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61. 发明公开

EP3264204A3 A CONFIGURABLE AUTOMOTIVE CONTROLLER 有权转让
标题翻译：可配置的汽车控制器
公开(公告)号：EP3264204A3
公开(公告)日：2018-01-17
申请号：EP17184543.1
申请日：2009-07-02
申请人： Honeywell International Inc.
发明人： STEWART, Greg , BORRELLI, Francesco , PEKAR, Jaroslav
IPC分类号： G05B13/04 , G05B15/02
CPC分类号： G05B13/048 , G05B15/02
摘要： An engine control unit (31) having a one-time integration of a model predictive control template via a potentially long software process. Changes to a control structure (42) may subsequently be made via a calibration dataset (39) connected to the engine control unit (31) without incurring the potentially long and laborious software process of implementing the template of other approaches in the related art.
摘要翻译：一种发动机控制单元（31），其通过潜在的长软件过程一次性集成模型预测控制模板。随后可以通过连接到发动机控制单元（31）的校准数据集（39）进行对控制结构（42）的改变，而不会导致在相关领域中实现其他方法的模板的潜在漫长和费力的软件过程。

62. 发明公开

EP2738369A3 Suction sealing for turbocharger 有权转让
标题翻译：涡轮增压器的吸气密封
公开(公告)号：EP2738369A3
公开(公告)日：2017-12-27
申请号：EP13190943.4
申请日：2013-10-30
申请人： Honeywell International Inc.
发明人： Gupta, Suryakant , Mulani, Parikshit I , John, Poomkuzhimannil Zachariah , Surendran, Anish , Gupta, Anish Kumar , Nambi, Sundaravel , V, Santosh Kumar
IPC分类号： F02C6/12 , F01D11/00
CPC分类号： F02B37/18 , F01D11/00 , F02B37/186 , F02C6/12 , F05D2220/40 , Y02T10/144
摘要： A system can include a turbine housing that defines a turbine wheel space, an exhaust chamber in fluid communication with the turbine wheel space and a control shaft bore that extends from the exhaust chamber to an outer surface of the turbine housing; a blunt body positionable above the turbine wheel space where the blunt body includes an opening and a lumen in fluid communication with the opening; and a suction conduit connectable for fluid communication between the control shaft bore of the turbine housing and the lumen of the blunt body. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译：系统可以包括限定涡轮机叶轮空间的涡轮机壳体，与涡轮机叶轮空间流体连通的排气室和从排气室延伸到涡轮机壳体的外表面的控制轴孔; 可定位在涡轮机叶轮空间上方的钝体，其中钝体包括开口和与开口流体连通的内腔; 以及可连接用于在涡轮机壳体的控制轴孔与钝头体的内腔之间流体连通的抽吸导管。还公开了装置，组件，系统，方法等的各种其他示例。

63. 发明公开

EP2573362A3 Turbocharger comprising a sleeve 失效转让
标题翻译：包括套筒的涡轮增压器
公开(公告)号：EP2573362A3
公开(公告)日：2017-12-27
申请号：EP12184568.9
申请日：2012-09-14
申请人： Honeywell International Inc.
发明人： Kocher, Ryan Matthew , Maynigo, Corazon , Thompson, Glenn F.
IPC分类号： F02C6/12 , F01D25/18
CPC分类号： F04D29/102 , F01D25/14 , F01D25/18 , F02B37/00 , F02C6/12 , F04D29/668 , F16C19/184 , F16C35/077 , F16C2360/24 , Y02T10/144 , Y10T29/4932
摘要： A turbocharger rotating assembly includes a bearing; a shaft and turbine wheel assembly supported by the bearing; a seal ring disposed about the shaft; and a sleeve that supports the bearing and that includes a compressor end and a turbine end, a bore extending axially from the compressor end to the turbine end, a first counter bore that forms an axial face that axially locates the bearing in the bore, a second counter bore disposed axially between the first counter bore and the turbine end wherein the second counter bore comprises a seal surface that forms a lubricant and exhaust seal with the seal ring disposed about the shaft, and a securing feature to secure the sleeve with respect to a turbocharger housing. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译：涡轮增压器旋转组件包括轴承; 由所述轴承支撑的轴和涡轮机叶轮组件; 围绕所述轴布置的密封环; 所述套筒支撑所述轴承并且包括压缩机端和涡轮机端，从所述压缩机端向所述涡轮机端轴向延伸的孔，形成将所述轴承轴向定位在所述孔中的轴向面的第一沉孔，第二沉孔轴向地设置在第一沉孔与涡轮端之间，其中第二沉孔包括密封表面，该密封表面与围绕轴布置的密封环形成润滑剂和排气密封;以及固定特征，以相对于轴涡轮增压器壳体。还公开了装置，组件，系统，方法等的各种其他示例。

