-
公开(公告)号：US20090077966A1
公开(公告)日：2009-03-26
申请号：US12093747
申请日：2005-11-16
CPC分类号： F02B37/22 , F01D17/143 , F01D17/146 , F05D2220/40 , Y02T10/144
摘要： A sliding piston cartridge (50) for a turbocharger (20) that is insertable into a bore (44) in the turbine housing (38) as a unit and that includes all of the components of a sliding piston type variable nozzle. The sliding piston cartridge comprises a carrier (52) having a tubular portion that interfaces with the bore of the turbine housing. A sliding piston (62) is disposed within the carrier and makes sliding contact therewith. Vanes (58) are mounted on or formed as a part of the carrier at its upstream end, the vanes extending across a turbine nozzle. The piston slides between a closed position and an open position relative to the carrier. The tubular portion of the carrier can include openings (66) that are progressively uncovered by the piston as it moves toward the open position, to allow additional flow to enter the turbine wheel without passing through the vanes.
摘要翻译： 一种用于涡轮增压器（20）的滑动活塞筒（50），其可作为一个单元插入涡轮壳体（38）中的孔（44）中，并且包括滑动活塞式可变喷嘴的所有部件。 滑动活塞筒包括具有与涡轮壳体的孔相接合的管状部分的托架（52）。 滑动活塞（62）设置在载体内并与其滑动接触。 叶片（58）在其上游端安装在载体的一部分上或形成为载体的一部分，叶片延伸穿过涡轮喷嘴。 活塞在关闭位置和相对于载体的打开位置之间滑动。 载体的管状部分可以包括当活塞向打开位置移动时逐渐未被活塞覆盖的开口（66），以允许额外的流动进入涡轮机叶轮而不通过叶片。
-
公开(公告)号：US08191367B2
公开(公告)日：2012-06-05
申请号：US12093747
申请日：2005-11-16
CPC分类号： F02B37/22 , F01D17/143 , F01D17/146 , F05D2220/40 , Y02T10/144
摘要： A sliding piston cartridge (50) for a turbocharger (20) that is insertable into a bore (44) in the turbine housing (38) as a unit and that includes all of the components of a sliding piston type variable nozzle. The sliding piston cartridge comprises a carrier (52) having a tubular portion that interfaces with the bore of the turbine housing. A sliding piston (62) is disposed within the carrier and makes sliding contact therewith. Vanes (58) are mounted on or formed as a part of the carrier at its upstream end, the vanes extending across a turbine nozzle. The piston slides between a closed position and an open position relative to the carrier. The tubular portion of the carrier can include openings (66) that are progressively uncovered by the piston as it moves toward the open position, to allow additional flow to enter the turbine wheel without passing through the vanes.
摘要翻译： 一种用于涡轮增压器（20）的滑动活塞筒（50），其可作为一个单元插入涡轮机壳体（38）中的孔（44）中并且包括滑动活塞式可变喷嘴的所有部件。 滑动活塞筒包括具有与涡轮壳体的孔相接合的管状部分的托架（52）。 滑动活塞（62）设置在载体内并与其滑动接触。 叶片（58）在其上游端安装在载体的一部分上或形成为载体的一部分，叶片延伸穿过涡轮喷嘴。 活塞在关闭位置和相对于载体的打开位置之间滑动。 载体的管状部分可以包括当活塞向打开位置移动时逐渐未被活塞覆盖的开口（66），以允许额外的流动进入涡轮机叶轮而不通过叶片。
-
公开(公告)号：US08353666B2
公开(公告)日：2013-01-15
申请号：US13187295
申请日：2011-07-20
IPC分类号： F04D29/58
CPC分类号： F02C6/12 , F05D2220/40
摘要： A turbocharger for internal combustion engines, having a heat shield disposed between a turbine housing and center housing of the turbocharger for shielding the center housing from exhaust gases passing through the turbine. The heat shield in one embodiment is centered on a generally conical surface of the center housing, by engagement between the conical surface and a centering portion of the heat shield. In another embodiment, the heat shield has a generally conical portion that is non-axisymmetric, having a plurality of radially enlarged lobes that engage a radially inwardly facing surface of the turbine housing for centering the heat shield.
