extend between the nozzle ring and an opposite wall formed by an insert in the turbine housing. A vane sealing member is supported on the insert, and has a portion disposed between distal ends of the vanes and the insert. This portion of the vane sealing member is configured to be contacted by the distal ends of the vanes when the vanes are in the closed position, while a clearance exists between the portion of the vane sealing member and the distal ends of the vanes when the vanes are in the open position.
摘要翻译： 可变喷嘴涡轮增压器包括涡轮机壳体和中心壳体，以及大致环形的喷嘴环和可旋转地安装到喷嘴环的叶片阵列，使得叶片可绕其轴线枢转，以调节排放气体流到涡轮机叶轮 。 叶片在喷嘴环和由涡轮壳体中的插入件形成的相对壁之间延伸。 叶片密封构件支撑在插入件上，并且具有设置在叶片的远端和插入件之间的部分。 叶片密封构件的该部分构造成当叶片处于关闭位置时与叶片的远端接触，而当叶片密封构件的部分与叶片的远端之间存在间隙时，叶片 处于开放状态。
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公开(公告)号：US08985943B2
公开(公告)日：2015-03-24
申请号：US13250679
申请日：2011-09-30
申请人： Chris Groves , Lionel Toussaint , Peter Davies , Pierre Barthelet
发明人： Chris Groves , Lionel Toussaint , Peter Davies , Pierre Barthelet
CPC分类号： F01D17/165 , F01D11/001 , F01D11/003 , F02C6/12
摘要： A variable-nozzle turbocharger includes a turbine housing and a center housing, and a generally annular nozzle ring and an array of vanes rotatably mounted to the nozzle ring such that the vanes can be pivoted about their axes for regulating exhaust gas flow to the turbine wheel. The vanes extend between the nozzle ring and an opposite wall formed by an insert in the turbine housing. A vane sealing member is supported on the insert, and has a portion disposed between distal ends of the vanes and the insert. This portion of the vane sealing member is configured to be contacted by the distal ends of the vanes when the vanes are in the closed position, while a clearance exists between the portion of the vane sealing member and the distal ends of the vanes when the vanes are in the open position.
摘要翻译： 可变喷嘴涡轮增压器包括涡轮机壳体和中心壳体，以及大致环形的喷嘴环和可旋转地安装到喷嘴环的叶片阵列，使得叶片可绕其轴线枢转，以调节排放气体流到涡轮机叶轮 。 叶片在喷嘴环和由涡轮壳体中的插入件形成的相对壁之间延伸。 叶片密封构件支撑在插入件上，并且具有设置在叶片的远端和插入件之间的部分。 叶片密封构件的该部分构造成当叶片处于关闭位置时与叶片的远端接触，而当叶片密封构件的部分与叶片的远端之间存在间隙时，叶片 处于开放状态。
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3.发明申请Sealing Arrangement Between a Variable-Nozzle Assembly and a Turbine Housing of a Turbocharger 有权可变喷嘴组件与涡轮增压器的涡轮机壳体之间的密封布置公开(公告)号：US20130036733A1
公开(公告)日：2013-02-14
申请号：US13205330
申请日：2011-08-08
CPC分类号： F02B37/24 , B23P15/006 , F01D9/04 , F01D17/165 , F02B37/22 , F02C6/12 , F02D41/0007 , F05D2220/40 , F05D2240/55 , Y10T29/49243
摘要： A turbocharger includes a variable-nozzle assembly that includes an insert having a tubular portion received into a stepped bore of a turbine housing and having a nozzle portion extending radially out from one end of the tubular portion, and a generally annular nozzle ring axially spaced from the nozzle portion and an array of vanes rotatably mounted to the nozzle ring. Sealing of the interface between the tubular portion of the insert and the turbine housing is provided by a sealing ring formed as a generally annular body having a U- or V-shaped cross-section oriented such that an open side of the U- or V-shaped cross-section faces in a radial direction. The U- or V-shaped cross-section defines two opposing legs, one of the legs being engaged against an end face of the tubular portion of the insert and the other leg being engaged against an upstream-facing step surface of the turbine housing bore.
摘要翻译： 涡轮增压器包括可变喷嘴组件，其包括具有容纳在涡轮机壳体的阶梯孔中的管状部分的插入件，并且具有从管状部分的一端径向地延伸的喷嘴部分，以及大体上环形的喷嘴环， 喷嘴部分和可旋转地安装到喷嘴环的叶片阵列。 插入件的管状部分和涡轮机壳体之间的界面的密封由形成为大致环形体的密封环提供，该环形体的U形或V形横截面被定向为使得U形或V形的开口侧 形截面面向径向。 U形或V形横截面限定两个相对的腿，其中一个腿与插入件的管状部分的端面接合，另一个腿与涡轮机壳体孔的上游侧台阶表面接合 。
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4.发明授权Sealing arrangement between a variable-nozzle assembly and a turbine housing of a turbocharger 有权可变喷嘴组件与涡轮增压器的涡轮壳体之间的密封布置公开(公告)号：US08763393B2
公开(公告)日：2014-07-01
申请号：US13205330
申请日：2011-08-08
CPC分类号： F02B37/24 , B23P15/006 , F01D9/04 , F01D17/165 , F02B37/22 , F02C6/12 , F02D41/0007 , F05D2220/40 , F05D2240/55 , Y10T29/49243
摘要： A turbocharger includes a variable-nozzle assembly that includes an insert having a tubular portion received into a stepped bore of a turbine housing and having a nozzle portion extending radially out from one end of the tubular portion, and a generally annular nozzle ring axially spaced from the nozzle portion and an array of vanes rotatably mounted to the nozzle ring. Sealing of the interface between the tubular portion of the insert and the turbine housing is provided by a sealing ring formed as a generally annular body having a U- or V-shaped cross-section oriented such that an open side of the U- or V-shaped cross-section faces in a radial direction. The U- or V-shaped cross-section defines two opposing legs, one of the legs being engaged against an end face of the tubular portion of the insert and the other leg being engaged against an upstream-facing step surface of the turbine housing bore.
