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1. 发明申请

WO2013173220A1 TURBOCHARGER WITH JOURNAL BEARING 审中-公开
标题翻译：涡轮增压器与日本轴承
公开(公告)号：WO2013173220A1
公开(公告)日：2013-11-21
申请号：PCT/US2013/040758
申请日：2013-05-13
申请人： HONEYWELL INTERNATIONAL INC.
发明人： DAGUIN, Frederic , CASTAN, Joel , VAZEILLE, Nicolas , ARMAND, Dominique , LIU, Steven , CHEN, Yong, Jun , ADACHI, Shinichi
IPC分类号： F02B39/00 , F02B39/14 , F02C7/06 , F16C17/00
CPC分类号： F04D29/056 , F01D25/162 , F01D25/166 , F02B37/00 , F02B37/16 , F05D2220/40 , F05D2260/36 , F16C17/10 , F16C27/045 , F16C33/1065 , F16C33/1085 , F16C35/02 , F16C2226/50 , F16C2360/24 , Y02T10/144
摘要： A turbocharger assembly can include a housing with a through bore and an axial face disposed in the through bore; a locating plate with a keyed opening attached to the housing; and a journal bearing disposed in the through bore where the journal bearing includes a keyed compressor end and an enlarged outer portion defined between two axial faces by an outer diameter and an axial length where the axial face disposed in the through bore of the housing, the locating plate, and the two axial faces of the journal bearing axially locate the journal bearing in the through bore and where the keyed opening of the locating plate and the keyed compressor end of the journal bearing azimuthally locate the journal bearing in the through bore. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译：涡轮增压器组件可以包括具有通孔的壳体和设置在通孔中的轴向面; 具有附接到所述壳体的带键的定位板; 以及设置在所述通孔中的轴颈轴承，其中所述轴颈轴承包括键合的压缩机端部和限定在两个轴向面之间的扩大的外部部分，所述外部部件的外径和轴向长度设置在所述壳体的通孔中，定位板，并且轴颈轴承的两个轴向面轴向地将轴颈轴承定位在通孔中，定位板的带键开口和轴颈轴承的键合压缩机端部将轴颈轴承定位在通孔中。还公开了装置，组件，系统，方法等的各种其它示例。

2. 发明申请

WO2016171933A1 TURBOCHARGER SPRING ASSEMBLY 审中-公开
标题翻译：涡轮增压器组件
公开(公告)号：WO2016171933A1
公开(公告)日：2016-10-27
申请号：PCT/US2016/026872
申请日：2016-04-11
申请人： HONEYWELL INTERNATIONAL INC.
发明人： HETTINGER, Raphael , BOILEAU, Raphael , DAGUIN, Frederic , MOLINA, Jose Antonio , MORINIGO, Tomas
IPC分类号： F02B39/00 , F01D25/16 , F16C19/06
CPC分类号： F01D25/164 , F02C6/12 , F02C7/06 , F05D2220/40 , F05D2240/54 , F05D2260/602 , F05D2300/43 , F16C19/163 , F16C19/548 , F16C25/083 , F16C33/6659 , F16C2360/24
摘要： A turbo charger bearing assembly comprising a spacer that comprises an axial through bore, a compressor side surface and a turbine side surface. The compressor side surface faces an outer race of a compressor side rolling element bearing. The turbine side surface faces an outer race of a turbine side rolling element bearing. The spacer further includes a spring that is seated between first and second end caps disposed in part in the axial through bore of the spacer. The spring biases an axially facing surface of the first end cap against the outer race surface of the compressor side rolling element bearing, and the second end cap against the outer race surface of the turbine side rolling element bearing.
摘要翻译：一种涡轮增压器轴承组件，包括包括轴向通孔，压缩机侧表面和涡轮机侧表面的间隔件。压缩机侧面与压缩机侧滚动体轴承的外圈面对。涡轮机侧面面对涡轮机侧滚动体轴承的外圈。间隔件还包括一个位于第一和第二端盖之间的弹簧，该第一和第二端帽部分地设置在间隔件的轴向通孔中。弹簧将第一端盖的轴向面向压缩机侧滚动体轴承的外圈面偏压，并且第二端盖抵靠涡轮侧滚动体轴承的外圈面。

