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公开(公告)号：US20090226307A1
公开(公告)日：2009-09-10
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。
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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。
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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。
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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。
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5.发明申请TURBOCHARGER HAVING PISTON-TYPE VARIABLE NOZZLE WITH INTEGRATED ACTUATION SYSTEM 审中-公开具有集成执行系统的活塞式可变喷嘴的涡轮增压器公开(公告)号：US20090301082A1
公开(公告)日：2009-12-10
申请号：US12093771
申请日：2005-11-16
IPC分类号： F02D23/00
CPC分类号： F01D17/167 , F01D17/143 , F02B37/22 , F05D2220/40 , F05D2240/55 , F05D2260/52
摘要： A turbocharger (20) having a sliding piston type variable turbine nozzle includes a tubular piston (40) disposed in a bore (32) of the turbine housing and axially slidable relative to the turbine housing, the piston being slidable between a closed position and an open position for blocking the nozzle (36) opening by an amount dependent on axial positioning of the piston so as to regulate flow into the turbine wheel (30). The turbine housing (32) and piston (40) are structured and arranged to define a cavity (50) therebetween, and there are seals (52a, 52b) between the turbine housing and piston for sealing the cavity, the turbine housing (32) defining a passage (54) connecting with the cavity (50) and adapted to be connected with a fluid source such that application of differential fluid pressure through the passage to the cavity urges the piston to axially slide in the turbine housing.
摘要翻译： 具有滑动活塞式可变涡轮喷嘴的涡轮增压器（20）包括设置在涡轮机壳体的孔（32）中并相对于涡轮壳体可轴向滑动的管状活塞（40），所述活塞可在闭合位置和 打开位置，用于阻止喷嘴（36）的开启量取决于活塞的轴向定位，以便调节进入涡轮机叶轮（30）的流量。 涡轮壳体（32）和活塞（40）被构造和布置成在它们之间限定空腔（50），并且在涡轮壳体和活塞之间存在用于密封空腔的密封件（52a，52b），涡轮机壳体（32） 限定与空腔（50）连接并适于与流体源连接的通道（54），使得通过通道到空腔的差动流体压力的施加促使活塞在涡轮壳体中轴向滑动。
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公开(公告)号：US20070122267A1
公开(公告)日：2007-05-31
申请号：US11289217
申请日：2005-11-29
申请人： Alain Lombard , Sebastien Ferrari , Jean Perrin , Patrick Masson
发明人： Alain Lombard , Sebastien Ferrari , Jean Perrin , Patrick Masson
IPC分类号： F01D17/00
CPC分类号： F01D17/105 , F01D17/143 , F02B37/18 , F05D2220/40 , F05D2250/41 , F05D2260/52
摘要： A turbine housing assembly includes a tubular piston disposed in a bore of a turbine housing and axially slidable between a closed position and an open position for blocking a nozzle by an amount dependent on axial positioning of the piston. A bypass control member is disposed in the turbine housing and is slidable between a no-bypass position closing a bypass passage and a open bypass opening the bypass passage. The piston is structured and arranged to slide relative to the bypass control member for a part of a full stroke of the piston from the closed position toward the open position thereof, and then to engage the bypass control member and cause the bypass control member to slide together with the piston as the piston further slides toward the open position thereof such that the bypass control member is moved toward the bypass position.
