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公开(公告)号：US20090272112A1
公开(公告)日：2009-11-05
申请号：US12115245
申请日：2008-05-05
CPC分类号： F01D11/00 , F01D17/165 , F02C6/12 , F02C9/22 , F05D2220/40
摘要： A variable nozzle for a turbocharger includes a plurality of vanes rotatably mounted on a nozzle ring and disposed in a nozzle flow path defined between the nozzle ring and an opposite nozzle wall. Either or both of the faces of the nozzle ring and nozzle wall include(s) at least one step that defines sealing surfaces positioned to be substantially abutted by airfoil surfaces of the vanes in the closed position of the vanes and to be spaced from the airfoil surfaces in positions other than the closed position. This substantial abutment between the airfoil surfaces and the sealing surfaces serves to substantially prevent exhaust gas from leaking past the ends of the airfoil portions. At the same time, clearances between the nozzle ring face and the end faces of the airfoil portions can be sufficiently large to prevent binding of the vanes under all operating conditions.
摘要翻译： 用于涡轮增压器的可变喷嘴包括可旋转地安装在喷嘴环上并且设置在限定在喷嘴环和相对的喷嘴壁之间的喷嘴流动路径中的多个叶片。 喷嘴环和喷嘴壁的任何一个或两个表面包括至少一个台阶，其限定密封表面，该密封表面定位成在叶片的关闭位置基本上与叶片的翼型表面邻接并且与叶片间隔开 在关闭位置以外的位置的表面。 翼型件表面和密封表面之间的这种实质的邻接用于基本上防止废气从机翼部分的端部泄漏。 同时，喷嘴环面和翼型部分的端面之间的间隙可以足够大，以防止在所有操作条件下叶片的结合。
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公开(公告)号：US08056336B2
公开(公告)日：2011-11-15
申请号：US12115245
申请日：2008-05-05
IPC分类号： F02D23/00 , F01B25/02 , F01D17/12 , F03D7/00 , F03D5/00 , F03B1/00 , F03B11/02 , F04D15/00 , F04D27/00 , F04D29/44 , F04D29/56 , F04D29/54
CPC分类号： F01D11/00 , F01D17/165 , F02C6/12 , F02C9/22 , F05D2220/40
摘要： A variable nozzle for a turbocharger includes a plurality of vanes rotatably mounted on a nozzle ring and disposed in a nozzle flow path defined between the nozzle ring and an opposite nozzle wall. Either or both of the faces of the nozzle ring and nozzle wall include(s) at least one step that defines sealing surfaces positioned to be substantially abutted by airfoil surfaces of the vanes in the closed position of the vanes and to be spaced from the airfoil surfaces in positions other than the closed position. This substantial abutment between the airfoil surfaces and the sealing surfaces serves to substantially prevent exhaust gas from leaking past the ends of the airfoil portions. At the same time, clearances between the nozzle ring face and the end faces of the airfoil portions can be sufficiently large to prevent binding of the vanes under all operating conditions.
摘要翻译： 用于涡轮增压器的可变喷嘴包括可旋转地安装在喷嘴环上并且设置在限定在喷嘴环和相对的喷嘴壁之间的喷嘴流动路径中的多个叶片。 喷嘴环和喷嘴壁的任何一个或两个表面包括至少一个台阶，其限定密封表面，该密封表面定位成在叶片的关闭位置基本上与叶片的翼型表面邻接并且与叶片间隔开 在关闭位置以外的位置的表面。 翼型件表面和密封表面之间的这种实质的邻接用于基本上防止废气从机翼部分的端部泄漏。 同时，喷嘴环面和翼型部分的端面之间的间隙可以足够大，以防止在所有操作条件下叶片的结合。
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公开(公告)号：US20130078083A1
公开(公告)日：2013-03-28
申请号：US13245218
申请日：2011-09-26
申请人： Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Denis Jeckel , Dominique Petitjean , Philippe Arnold , Karl-Heinz Bauer
发明人： Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Denis Jeckel , Dominique Petitjean , Philippe Arnold , Karl-Heinz Bauer
CPC分类号： F01D11/02 , F01D17/165 , F02C6/12 , F05D2220/40
摘要： A variable nozzle for a turbocharger includes a plurality of vanes rotatably mounted on a nozzle ring and disposed in a nozzle flow path defined between the nozzle ring and an opposite nozzle wall. Either or both of the faces of the nozzle ring and nozzle wall include(s) grooves extending substantially transverse to a general flow direction of the flow through the nozzle, and there are clearances between the ends of the vanes and the adjacent faces. Leakage flow through the clearance between the end of each vane and the adjacent face having the grooves must proceed across the grooves, and thus a labyrinthine flow passage is presented to the leakage flow. The labyrinthine passage has a greater resistance to flow than would be the case without the grooves. Accordingly, leakage flow is reduced, which is beneficial to turbine efficiency.