3. 发明公开

EP2850300A1 TURBOCHARGER WITH JOURNAL BEARING 有权转让
标题翻译： TURBOLADER MIT GLEITLAGER
公开(公告)号：EP2850300A1
公开(公告)日：2015-03-25
申请号：EP13790839.8
申请日：2013-05-13
申请人： Honeywell International Inc.
发明人： DAGUIN, Frederic , CASTAN, Joel , VAZEILLE, Nicolas , ARMAND, Dominique , LIU, Steven , CHEN, Yong, Jun , ADACHI, Shinichi
IPC分类号： F02B39/00 , F02B39/14 , F02C7/06 , F16C17/00
CPC分类号： F04D29/056 , F01D25/162 , F01D25/166 , F02B37/00 , F02B37/16 , F05D2220/40 , F05D2260/36 , F16C17/10 , F16C27/045 , F16C33/1065 , F16C33/1085 , F16C35/02 , F16C2226/50 , F16C2360/24 , Y02T10/144
摘要： A turbocharger assembly can include a housing with a through bore and an axial face disposed in the through bore; a locating plate with a keyed opening attached to the housing; and a journal bearing disposed in the through bore where the journal bearing includes a keyed compressor end and an enlarged outer portion defined between two axial faces by an outer diameter and an axial length where the axial face disposed in the through bore of the housing, the locating plate, and the two axial faces of the journal bearing axially locate the journal bearing in the through bore and where the keyed opening of the locating plate and the keyed compressor end of the journal bearing azimuthally locate the journal bearing in the through bore. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
摘要翻译：涡轮增压器组件可以包括具有通孔的壳体和设置在通孔中的轴向面; 具有附接到所述壳体的带键的定位板; 以及设置在所述通孔中的轴颈轴承，其中所述轴颈轴承包括键合的压缩机端和限定在两个轴向面之间的扩大的外部，所述外部部分具有设置在所述壳体的通孔中的轴向面的外径和轴向长度，定位板，并且轴颈轴承的两个轴向面轴向地将轴颈轴承定位在通孔中，定位板的带键开口和轴颈轴承的键合压缩机端部将轴颈轴承定位在通孔中。还公开了装置，组件，系统，方法等的各种其它示例。

4. 发明公开

EP3244027A1 TURBOCHARGER ASSEMBLY 有权转让
标题翻译：涡轮增压器总成
公开(公告)号：EP3244027A1
公开(公告)日：2017-11-15
申请号：EP17166958.3
申请日：2017-04-18
申请人： Honeywell International Inc. , BMW AG
发明人： HETTINGER, Raphael , DAGUIN, Frederic , BOILEAU, Raphael , CAPELLI, Magali , SIMON, Pascal , GAINETON, Nicolas , BLUMENSCHEIN, Erich , HOFER, Raphael , REICHHART, Michael , RISCH, Georg , STEINWENDER, Lorenz , GRUN, Florian , GODOR, Istvan
IPC分类号： F01D25/16 , F02C6/12 , F01D25/18
CPC分类号： F02B39/14 , F01D25/125 , F01D25/16 , F01D25/164 , F01D25/168 , F01D25/183 , F01D25/186 , F01D25/24 , F02B33/40 , F02C6/12 , F05D2220/40 , F05D2240/53 , F05D2240/54 , F16C19/548 , F16C33/1085 , F16C33/586 , F16C33/66 , F16C2360/24
摘要： A turbocharger system can include a housing that includes a through bore, a plurality of lubricant bores, a plurality of lubricant bore to through bore openings and a recessed compressor-side surface that defines in part a passage that fluidly couples at least two of the lubricant bores; a rolling element bearing unit disposed at least in part in the through bore of the housing; and, a plate that covers at least a portion of the recessed compressor-side surface of the housing.
摘要翻译：涡轮增压器系统可以包括壳体，该壳体包括通孔，多个润滑剂孔，通向通孔开口的多个润滑剂孔以及凹入的压缩机侧表面，所述凹入的压缩机侧表面部分地限定流体地联接至少两个润滑剂孔; 滚动元件轴承单元，其至少部分地设置在壳体的通孔中; 以及覆盖壳体的凹入的压缩机侧表面的至少一部分的板。