摘要翻译： 涡轮机壳体组件包括设置在涡轮机壳体的孔中的管状活塞，并且可在关闭位置和打开位置之间轴向滑动，用于将喷嘴阻挡一定量，该量取决于活塞的轴向定位。 旁通控制构件设置在涡轮机壳体中，并且可在闭合旁路通道的非旁路位置和打开旁路通道的打开旁路之间滑动。 活塞被构造和布置成相对于旁路控制构件滑动，使活塞的整个行程的一部分从关闭位置朝向其打开位置滑动，然后接合旁路控制构件，并使旁路控制构件滑动 与活塞一起，随着活塞进一步向其打开位置滑动，使得旁路控制构件朝向旁路位置移动。
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公开(公告)号：US20130247565A1
公开(公告)日：2013-09-26
申请号：US13425943
申请日：2012-03-21
申请人： Manuel Marques , Jean-Jacques Laissus , Mani Palaniyappan , Alain Lombard , Quentin Roberts , Johann Kurtzmann , Aitor Herrera Celaya , Nicolas Serres
发明人： Manuel Marques , Jean-Jacques Laissus , Mani Palaniyappan , Alain Lombard , Quentin Roberts , Johann Kurtzmann , Aitor Herrera Celaya , Nicolas Serres
IPC分类号： F02B37/00
CPC分类号： F02B37/00 , F01D25/28 , F02F1/243 , F05D2220/40 , Y02T10/144
摘要： A turbocharger assembly includes a center housing rotating assembly, which comprises a center housing, bearings housed in the center housing, a shaft rotatably supported in the bearings, and compressor and turbine wheels affixed to opposite ends of the shaft; an engine cylinder head and a housing member formed together as a one-piece integral structure, wherein the housing member defines a compressor volute that receives compressed air from the compressor wheel, a turbine volute for receiving exhaust gas from the engine, a turbine nozzle for directing exhaust gas from the turbine volute into the turbine wheel, and a turbine contour; a compressor contour plug that defines an axial inlet for the compressor and a compressor contour; and a wastegate unit operable for allowing exhaust gas to bypass the turbine wheel when the wastegate unit is open and preventing exhaust gas from bypassing the turbine wheel when the wastegate unit is closed.
摘要翻译： 涡轮增压器组件包括中心壳体旋转组件，其包括中心壳体，容纳在中心壳体中的轴承，可旋转地支撑在轴承中的轴，以及固定到轴的相对端的压缩机和涡轮机轮; 发动机气缸盖和作为一体式整体结构一起形成的壳体构件，其中所述壳体构件限定从所述压缩机叶轮接收压缩空气的压缩机蜗壳，用于接收来自所述发动机的废气的涡轮蜗杆，用于 将废气从涡轮蜗杆引导到涡轮机叶轮中，以及涡轮轮廓; 压缩机轮廓塞，其限定用于压缩机的轴向入口和压缩机轮廓; 以及废气门单元，其可操作用于当废气门单元打开时允许废气绕过涡轮机叶轮，并且当废气门单元关闭时防止废气绕过涡轮机叶轮。
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公开(公告)号：US08353664B2
公开(公告)日：2013-01-15
申请号：US12611816
申请日：2009-11-03
申请人： Alain Lombard , Michael Ladonnet , Michel Thirion
发明人： Alain Lombard , Michael Ladonnet , Michel Thirion
IPC分类号： F02B37/18
CPC分类号： F01D9/026 , F01D17/105 , F01D17/141 , F02B37/183 , F02C6/12 , F05D2220/40 , F05D2250/411 , Y02T10/144
摘要： A turbocharger includes a turbine wheel mounted within a turbine housing and connected to a compressor wheel by a shaft. The turbine housing defines an exhaust gas inlet connected to a volute that surrounds the turbine wheel, and an axial bore through which exhaust gas that has passed through the turbine wheel is discharged from the turbine housing. The turbine housing further defines an annular bypass passage surrounding the bore and arranged to allow exhaust gas to bypass the turbine wheel. An annular bypass valve is disposed in the bypass passage. The bypass valve comprises a fixed annular valve seat and a rotary annular valve member arranged coaxially with the valve seat. The valve member is disposed against the valve seat and is rotatable about the axis for selectively varying a degree of alignment between respective orifices in the valve seat and valve member.