64. 发明授权

EP2351911B1 VARIABLE GEOMETRY VANE ASSEMBLY FOR A TURBOCHARGER 有权转让
标题翻译：用于涡轮增压器的可变几何叶片组件
公开(公告)号：EP2351911B1
公开(公告)日：2017-11-29
申请号：EP10196275.1
申请日：2010-12-21
申请人： Honeywell International Inc.
发明人： Espasa, Olivier , Barthelet, Pierre , Mailfert, Julien
IPC分类号： F01D17/16
CPC分类号： F01D17/165 , F05D2220/40 , F05D2260/30 , F05D2260/37 , F05D2260/56
摘要： A variable-vane assembly for a variable nozzle turbine comprises a nozzle ring supporting a plurality of vanes affixed to vane arms that are engaged in recesses in the inner edge of a unison ring. The unison ring is rotatable about the axis of the nozzle ring so as to pivot the vane arms, thereby pivoting the vanes in unison. The unison ring is radially restrained by a combination of radial guide rollers and fixed axial-radial guide pins secured to the nozzle ring, and is axially restrained by one or more axial stops affixed to the nozzle ring.

65. 发明授权

EP2808513B1 Valve seat and gasket for exhaust bypass valve 失效转让
标题翻译：用于排气旁通阀的阀座和垫圈
公开(公告)号：EP2808513B1
公开(公告)日：2017-11-22
申请号：EP14167963.9
申请日：2014-05-12
申请人： Honeywell International Inc.
发明人： Jeanson, Arthur , Perrin, Jean-Luc , Bodin, Jean-Yves
IPC分类号： F02B37/00 , F02B37/013 , F02B37/18 , F02M26/65 , F16L17/035 , F16L23/04
CPC分类号： F02M25/0787 , F02B37/004 , F02B37/013 , F02B37/183 , F02M26/65 , F16L17/035 , F16L23/04 , Y02T10/144
摘要： An assembly can include a valve seat for an exhaust bypass valve of a serial turbocharger system; and a gasket that includes a planar portion that defines a perimeter and that includes a tab that extends from the perimeter of the planar portion for engagement with the valve seat to secure the gasket to the valve seat. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.

66. 发明授权

EP2915975B1 TURBOCHARGER TURBINE WASTEGATE MECHANISM 有权转让
标题翻译：涡轮增压器涡轮机废弃机构
公开(公告)号：EP2915975B1
公开(公告)日：2017-10-04
申请号：EP15155299.9
申请日：2015-02-16
申请人： Honeywell International Inc.
发明人： Micanek, Vit , Cizek, Petr , Hahn, Stanislav
IPC分类号： F02B37/18 , F02C6/12
CPC分类号： F02B37/186 , F01D17/105 , F01D17/141 , F01D25/24 , F02B47/08 , F02C6/12 , F05D2220/40 , F05D2260/52 , F05D2260/57 , Y02T10/121 , Y02T10/144
摘要： An assembly can include a turbine housing (210, 810) that includes a bore (212), a wastegate seat (226) and a wastegate passage that extends to the wastegate seat; a bushing (242) configured for receipt by the bore; a rotatable wastegate shaft (252) configured for receipt by the bushing; a wastegate plug (256) extending from the wastegate shaft; a control arm (244, 844) operatively coupled to the wastegate shaft (244); a control linkage (803) operatively coupled to the control arm (844) where the control linkage includes a control axis; an actuator (801) operatively coupled to the control linkage for translation of the control linkage in a direction of the control axis; and a biasing mechanism (910) operatively coupled to the control linkage where the biasing mechanism applies an off-axis force to the control linkage. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译：组件可以包括涡轮机壳体（210,810），其包括孔（212），废气门座（226）和延伸至废气门座的废气门通道; 衬套（242），其构造成用于由所述孔容纳; 可旋转废气门轴（252），所述可旋转废气门轴（252）构造成由所述衬套接收; 废气门塞（256），其从废气门轴延伸; 控制臂（244,844），其可操作地联接到废气门轴（244）; 控制联动装置（803），其可操作地联接至所述控制臂（844），其中所述控制联动装置包括控制轴线; 致动器（801），所述致动器（801）操作性地联接到所述控制联动装置，以及可操作地联接到控制联动装置的偏置机构（910），其中偏置机构将偏轴力施加到控制联动装置。还公开了装置，组件，系统，方法等的各种其他示例。

67. 发明授权

EP2894297B1 Turbine shroud contour exducer relief 有权转让
标题翻译：涡轮护罩轮廓导出装置
公开(公告)号：EP2894297B1
公开(公告)日：2017-09-27
申请号：EP14193961.1
申请日：2014-11-19
申请人： Honeywell International Inc.
发明人： Alexander, Brian
IPC分类号： F01D5/04 , F01D9/04 , F01D25/24
CPC分类号： F01D25/24 , F01D5/043 , F01D9/04 , F05D2220/40 , Y10T29/49243
摘要： A turbocharger turbine having a blade-gap zone between the blades and the shroud wall. The blade-gap zone is larger at and near the exducer than at an upstream location where the shroud wall is at its minimum radius. Also disclosed is a method of customizing and manufacturing a turbine by establishing an optimized blade-gap zone at the exducer, and machining it into a turbine housing.
摘要翻译：涡轮增压器涡轮在叶片和护罩壁之间具有叶片间隙区域。叶片间隙区域在出口器处和附近比在护罩壁处于其最小半径的上游位置处更大。还公开了一种定制和制造涡轮机的方法，其通过在出口器处建立优化的叶片间隙区并将其加工到涡轮机壳体中。