摘要翻译： 涡轮增压器包括可变喷嘴组件，其包括具有容纳在涡轮机壳体的阶梯孔中的管状部分的插入件，并且具有从管状部分的一端径向地延伸的喷嘴部分，以及大体上环形的喷嘴环， 喷嘴部分和可旋转地安装到喷嘴环的叶片阵列。 插入件的管状部分和涡轮机壳体之间的界面的密封由形成为大致环形体的密封环提供，该环形体的U形或V形横截面被定向为使得U形或V形的开口侧 形截面面向径向。 U形或V形横截面限定两个相对的腿，其中一个腿与插入件的管状部分的端面接合，另一个腿与涡轮机壳体孔的上游侧台阶表面接合 。
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公开(公告)号：US20110138805A1
公开(公告)日：2011-06-16
申请号：US12638198
申请日：2009-12-15
申请人： Pierre Barthelet , Olivier Espasa , Julien Mailfert , Nicolas Morand , Emmanuel Severin , Lionel Toussaint
发明人： Pierre Barthelet , Olivier Espasa , Julien Mailfert , Nicolas Morand , Emmanuel Severin , Lionel Toussaint
CPC分类号： F01D17/165 , F05D2220/40 , F05D2250/711 , F05D2260/50 , F05D2260/53
摘要： A turbocharger assembly comprises a variable-vane assembly. The variable-vane assembly includes a unison ring with vane arms and/or a main-arm which adjust the setting angle of vanes. Vane arm-engaging elements and main-arm-engaging elements in the unison ring engage ends of the vane arms and the main-arm, respectively. Each vane arm-engaging element comprises an inner contact surface that engages an outer contact surface of the respective vane arm. The main-arm-engaging element comprises an inner actuation surface that engages an outer actuation surface of the main-arm. The inner contact surface and the outer contact surface and/or the inner actuation surface and the outer actuation surface may comprise conjugate curve profiles, such as involute curve profiles based on the involute of a circle. Use of conjugate curve profiles may result in rolling movement between the unison ring and vane arms and/or main arm, which may reduce friction occurring during pivoting of the vanes.
摘要翻译： 涡轮增压器组件包括可变叶片组件。 可变叶片组件包括具有叶片臂的协调环和/或调整叶片的设定角度的主臂。 共振环中的叶片臂接合元件和主臂接合元件分别接合叶片臂和主臂的端部。 每个叶片臂接合元件包括接合相应叶片臂的外接触表面的内接触表面。 主臂接合元件包括接合主臂的外部致动表面的内部致动表面。 内部接触表面和外部接触表面和/或内部致动表面和外部致动表面可以包括共轭曲线轮廓，例如基于圆的渐开线的渐开线曲线轮廓。 使用共轭曲线可能导致协调环和叶片臂和/或主臂之间的滚动运动，这可以减少在叶片枢转期间发生的摩擦。
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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：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：US20130302148A1
公开(公告)日：2013-11-14
申请号：US13469268
申请日：2012-05-11
IPC分类号： F01D25/26
CPC分类号： F01D11/003 , F01D11/005 , F01D17/165 , F01D25/24 , F02C6/12 , F02C7/28 , F05D2220/40 , F05D2240/55 , F16J15/0887 , F16J15/164
摘要： A turbine assembly can include a turbine wheel, a shroud component, a turbine housing, and an expansion seal that includes a lower lip, an upper lip, and a wall that extends between the lower lip and the upper lip and that is disposed between an outer seal surface of the shroud component and an inner seal surface of the turbine housing. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译： 涡轮组件可以包括涡轮机叶轮，护罩部件，涡轮机壳体和膨胀密封件，其包括在下唇缘和上唇缘之间延伸的下唇缘，上唇缘和壁，并且位于 护罩部件的外密封表面和涡轮壳体的内密封表面。 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：US07302330B1
公开(公告)日：2007-11-27
申请号：US11515517
申请日：2006-09-01
IPC分类号： G06F7/00
CPC分类号： F16H61/143 , F16H59/141 , F16H59/24 , F16H59/36 , F16H63/50 , F16H2059/366 , F16H2061/145 , Y10T477/735
摘要： A method of dynamically controlling pressure to a torque converter clutch (TCC) of a torque converter coupled to a transmission is provided. The method includes: monitoring throttle position; monitoring engine speed; controlling pressure to the torque converter clutch to increase slip after the throttle position indicates a tip-in has occurred and when engine speed is low; regulating at least one of a transmission steady state pressure to the transmission and pressure to the torque converter to maintain the increased slip; and controlling pressure to the torque converter to reduce slip by engaging the torque converter clutch.
摘要翻译： 提供了一种动态地控制耦合到变速器的变矩器的变矩器离合器（TCC）的压力的方法。 该方法包括：监控节气门位置; 监控发动机转速; 控制变矩器离合器的压力，以在节气门位置指示发生提前进入并且当发动机转速低时增加滑差; 调节变速器的变速器稳态压力和变矩器的压力中的至少一个以保持增加的滑差; 并且通过接合变矩器离合器来控制对变矩器的压力以减小滑动。
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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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