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公开(公告)号：US10415599B2
公开(公告)日：2019-09-17
申请号：US14928743
申请日：2015-10-30
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Leon Hu , Dave R. Hanna , Jianwen James Yi , Eric Warren Curtis
IPC: F04D29/28 , F04D29/66 , F04D17/10 , F04D25/04 , F04D25/02 , F04D29/051 , F02C6/12 , F01D3/00 , F04D29/16 , F01D5/04
Abstract: Methods and systems are provided for a turbocharger system to reduce and balance axial thrust load on the turbine shaft and the associated bearing system and sealing. In one example, a partial back plate compressor may be used in combination with an axial turbine to reduce axial thrust load and to improve turbocharger transient response time. In another example, a regenerative turbocharger system with back-to-back turbo pump may be used to reduce and balance axial thrust load.
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公开(公告)号：US20170122339A1
公开(公告)日：2017-05-04
申请号：US14928743
申请日：2015-10-30
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Leon Hu , Dave R. Hanna , Jianwen James Yi , Eric Warren Curtis
CPC classification number: F04D29/662 , F01D3/00 , F01D5/048 , F02C6/12 , F04D17/10 , F04D25/024 , F04D25/045 , F04D29/051 , F04D29/162 , F04D29/284 , F05D2220/40 , F05D2260/15
Abstract: Methods and systems are provided for a turbocharger system to reduce and balance axial thrust load on the turbine shaft and the associated bearing system and sealing. In one example, a partial back plate compressor may be used in combination with an axial turbine to reduce axial thrust load and to improve turbocharger transient response time. In another example, a regenerative turbocharger system with back-to-back turbo pump may be used to reduce and balance axial thrust load.
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公开(公告)号：US09945258B2
公开(公告)日：2018-04-17
申请号：US14511987
申请日：2014-10-10
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Leon Hu , David R Hanna
IPC: F01D25/26
CPC classification number: F01D25/26 , F05D2220/40 , F05D2250/283 , F05D2250/61 , F05D2260/231
Abstract: Systems are provided for a reinforcement element coupled to a sheet metal turbine housing that imparts desirable thermal-protective and structurally strengthening characteristics to the housing layers. In one example, a system may include a turbine comprising a housing surrounding a turbine rotor, the housing having an outer layer surrounding an inner layer at a distance to form an intermediate space between the inner and outer layers. Moreover, disposed in the intermediate space is a reinforcement element coupled to the inner and outer layers, providing strength and consistent rigidity without a significant increase in weight to the housing.
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公开(公告)号：US20160146100A1
公开(公告)日：2016-05-26
申请号：US14709339
申请日：2015-05-11
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Ben Zhao , Leon Hu , Jianwen James Yi , Eric Warren Curtis , Jizhong Zhang
CPC classification number: F02B37/24 , F01D5/141 , F01D17/165 , F02B39/00 , F05D2210/30 , F05D2220/40 , F05D2240/12 , Y02T10/144
Abstract: Various systems and methods are described for a variable geometry turbine. In one example, a nozzle vane includes a stationary having a first cambered sliding surface and a sliding vane having a second cambered sliding surface where the second cambered sliding surface includes a flow disrupting feature in contact with the first sliding cambered surface. The sliding vane may be positioned to slide in a direction from substantially tangent along a curved path to an inner circumference of the turbine nozzle and selectively uncover the flow disrupting feature.
Abstract translation: 对于可变几何涡轮机描述了各种系统和方法。 在一个示例中，喷嘴叶片包括具有第一弧形滑动表面的静止件和具有第二弧形滑动表面的滑动叶片，其中第二弧形滑动表面包括与第一滑动弧形表面接触的流动中断特征。 滑动叶片可以定位成沿着弯曲路径从基本上切线到涡轮喷嘴的内圆周的方向滑动，并且选择性地露出流动扰动特征。
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公开(公告)号：US20160102579A1
公开(公告)日：2016-04-14
申请号：US14511987
申请日：2014-10-10
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Leon Hu , David R. Hanna
IPC: F01D25/26
CPC classification number: F01D25/26 , F05D2220/40 , F05D2250/283 , F05D2250/61 , F05D2260/231
Abstract: Systems are provided for a reinforcement element coupled to a sheet metal turbine housing that imparts desirable thermal-protective and structurally strengthening characteristics to the housing layers. In one example, a system may include a turbine comprising a housing surrounding a turbine rotor, the housing having an outer layer surrounding an inner layer at a distance to form an intermediate space between the inner and outer layers. Moreover, disposed in the intermediate space is a reinforcement element coupled to the inner and outer layers, providing strength and consistent rigidity without a significant increase in weight to the housing.