摘要翻译： 一种用于内燃机的涡轮增压器，其具有设置在涡轮壳体和涡轮增压器的中心壳体之间的隔热罩，用于将中心壳体与通过涡轮机的排气隔离。 一个实施例中的隔热罩通过锥形表面与隔热罩的定心部分之间的接合在中心壳体的大致圆锥形表面上居中。 在另一个实施例中，隔热罩具有非轴对称的大致圆锥形的部分，其具有多个径向扩大的凸角，其接合涡轮机壳体的径向向内的表面以对准隔热罩。
-
公开(公告)号：US08123470B2
公开(公告)日：2012-02-28
申请号：US11836993
申请日：2007-08-10
IPC分类号： F01D1/02
CPC分类号： F02C6/12 , F01D17/141 , F05D2220/40
摘要： A turbine assembly for a turbocharger includes a variable nozzle formed by a sliding half-collar piston. A first-stage nozzle has a plurality of first vanes supported by a first nozzle ring and extending axially therefrom. A second-stage nozzle has a second nozzle ring connected to the ends of the first vanes, and a plurality of second vanes extending axially therefrom. The piston regulates flow through the second-stage nozzle, while the first-stage nozzle remains open when the piston is fully closed. The second nozzle ring at least partially divides the first vanes from the second vanes. The half-collar piston includes recesses that receive the second vanes and only partially surround the girth of each second vane.
摘要翻译： 用于涡轮增压器的涡轮组件包括由滑动半环活塞形成的可变喷嘴。 第一级喷嘴具有由第一喷嘴环支撑并从其轴向延伸的多个第一叶片。 第二级喷嘴具有连接到第一叶片的端部的第二喷嘴环和从其轴向延伸的多个第二叶片。 当活塞完全关闭时，活塞调节通过第二级喷嘴的流量，而第一级喷嘴保持打开。 第二喷嘴环至少部分地将第一叶片与第二叶片分开。 半领活塞包括容纳第二叶片并且仅部分地围绕每个第二叶片的环的凹部。
-
5.发明申请Variable Geometry Turbine For A Turbocharger And Method Of Controlling The Turbine 失效用于涡轮增压器的可变几何涡轮机和控制涡轮机的方法公开(公告)号：US20090169366A1
公开(公告)日：2009-07-02
申请号：US11886834
申请日：2005-03-25
IPC分类号： F01D17/00
CPC分类号： F02C6/12 , F01D17/105 , F01D17/143 , F02B37/18 , F05D2220/40
摘要： There is described a variable geometry turbine having a sliding element (5) for the control of the section throat of the turbine (1) by sliding movement along an axial direction of a turbine wheel (71). The turbine wheel operates to convert a flow of working fluid into mechanical energy. At least one bypass channel (51) is defined in the sliding element (5). The bypass channel is further connected to a turbine wheel outlet area (79) downstream of the turbine wheel for selectively guiding an excess flow of working fluid past the turbine wheel (71), so as to control the operation of the turbine. A use of the variable geometry turbine with a turbocharger for an engine and a method for controlling such turbine is also described.
摘要翻译： 描述了具有滑动元件（5）的可变几何涡轮机，用于通过沿着涡轮机叶轮（71）的轴向的滑动运动来控制涡轮机（1）的部分喉部。 涡轮机轮操作以将工作流体流转换成机械能。 至少一个旁通通道（51）限定在滑动元件（5）中。 旁路通道进一步连接到涡轮机叶轮下游的涡轮机叶轮出口区域（79），用于选择性地引导工作流体的过量流过涡轮机叶轮（71），以便控制涡轮机的运行。 还描述了使用具有用于发动机的涡轮增压器的可变几何涡轮机和用于控制这种涡轮机的方法。
-
6.发明授权Variable geometry turbine for a turbocharger and method of controlling the turbine 失效用于涡轮增压器的可变几何涡轮机和控制涡轮机的方法公开(公告)号：US08047772B2
公开(公告)日：2011-11-01
申请号：US11886834
申请日：2005-03-25
CPC分类号： F02C6/12 , F01D17/105 , F01D17/143 , F02B37/18 , F05D2220/40
摘要： There is described a variable geometry turbine having a sliding element (5) for the control of the section throat of the turbine (1) by sliding movement along an axial direction of a turbine wheel (71). The turbine wheel operates to convert a flow of working fluid into mechanical energy. At least one bypass channel (51) is defined in the sliding element (5). The bypass channel is further connected to a turbine wheel outlet area (79) downstream of the turbine wheel for selectively guiding an excess flow of working fluid past the turbine wheel (71), so as to control the operation of the turbine. A use of the variable geometry turbine with a turbocharger for an engine and a method for controlling such turbine is also described.