摘要翻译： 涡轮增压器包括安装在涡轮机壳体内并通过轴连接到压缩机叶轮的涡轮机叶轮。 涡轮壳体限定了连接到围绕涡轮机叶轮的蜗壳的排气入口，并且已经穿过涡轮机叶轮的废气从该涡轮机壳体排出的轴向孔。 涡轮机壳体进一步限定围绕孔的环形旁路通道，并布置成允许废气绕过涡轮机叶轮。 环形旁通阀设置在旁通通道中。 旁通阀包括固定环形阀座和与阀座同轴布置的旋转环形阀构件。 阀构件设置成抵靠阀座并且可围绕轴线旋转，以选择性地改变阀座和阀构件中各个孔口之间的对准程度。
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9.发明授权Turbine assembly for an exhaust gas-driven turbocharger having a variable nozzle 有权具有可变喷嘴的排气驱动涡轮增压器的涡轮机组件公开(公告)号：US08113770B2
公开(公告)日：2012-02-14
申请号：US12364715
申请日：2009-02-03
申请人： Alain Lombard , Nicolas Serres , Michael Ladonnet
发明人： Alain Lombard , Nicolas Serres , Michael Ladonnet
摘要： A turbocharger with an exhaust gas-driven turbine includes a variable nozzle formed by a stator supporting fixed vanes and defining bypass openings, and a rotor supporting movable vanes and defining bypass channels. Each fixed vane overlaps with a movable vane by a varying extent dependent on rotational position of the rotor. In a fully open position of the rotor, the movable vanes have a maximum extent of overlap with the fixed vanes, and the bypass channels align with the bypass openings so that some of the exhaust gas flows through the aligned bypass openings and channels, bypassing the turbine wheel.
摘要翻译： 具有排气驱动涡轮的涡轮增压器包括由支撑固定叶片并限定旁路开口的定子形成的可变喷嘴，以及支撑可动叶片并限定旁路通道的转子。 每个固定叶片根据转子的旋转位置与可移动叶片重叠变化程度。 在转子的完全打开位置，可动叶片与固定叶片具有最大程度的重叠，并且旁路通道与旁路开口对准，使得一些废气流过对准的旁路开口和通道，从而绕过 涡轮机轮。
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10.发明申请公开(公告)号：US20110268559A1
公开(公告)日：2011-11-03
申请号：US12771434
申请日：2010-04-30
申请人： Alain Lombard , Michel Thirion , Nicolas Serres
发明人： Alain Lombard , Michel Thirion , Nicolas Serres
IPC分类号： F01D17/00
CPC分类号： F01D17/105 , F01D17/148 , F01D17/167 , F02C6/12 , F05D2220/40 , F05D2250/311 , F05D2250/411 , F05D2260/606 , F05D2270/66
摘要： A turbocharger includes an annular bypass passage to allow exhaust gas to bypass the turbine wheel. An annular bypass valve is disposed in the bypass passage. The bypass valve comprises a fixed annular valve seat and a rotary annular valve member arranged coaxially with the valve seat. The valve member is disposed against the valve seat and is rotatable about the axis for selectively varying a degree of alignment between respective orifices in the valve seat and valve member. The turbine includes a nozzle having a vane assembly. In one embodiment the vane assembly has only fixed vanes. In another embodiment the vane assembly includes both fixed vanes and variable vanes, and the variable vanes are part of a rotor that rotates together with the rotary valve member.
摘要翻译： 涡轮增压器包括环形旁路通道，以允许废气绕过涡轮机叶轮。 环形旁通阀设置在旁通通道中。 旁通阀包括固定环形阀座和与阀座同轴布置的旋转环形阀构件。 阀构件设置成抵靠阀座并且可围绕轴线旋转，以选择性地改变阀座和阀构件中各个孔口之间的对准程度。 涡轮机包括具有叶片组件的喷嘴。 在一个实施例中，叶片组件仅具有固定叶片。 在另一个实施例中，叶片组件包括固定叶片和可变叶片，并且可变叶片是与旋转阀构件一起旋转的转子的一部分。
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