摘要翻译： 用于涡轮增压器的可变喷嘴包括可旋转地安装在喷嘴环上并且设置在限定在喷嘴环和相对的喷嘴壁之间的喷嘴流动路径中的多个叶片。 喷嘴环和喷嘴壁的一个或两个表面包括基本上横向于通过喷嘴的流动的大致流动方向延伸的槽，并且在叶片的端部和相邻的面之间存在间隙。 通过每个叶片的端部与具有凹槽的相邻面之间的间隙的泄漏流必须经过沟槽，并且因此向泄漏流提供迷宫式流路。 迷宫通道比没有凹槽的情况具有更大的阻力。 因此，泄漏流量减少，这有利于涡轮机的效率。
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公开(公告)号：US20130078082A1
公开(公告)日：2013-03-28
申请号：US13245263
申请日：2011-09-26
申请人： Philippe Arnold , Denis Jeckel , Dominique Petitjean , Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Karl-Heinz Bauer , Chris Groves
发明人： Philippe Arnold , Denis Jeckel , Dominique Petitjean , Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Karl-Heinz Bauer , Chris Groves
IPC分类号： F01D17/12
CPC分类号： F01D17/16 , F02C6/12 , F05D2240/12
摘要： A variable-nozzle assembly for a turbocharger includes 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. A unison ring engages vane arms that are affixed to axles of the vanes, such that rotation of the unison ring causes the vanes to pivot between a closed position and an open position. The vanes have proximal ends that are adjacent a face of the nozzle ring. A vane sealing member is supported on the nozzle ring and has a portion disposed between the proximal ends of the vanes and the face of the nozzle ring. The unison ring includes cams that engage cam followers. Rotational movement of the unison ring causes the cam followers to be moved axially and thereby urge the vane sealing member against the proximal ends of the vanes.
摘要翻译： 用于涡轮增压器的可变喷嘴组件包括大致环形的喷嘴环和可旋转地安装到喷嘴环的叶片阵列，使得叶片可围绕它们的轴线枢转以调节到涡轮机叶轮的排气流。 协调环接合固定到叶片的轴的叶片臂，使得协调环的旋转导致叶片在关闭位置和打开位置之间枢转。 叶片具有邻近喷嘴环的表面的近端。 叶片密封构件支撑在喷嘴环上，并且具有设置在叶片的近端和喷嘴环的表面之间的部分。 协调环包括接合凸轮从动件的凸轮。 协调环的旋转运动导致凸轮从动件轴向移动，从而推动叶片密封构件抵靠叶片的近端。
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公开(公告)号：US20110176907A1
公开(公告)日：2011-07-21
申请号：US12689895
申请日：2010-01-19
申请人： Chris Groves , Mark Groskreutz , Dominique Petitjean , Anthony Ruquart , Philippe Arnold , Guillaume Dupont , Baptiste Szczyrba
发明人： Chris Groves , Mark Groskreutz , Dominique Petitjean , Anthony Ruquart , Philippe Arnold , Guillaume Dupont , Baptiste Szczyrba
CPC分类号： F04D25/04 , F01D25/166 , F01D25/18 , F04D29/0563 , F05D2220/40 , F05D2240/52 , F05D2240/53 , F05D2240/54 , F05D2300/50212 , F16C17/10 , F16C17/243 , F16C27/02 , F16C33/1065 , F16C2360/24
摘要： An exemplary multi-piece bearing for a turbocharger includes a cylindrical piece that has a coefficient of thermal expansion, opposing ends and an outer surface and an inner surface that extend between the opposing ends where the outer surface includes one or more lubricant openings; an end piece that has a different coefficient of thermal expansion and a face where the face includes one or more lubricant openings; and lubricant passages formed by the cylindrical piece and the end piece for passage of lubricant between the one or more lubricant openings of the outer surface of the cylindrical piece and the one or more lubricant openings of the face of the end piece. As described herein, such an exemplary multi-piece bearing can, upon selection of coefficients of thermal expansion, help maintain axial clearances between various components during operation of a turbocharger. Other exemplary bearings, arrangements and methods are also disclosed.