Abstract translation: 系统被设置用于联接到金属板式涡轮机壳体的增强元件，其对外壳层施加期望的热保护和结构强化特性。 在一个示例中，系统可以包括涡轮机，其包括围绕涡轮机转子的壳体，壳体具有围绕内层一定距离的外层，以在内层和外层之间形成中间空间。 此外，设置在中间空间中的是与内层和外层联接的增强元件，提供强度和一致的刚度，而不会显着地增加与壳体的重量。
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Patent Agency Ranking
公开(公告)号：US10519799B2
公开(公告)日：2019-12-31
申请号：US15828681
申请日：2017-12-01
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Ben Zhao , Leon Hu , Jianwen James Yi , Eric Warren Curtis , Jizhong Zhang
IPC: F01D17/16
Abstract: Various systems and methods are described for a variable geometry turbine. In one example, a nozzle vane includes a stationary having a first cambered sliding surface and a sliding vane having a second cambered sliding surface where the second cambered sliding surface includes a flow disrupting feature in contact with the first sliding cambered surface. The sliding vane may be positioned to slide in a direction from substantially tangent along a curved path to an inner circumference of the turbine nozzle and selectively uncover the flow disrupting feature.
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公开(公告)号：US20140060009A1
公开(公告)日：2014-03-06
申请号：US13867734
申请日：2013-04-22
Applicant: FORD GLOBAL TECHNOLOGIES, LLC
Inventor： Xiaogang Zhang , Jianwen James Yi , Wen Dai , Paul M. Laing , John Hedges , Julia Helen Buckland , Harold Huimin Sun
IPC: F01N3/18
CPC classification number: F01N3/18 , F01N3/22 , F01N3/30 , F01N13/009 , F02B37/168 , F02B37/18 , Y02A50/2322 , Y02T10/144 , Y02T10/20
Abstract: A vehicle system operation method is provided. The method comprises, during a first operating condition, increasing back pressure in a first exhaust conduit positioned upstream of a turbine and downstream of a first emission control device and during a second operating condition, reducing back pressure in the first exhaust conduit and flowing boosted air from downstream of a compressor into a second exhaust conduit positioned upstream of a second emission control device and downstream of the turbine.
Abstract translation: 提供车辆系统操作方法。 该方法包括在第一操作条件期间在位于涡轮机上游并位于第一排放控制装置下游的第一排气管道中增加背压，并且在第二操作条件期间，减小第一排气管道中的背压并使增压空气流动 从压缩机的下游到位于第二排放控制装置上游并位于涡轮下游的第二排气导管。
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公开(公告)号：US20180087453A1
公开(公告)日：2018-03-29
申请号：US15828681
申请日：2017-12-01
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Ben Zhao , Leon Hu , Jianwen James Yi , Eric Warren Curtis , Jizhong Zhang
Abstract: Various systems and methods are described for a variable geometry turbine. In one example, a nozzle vane includes a stationary having a first cambered sliding surface and a sliding vane having a second cambered sliding surface where the second cambered sliding surface includes a flow disrupting feature in contact with the first sliding cambered surface. The sliding vane may be positioned to slide in a direction from substantially tangent along a curved path to an inner circumference of the turbine nozzle and selectively uncover the flow disrupting feature.
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公开(公告)号：US09890700B2
公开(公告)日：2018-02-13
申请号：US14709339
申请日：2015-05-11
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Ben Zhao , Leon Hu , Jianwen James Yi , Eric Warren Curtis , Jizhong Zhang
CPC classification number: F02B37/24 , F01D5/141 , F01D17/165 , F02B39/00 , F05D2210/30 , F05D2220/40 , F05D2240/12 , Y02T10/144
Abstract: Various systems and methods are described for a variable geometry turbine. In one example, a nozzle vane includes a stationary having a first cambered sliding surface and a sliding vane having a second cambered sliding surface where the second cambered sliding surface includes a flow disrupting feature in contact with the first sliding cambered surface. The sliding vane may be positioned to slide in a direction from substantially tangent along a curved path to an inner circumference of the turbine nozzle and selectively uncover the flow disrupting feature.
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公开(公告)号：US09267427B2
公开(公告)日：2016-02-23
申请号：US13915452
申请日：2013-06-11
Applicant: Ford Global Technologies, LLC
Inventor： Harold Huimin Sun , Liangjun Hu , Ben Zhao , Dave R. Hanna
CPC classification number: F02B37/22 , F01D17/165 , F02B37/24 , F05D2220/40
Abstract: Embodiments may provide variable geometry turbine, a nozzle vane for a variable geometry turbine, and a method. The variable geometry turbine that may include a turbine wheel and a plurality of adjustable vanes radially positioned around the turbine wheel. The turbine may also include a flow disrupting feature on one or more outside surfaces of one or more of the plurality of adjustable vanes.
Abstract translation: 实施例可以提供可变几何涡轮机，用于可变几何涡轮机的喷嘴叶片和方法。 可变几何涡轮机，其可以包括涡轮机叶轮和围绕涡轮机叶片径向定位的多个可调叶片。 涡轮机还可以包括在多个可调叶片中的一个或多个的一个或多个外表面上的流动破坏特征。
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