摘要翻译： 描述了具有滑动元件（5）的可变几何涡轮机，用于通过沿着涡轮机叶轮（71）的轴向的滑动运动来控制涡轮机（1）的部分喉部。 涡轮机轮操作以将工作流体流转换成机械能。 至少一个旁通通道（51）限定在滑动元件（5）中。 旁路通道进一步连接到涡轮机叶轮下游的涡轮机叶轮出口区域（79），用于选择性地引导工作流体的过量流过涡轮机叶轮（71），以便控制涡轮机的运行。 还描述了使用具有用于发动机的涡轮增压器的可变几何涡轮机和用于控制这种涡轮机的方法。
-
7.发明申请Method of Controlling a Turbocharger Having a Variable-Geometry Mechanism and a Waste Gate 有权控制具有可变几何机构和废物门的涡轮增压器的方法公开(公告)号：US20080282698A1
公开(公告)日：2008-11-20
申请号：US12089759
申请日：2005-10-12
CPC分类号： F02B37/22 , F02B37/12 , F02B37/18 , Y02T10/144
摘要： A method for controlling a variable-geometry turbine (24) that includes a variable-geometry mechanism that is movable between a fully closed position closing a relatively greater portion of the turbine nozzle and a fully open position closing a relatively smaller portion of the nozzle. The turbine (24) further comprises a waste gate (40) movable between a closed position and an open position in which some of the exhaust gas bypasses the turbine (24). At low engine speeds, turbocharger boost us regulated by regulating the position of the wastegate. At high engine speeds, the variable geometry is fully open and the wastegate is opened again. When at medium engine speeds, the variable geometry mechanism is to be moved from its closed position toward its fully open position, the waste gate (40) is in an open position to cause a proportion of the exhaust gas to bypass the turbine (24) and thereby reduce the pressure of the exhaust gas in the chamber. While this reduced pressure of the exhaust gas is in effect, the variable-geometry mechanism is moved from the fully closed position toward the fully open position while simultaneously the waste gate begins to close.
摘要翻译： 一种用于控制可变几何涡轮机（24）的方法，所述可变几何涡轮机（24）包括可变几何机构，所述可变几何机构可在关闭所述涡轮喷嘴的较大部分的完全关闭位置和闭合所述喷嘴的较小部分的完全打开位置之间移动。 涡轮机（24）还包括在关闭位置和打开位置之间移动的废气门（40），在该位置中，一些排气绕过涡轮机（24）。 在低发动机转速下，涡轮增压器通过调节废气门的位置来提高我们的调节。 在高发动机转速下，可变几何形状完全打开，废气门再次打开。 当处于中等发动机速度时，可变几何机构将从其关闭位置移动到其完全打开位置，废物门40处于打开位置，以使排气的一部分绕过涡轮机24， 从而降低室内的废气的压力。 虽然废气的这种减小的压力是有效的，但是可变几何机构从完全关闭位置移动到完全打开位置，同时废气门开始关闭。
-
8.发明授权Method of controlling a turbocharger having a variable-geometry mechanism and a waste gate 有权控制具有可变几何机构和废气门的涡轮增压器的方法公开(公告)号：US08112994B2
公开(公告)日：2012-02-14
申请号：US12089759
申请日：2005-10-12
IPC分类号： F02D23/00
CPC分类号： F02B37/22 , F02B37/12 , F02B37/18 , Y02T10/144
摘要： A method for controlling a variable-geometry turbine (24) that includes a variable-geometry mechanism that is movable between a fully closed position closing a relatively greater portion of the turbine nozzle and a fully open position closing a relatively smaller portion of the nozzle. The turbine (24) further comprises a waste gate (40) movable between a closed position and an open position in which some of the exhaust gas bypasses the turbine (24). At low engine speeds, turbocharger boost us regulated by regulating the position of the wastegate. At high engine speeds, the variable geometry is fully open and the wastegate is opened again. When at medium engine speeds, the variable geometry mechanism is to be moved from its closed position toward its fully open position, the waste gate (40) is in an open position to cause a proportion of the exhaust gas to bypass the turbine (24) and thereby reduce the pressure of the exhaust gas in the chamber. While this reduced pressure of the exhaust gas is in effect, the variable-geometry mechanism is moved from the fully closed position toward the fully open position while simultaneously the waste gate begins to close.