摘要翻译： 用于涡轮增压器的示例性多件式轴承包括具有热膨胀系数，相对端和外表面的圆柱形件和在外表面包括一个或多个润滑剂开口的相对端之间延伸的内表面; 具有不同热膨胀系数的端片和面包括一个或多个润滑剂开口的面; 以及由圆柱形件和端件形成的用于使润滑剂在圆柱形件的外表面的一个或多个润滑剂开口与端件件的表面的一个或多个润滑剂开口之间形成的润滑剂通道。 如本文所述，这种示例性多件式轴承可以在选择热膨胀系数时有助于在涡轮增压器的运行期间维持各种部件之间的轴向间隙。 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：US09097120B2
公开(公告)日：2015-08-04
申请号：US12869307
申请日：2010-08-26
申请人： Dominique Petitjean , Guillaume Dupont , Anthony Ruquart , Philippe Arnold , Manimurugan Palaniyappan , Manuel Marques , Jean-Jacques Laissus , Raphael Ceotto
发明人： Dominique Petitjean , Guillaume Dupont , Anthony Ruquart , Philippe Arnold , Manimurugan Palaniyappan , Manuel Marques , Jean-Jacques Laissus , Raphael Ceotto
CPC分类号： F01D9/026 , F01D9/045 , F01D21/045 , F01D25/24 , F05D2220/40 , F05D2230/21 , F05D2230/232 , F05D2230/54 , F05D2240/12
摘要： An assembly includes a cast cartridge component and a curved wall where the cast cartridge includes a base plate having an opening configured for receipt of a turbine wheel, an exhaust conduit having an inlet and an outlet, a cylindrical wall, and vanes disposed between the cylindrical wall and the base plate where adjacent vanes define throats; where the curved wall includes a proximal end and a distal end, and an upper edge and a lower edge; and where joinder of the proximal end and the outlet of the exhaust conduit, joinder of the upper edge and the cylindrical wall and joinder of the lower edge and the base plate forms a volute configured to direct exhaust received via the inlet to a turbine wheel via the throats. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译： 一种组件包括铸造筒部件和弯曲壁，其中铸造筒包括具有构造成用于接收涡轮机叶轮的开口的基板，具有入口和出口的排气导管，圆柱形壁和设置在圆柱形 壁和底板，其中相邻的叶片限定喉部; 其中弯曲的壁包括近端和远端，以及上边缘和下边缘; 并且其中排气管的近端和出口的接合，上边缘和圆柱形壁的接合以及下边缘和底板的接合形成蜗壳，其被构造成将经由入口接收的排气引导到涡轮机叶轮经由 喉咙 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：US20100061668A1
公开(公告)日：2010-03-11
申请号：US12208494
申请日：2008-09-11
IPC分类号： F16C19/14
CPC分类号： F16C33/1075 , F01D25/166 , F01D25/168 , F02C6/12 , F05D2220/40 , F16C17/047 , F16C17/10 , F16C27/02 , F16C33/106 , F16C2360/24 , Y10T29/49645
摘要： An exemplary bearing for a turbocharger includes one or more thrust pads where each thrust pad includes a portion of a conical well; and a through-bore that includes lubricant channels, each channel configured to direct lubricant from the bore to a corresponding conical well of a thrust pad. Other exemplary technologies are also disclosed.
摘要翻译： 用于涡轮增压器的示例性轴承包括一个或多个推力垫，其中每个止推垫包括锥形井的一部分; 以及包括润滑剂通道的通孔，每个通道构造成将润滑剂从孔引导到止推垫的相应锥形孔。 还公开了其它示例性技术。
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公开(公告)号：US08967956B2
公开(公告)日：2015-03-03
申请号：US13245263
申请日：2011-09-26
申请人： Philippe Arnold , Denis Jeckel , Dominique Petitjean , Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Karl-Heinz Bauer , Chris Groves
发明人： Philippe Arnold , Denis Jeckel , Dominique Petitjean , Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Karl-Heinz Bauer , Chris Groves
CPC分类号： F01D17/16 , F02C6/12 , F05D2240/12
摘要： A variable-nozzle assembly for a turbocharger includes 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. A unison ring engages vane arms that are affixed to axles of the vanes, such that rotation of the unison ring causes the vanes to pivot between a closed position and an open position. The vanes have proximal ends that are adjacent a face of the nozzle ring. A vane sealing member is supported on the nozzle ring and has a portion disposed between the proximal ends of the vanes and the face of the nozzle ring. The unison ring includes cams that engage cam followers. Rotational movement of the unison ring causes the cam followers to be moved axially and thereby urge the vane sealing member against the proximal ends of the vanes.