5. 发明公开

EP3231992A1 TURBOCHARGER COMPRESSOR WHEEL ASSEMBLY 审中-公开
标题翻译：涡轮增压器压缩机轮组件
公开(公告)号：EP3231992A1
公开(公告)日：2017-10-18
申请号：EP17156795.1
申请日：2017-02-17
申请人： Honeywell International Inc.
发明人： DAGUIN, Frederic , REMY, Bernard , PERRIN, Jean-Luc , CASTAN, Joel , ARMAND, Dominique
IPC分类号： F01D5/02 , F16D1/072 , F16D1/076 , F16B19/05
摘要： A compressor wheel assembly of a turbocharger can include a compressor wheel that includes a through bore that extends from a base portion to a nose portion of the compressor wheel; a turbocharger shaft disposed in the through bore of the compressor wheel where the turbocharger shaft includes an end portion that extends axially away from the nose portion of the compressor wheel; and a swaged collar fixed to the end portion of the turbocharger shaft.
摘要翻译：涡轮增压器的压缩机叶轮组件可以包括压缩机叶轮，该压缩机叶轮包括从压缩机叶轮的基部部分延伸到鼻部部分的通孔; 设置在压缩机叶轮的通孔中的涡轮增压器轴，其中涡轮增压器轴包括远离压缩机叶轮的鼻部部分轴向延伸的端部; 以及固定到涡轮增压器轴的端部的锻造套环。

6. 发明公开

EP3081769A1 TURBOCHARGER BEARING ASSEMBLY 有权转让
标题翻译： LAGERANORDNUNGFÜRTURBOLADER
公开(公告)号：EP3081769A1
公开(公告)日：2016-10-19
申请号：EP16163758.2
申请日：2016-04-04
申请人： Honeywell International Inc.
发明人： HETTINGER, Raphael , BOILEAU, Raphael , DAGUIN, Frederic
IPC分类号： F01D25/16
CPC分类号： F02B39/14 , F01D25/164 , F01D25/166 , F01D25/18 , F05D2220/40 , F05D2240/53 , F05D2240/54 , F16C19/548 , F16C25/083 , F16C27/045 , F16C35/077 , F16C2360/24
摘要： An assembly can include a turbocharger center housing (280) that includes a through bore (796) and a counterbore (798) positioned between a compressor end and a turbine end of the through bore where the through bore (796) includes a sleeve mating surface (795) positioned between the compressor end and the counterbore (798) and a turbine side bearing lubricant film formation surface positioned between the counterbore (798) and the turbine end; and a sleeve (703) positioned at least in part in the through bore (796) of the turbocharger center housing (280) between the compressor end and the counterbore (798) where the sleeve (703) includes a locating flange (710) and an axial extension (714 716) that extends from the locating flange (710) where the axial extension includes an outer mating surface (720), an inner compressor side bearing lubricant film formation surface (752, 756), a compressor side axially facing spacer surface (757) and a turbine side axially facing spacer surface (760).
摘要翻译：组件可以包括涡轮增压器中心壳体（280），其包括定位在通孔的压缩机端和涡轮机端之间的通孔（796）和沉孔（798），其中通孔（796）包括套管配合表面（795）和位于所述沉孔（798）和所述涡轮机端之间的涡轮机侧轴承润滑剂膜形成表面; 以及至少部分地位于所述压缩机端和所述沉孔（798）之间的所述涡轮增压器中心壳体（280）的通孔（796）中的套筒（703），其中所述套筒（703）包括定位凸缘（710）和从所述定位凸缘（710）延伸的轴向延伸部（714,716），其中所述轴向延伸部包括外配合表面（720），内压缩机侧承载润滑剂膜形成表面（752,756），压缩机侧轴向间隔件表面（757）和涡轮机侧轴向面对的间隔件表面（760）。

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