摘要翻译： 一种用于控制可变几何涡轮机（24）的方法，所述可变几何涡轮机（24）包括可变几何机构，所述可变几何机构可在关闭所述涡轮喷嘴的较大部分的完全关闭位置和闭合所述喷嘴的较小部分的完全打开位置之间移动。 涡轮机（24）还包括在关闭位置和打开位置之间移动的废气门（40），在该位置中，一些排气绕过涡轮机（24）。 在低发动机转速下，涡轮增压器通过调节废气门的位置来提高我们的调节。 在高发动机转速下，可变几何形状完全打开，废气门再次打开。 当处于中等发动机速度时，可变几何机构将从其关闭位置移动到其完全打开位置，废物门40处于打开位置，以使排气的一部分绕过涡轮机24， 从而降低室内的废气的压力。 虽然废气的这种减小的压力是有效的，但是可变几何机构从完全关闭位置移动到完全打开位置，同时废气门开始关闭。
-
公开(公告)号：US08092162B2
公开(公告)日：2012-01-10
申请号：US12043630
申请日：2008-03-06
IPC分类号： F04D29/58
CPC分类号： F02C6/12 , F05D2220/40
摘要： A turbocharger for internal combustion engines, having a heat shield disposed between a turbine housing and center housing of the turbocharger for shielding the center housing from exhaust gases passing through the turbine. The heat shield in one embodiment is centered on a generally conical surface of the center housing, by engagement between the conical surface and a centering portion of the heat shield. In another embodiment, the heat shield has a generally conical portion that is non-axisymmetric, having a plurality of radially enlarged lobes that engage a radially inwardly facing surface of the turbine housing for centering the heat shield.
摘要翻译： 一种用于内燃机的涡轮增压器，其具有设置在涡轮壳体和涡轮增压器的中心壳体之间的隔热罩，用于将中心壳体与通过涡轮机的排气隔离。 一个实施例中的隔热罩通过锥形表面与隔热罩的定心部分之间的接合在中心壳体的大致圆锥形表面上居中。 在另一个实施例中，隔热罩具有非轴对称的大致圆锥形的部分，其具有多个径向扩大的凸角，其接合涡轮机壳体的径向向内的表面以对准隔热罩。
-
公开(公告)号：US20110274535A1
公开(公告)日：2011-11-10
申请号：US13187295
申请日：2011-07-20
IPC分类号： F04D29/58
CPC分类号： F02C6/12 , F05D2220/40
摘要： A turbocharger for internal combustion engines, having a heat shield disposed between a turbine housing and center housing of the turbocharger for shielding the center housing from exhaust gases passing through the turbine. The heat shield in one embodiment is centered on a generally conical surface of the center housing, by engagement between the conical surface and a centering portion of the heat shield. In another embodiment, the heat shield has a generally conical portion that is non-axisymmetric, having a plurality of radially enlarged lobes that engage a radially inwardly facing surface of the turbine housing for centering the heat shield.
摘要翻译： 一种用于内燃机的涡轮增压器，其具有设置在涡轮壳体和涡轮增压器的中心壳体之间的隔热罩，用于将中心壳体与通过涡轮机的排气隔离。 一个实施例中的隔热罩通过锥形表面与隔热罩的定心部分之间的接合在中心壳体的大致圆锥形表面上居中。 在另一个实施例中，隔热罩具有非轴对称的大致圆锥形的部分，其具有多个径向扩大的凸角，其接合涡轮机壳体的径向向内的表面以对准隔热罩。
-
-
-
-
-
-
-
-
-
搜索结果
11 条记录 (耗时 0.024 秒)