摘要翻译： 用于涡轮增压器的可变喷嘴组件包括大致环形的喷嘴环和可旋转地安装到喷嘴环的叶片阵列，使得叶片可围绕它们的轴线枢转以调节到涡轮机叶轮的排气流。 协调环接合固定到叶片的轴的叶片臂，使得协调环的旋转导致叶片在关闭位置和打开位置之间枢转。 叶片具有邻近喷嘴环的表面的近端。 叶片密封构件支撑在喷嘴环上，并且具有设置在叶片的近端和喷嘴环的表面之间的部分。 协调环包括接合凸轮从动件的凸轮。 协调环的旋转运动导致凸轮从动件轴向移动，从而推动叶片密封构件抵靠叶片的近端。
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9.发明授权公开(公告)号：US08967955B2
公开(公告)日：2015-03-03
申请号：US13245218
申请日：2011-09-26
申请人： Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Denis Jeckel , Dominique Petitjean , Philippe Arnold , Karl-Heinz Bauer
发明人： Pierre Barthelet , Emmanuel Severin , Nicolas Morand , Denis Jeckel , Dominique Petitjean , Philippe Arnold , Karl-Heinz Bauer
CPC分类号： F01D11/02 , F01D17/165 , F02C6/12 , F05D2220/40
摘要： A variable nozzle for a turbocharger includes a plurality of vanes rotatably mounted on a nozzle ring and disposed in a nozzle flow path defined between the nozzle ring and an opposite nozzle wall. Either or both of the faces of the nozzle ring and nozzle wall include(s) grooves extending substantially transverse to a general flow direction of the flow through the nozzle, and there are clearances between the ends of the vanes and the adjacent faces. Leakage flow through the clearance between the end of each vane and the adjacent face having the grooves must proceed across the grooves, and thus a labyrinthine flow passage is presented to the leakage flow. The labyrinthine passage has a greater resistance to flow than would be the case without the grooves. Accordingly, leakage flow is reduced, which is beneficial to turbine efficiency.
摘要翻译： 用于涡轮增压器的可变喷嘴包括可旋转地安装在喷嘴环上并且设置在限定在喷嘴环和相对的喷嘴壁之间的喷嘴流动路径中的多个叶片。 喷嘴环和喷嘴壁的一个或两个表面包括基本上横向于通过喷嘴的流动的大致流动方向延伸的槽，并且在叶片的端部和相邻的面之间存在间隙。 通过每个叶片的端部与具有凹槽的相邻面之间的间隙的泄漏流必须经过沟槽，并且因此向泄漏流提供迷宫式流路。 迷宫通道比没有凹槽的情况具有更大的阻力。 因此，泄漏流量减少，这有利于涡轮机的效率。
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公开(公告)号：US08534989B2
公开(公告)日：2013-09-17
申请号：US12689895
申请日：2010-01-19
申请人： Chris Groves , Mark Groskreutz , Dominique Petitjean , Anthony Ruquart , Philippe Arnold , Guillaume Dupont , Celine Szczyrba
发明人： Chris Groves , Mark Groskreutz , Dominique Petitjean , Anthony Ruquart , Philippe Arnold , Guillaume Dupont , Baptiste Szczyrba
IPC分类号： F04D29/056
CPC分类号： F04D25/04 , F01D25/166 , F01D25/18 , F04D29/0563 , F05D2220/40 , F05D2240/52 , F05D2240/53 , F05D2240/54 , F05D2300/50212 , F16C17/10 , F16C17/243 , F16C27/02 , F16C33/1065 , F16C2360/24
摘要： An exemplary multi-piece bearing for a turbocharger includes a cylindrical piece that has a coefficient of thermal expansion, opposing ends and an outer surface and an inner surface that extend between the opposing ends where the outer surface includes one or more lubricant openings; an end piece that has a different coefficient of thermal expansion and a face where the face includes one or more lubricant openings; and lubricant passages formed by the cylindrical piece and the end piece for passage of lubricant between the one or more lubricant openings of the outer surface of the cylindrical piece and the one or more lubricant openings of the face of the end piece. As described herein, such an exemplary multi-piece bearing can, upon selection of coefficients of thermal expansion, help maintain axial clearances between various components during operation of a turbocharger. Other exemplary bearings, arrangements and methods are also disclosed.
摘要翻译： 用于涡轮增压器的示例性多件式轴承包括具有热膨胀系数，相对端和外表面的圆柱形件和在外表面包括一个或多个润滑剂开口的相对端之间延伸的内表面; 具有不同热膨胀系数的端片和面包括一个或多个润滑剂开口的面; 以及由圆柱形件和端件形成的用于使润滑剂在圆柱形件的外表面的一个或多个润滑剂开口与端件件的表面的一个或多个润滑剂开口之间形成的润滑剂通道。 如本文所述，这种示例性多件式轴承可以在选择热膨胀系数时有助于在涡轮增压器的运行期间维持各种部件之间的轴向间隙。 还公开了其它示例性轴承，布置和方法。
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