68. 发明公开

EP3205863A1 SYSTEM AND METHOD FOR ESTIMATING TURBO SPEED OF AN ENGINE 审中-实审转让
标题翻译：用于估算发动机涡轮转速的系统和方法
公开(公告)号：EP3205863A1
公开(公告)日：2017-08-16
申请号：EP17152074.5
申请日：2017-01-18
申请人： Honeywell International Inc.
发明人： PACHNER, Daniel , LIU, Yuejiang , BRULHART, Francois-Xavier , UCHANSKI, Michael Robert
IPC分类号： F02D41/00
CPC分类号： F02D41/0007 , F02D2041/1416 , F02D2041/1433 , F02D2200/0402 , F02D2200/0404 , F02D2200/0406 , F02D2200/0414 , Y02T10/144
摘要： The speed of a turbocharger may be estimated using data from sensors that are readily available in most engine management systems. In some cases, a pressure measurement from a MAP sensor may be used, in combination with one or more computational models, to provide an efficient, lower cost estimate of turbo speed that can be used to control operation of the engine and/or the turbocharger.
摘要翻译：涡轮增压器的速度可以使用来自大多数发动机管理系统中容易获得的传感器的数据来估算。在一些情况下，可以使用来自MAP传感器的压力测量结合一个或多个计算模型来提供可用于控制发动机和/或涡轮增压器的操作的涡轮速度的高效，低成本估计。

69. 发明授权

EP2828500B1 TURBOCHARGER CARTRIDGE AND ENGINE CYLINDER HEAD ASSEMBLY 有权转让
公开(公告)号：EP2828500B1
公开(公告)日：2017-08-09
申请号：EP13765202.0
申请日：2013-03-08
申请人： Honeywell International Inc.
发明人： MARQUES, Manuel , LADONNET, Michael , LOMBARD, Alain , KURTZMANN, Johann
IPC分类号： F02B39/00 , F02B39/16 , F02B37/00 , F02F1/24
CPC分类号： F02B37/00 , F01D25/24 , F01N13/105 , F01N13/1805 , F02B37/18 , F02B39/14 , F02B67/10 , F02C6/12 , F02F1/24 , F05D2230/51 , F05D2230/52 , F05D2260/98

70. 发明公开

EP3179069A2 EXHAUST BYPASS VALVE OF MULTI-STAGE TURBOCHARGER 有权转让
标题翻译： ABGASUMGEHUNGSVENTIL EINES MEHRSTUFIGEN TURBOLADERS
公开(公告)号：EP3179069A2
公开(公告)日：2017-06-14
申请号：EP16196441.6
申请日：2016-10-28
申请人： Honeywell International Inc.
发明人： JEANSON, Arthur , CHAMMAS, Bassam , PERRIN, Jean-Luc
IPC分类号： F02B37/00 , F01D11/00 , F02B37/013 , F02B37/18
CPC分类号： F02B37/186 , F01D11/00 , F01D17/141 , F01D17/146 , F01D25/30 , F02B37/004 , F02B37/013 , F02C6/12 , F05D2220/40 , Y02T10/144
摘要： An assembly for a two-stage turbocharger can include a first turbocharger stage and a second turbocharger stage where one of the stages includes a boss that includes a bore; an exhaust bypass valve that includes an arm pivotable to orient the exhaust bypass valve in an open state and a closed state; a valve shaft disposed at least in part in the bore and operatively coupled to the exhaust bypass valve where the valve shaft includes an inner end, an outer end and an axial stop disposed between the inner end and the outer end; an outer bushing disposed at least in part in the bore and located axially along the valve shaft; and an inner bushing disposed at least in part in the bore and located axially along the valve shaft between the axial stop and a portion of the arm of the exhaust bypass valve.
摘要翻译：用于两级涡轮增压器的组件可以包括第一涡轮增压器级和第二涡轮增压器级，其中一级包括具有孔的凸台; 排气旁通阀，其包括可枢转以使排气旁通阀处于打开状态和关闭状态的臂; 阀轴至少部分地设置在所述孔中并且可操作地联接到所述排气旁通阀，其中所述阀轴包括内端，外端和设置在所述内端和所述外端之间的轴向止动件; 至少部分地设置在所述孔中并沿着所述阀轴轴向设置的外套筒; 以及内衬套，其至少部分地设置在所述孔中，并且在所述轴向止挡件和所述排气旁通阀的臂的一部分之间沿着所述阀轴轴向设置。

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