Camshaft assembly
    1.
    发明授权
    Camshaft assembly 有权
    凸轮轴总成

    公开(公告)号:US09032922B2

    公开(公告)日:2015-05-19

    申请号:US14058639

    申请日:2013-10-21

    CPC classification number: F01L1/34 F01L13/0036 F01L2013/0052

    Abstract: A camshaft assembly can control the motion of the intake or exhaust valves of an internal combustion engine and includes a base shaft extending along a longitudinal axis. The camshaft assembly further includes an axially movable structure mounted on the base shaft and axially movable relative to the base shaft. The axially movable structure includes a plurality of lobe packs. Each lobe pack includes a plurality of cam lobes. The axially movable structure includes a barrel cam defining a control groove. The camshaft assembly additionally includes an actuator including an actuator body and a pin movably coupled to the actuator body between a retracted position and an extended position. The axially movable structure can move axially relative to the base shaft when the base shaft rotates about the longitudinal axis and the pin is in the extended position and at least partially disposed in the control groove.

    Abstract translation: 凸轮轴组件可以控制内燃机的进气门或排气门的运动,并且包括沿着纵向轴线延伸的基轴。 凸轮轴组件还包括可轴向移动的结构,其安装在基座轴上并相对于基轴可轴向移动。 可轴向移动的结构包括多个叶片组。 每个凸角组件包括多个凸轮凸角。 轴向可移动结构包括限定控制槽的筒形凸轮。 凸轮轴组件另外包括致动器,该致动器包括致动器主体和在缩回位置和延伸位置之间可动地联接到致动器本体的销。 当基轴围绕纵向轴线旋转并且销处于伸出位置并且至少部分地设置在控制槽中时,可轴向移动的结构可相对于基部轴线轴向移动。

    Turbocharger compressor temperature control systems and methods
    2.
    发明授权
    Turbocharger compressor temperature control systems and methods 有权
    涡轮增压器压缩机温度控制系统及方法

    公开(公告)号:US09309803B2

    公开(公告)日:2016-04-12

    申请号:US14097665

    申请日:2013-12-05

    Abstract: A control system for a vehicle includes a target boost module and a turbocharger control module. The target boost module determines a target boost for first and second turbochargers based on an engine torque request. Based on a temperature of a compressor of the second turbocharger, the turbocharger control module: selectively opens a first bypass valve that regulates exhaust bypassing a first turbine of the first turbocharger; and selectively closes a cutoff valve that regulates exhaust flow through both a second turbine of the second turbocharger and a second bypass valve. The second bypass valve regulates exhaust bypassing the second turbine of the second turbocharger.

    Abstract translation: 车辆的控制系统包括目标升压模块和涡轮增压器控制模块。 目标升压模块基于发动机转矩请求确定第一和第二涡轮增压器的目标升压。 基于第二涡轮增压器的压缩机的温度,涡轮增压器控制模块:选择性地打开第一旁通阀,其调节绕过第一涡轮增压器的第一涡轮机的排气; 并且选择性地关闭调节通过第二涡轮增压器的第二涡轮机和第二旁通阀的排气流量的截止阀。 第二旁路阀调节绕过第二涡轮增压器的第二涡轮机的排气。

    Turbine housing
    3.
    发明授权
    Turbine housing 有权
    涡轮房

    公开(公告)号:US09068474B2

    公开(公告)日:2015-06-30

    申请号:US13750291

    申请日:2013-01-25

    Inventor: Joel Cowgill

    Abstract: A turbine housing comprises an exhaust port flange, a turbine discharge flange, a crossover flange, and a bearing support ring. The exhaust port flange is configured for mechanically coupling the turbine housing to a mating structure providing a source of working fluid. The turbine discharge flange is configured for mechanically coupling the turbine housing to an exhaust system. The crossover flange is configured for mechanically coupling the turbine housing to a crossover duct. The bearing support ring is configured for mechanically supporting a bearing, on which a turbine output shaft is supported. The turbine housing defines an inlet plenum, a turbine shroud, and a discharge vent. The exhaust port flange defines an inlet port configured to provide fluid communication between the inlet plenum and the source of working fluid. The turbine shroud defines a fluid expansion flow path for expansion of the stream of working fluid.

    Abstract translation: 涡轮壳体包括排气口凸缘,涡轮排出凸缘,交叉凸缘和轴承支撑环。 排气口法兰被构造成将涡轮机壳体机械地联接到提供工作流体源的配合结构。 涡轮排出法兰被构造成将涡轮机壳体机械地联接到排气系统。 交叉法兰被配置为将涡轮机壳体机械地联接到交叉管道。 轴承支撑环被构造成用于机械地支撑支撑涡轮机输出轴的轴承。 涡轮壳体限定入口气室,涡轮罩和排气口。 排气口法兰限定入口端口,该入口端口被配置为提供入口通风室和工作流体源之间的流体连通。 涡轮机罩限定了用于膨胀工作流体流的流体膨胀流动路径。

    TURBO SPEED CONTROL FOR MODE TRANSITIONS IN A DUAL TURBO SYSTEM
    4.
    发明申请
    TURBO SPEED CONTROL FOR MODE TRANSITIONS IN A DUAL TURBO SYSTEM 有权
    用于双涡轮系统中模式转换的涡轮速度控制

    公开(公告)号:US20150159544A1

    公开(公告)日:2015-06-11

    申请号:US14097587

    申请日:2013-12-05

    Abstract: A system for controlling an engine having a first turbocharger, a second turbocharger and a cutoff valve that regulates exhaust flow through a turbine of the second turbocharger, the system comprising: a speed determination module that determines a current speed of the first turbocharger, determines a current speed of the second turbocharger, and determines a target speed of the second turbocharger based on the current speed of the first turbocharger; and a boost control module that compares the target speed of the second turbocharger with the current speed of the second turbocharger, and that selectively adjusts a position of a cutoff valve to adjust the current speed of the second turbocharger based on the comparison.

    Abstract translation: 一种用于控制发动机的系统,所述发动机具有调节通过所述第二涡轮增压器的涡轮机的排气流的第一涡轮增压器,第二涡轮增压器和截止阀,所述系统包括:速度确定模块,其确定所述第一涡轮增压器的当前速度, 第二涡轮增压器的当前速度,并且基于第一涡轮增压器的当前速度确定第二涡轮增压器的目标速度; 以及升压控制模块,其将第二涡轮增压器的目标速度与第二涡轮增压器的当前速度进行比较,并且基于该比较选择性地调节截止阀的位置以调节第二涡轮增压器的当前速度。

    CAMSHAFT ASSEMBLY
    6.
    发明申请
    CAMSHAFT ASSEMBLY 有权
    CAMSHAFT大会

    公开(公告)号:US20150107540A1

    公开(公告)日:2015-04-23

    申请号:US14058639

    申请日:2013-10-21

    CPC classification number: F01L1/34 F01L13/0036 F01L2013/0052

    Abstract: A camshaft assembly can control the motion of the intake or exhaust valves of an internal combustion engine and includes a base shaft extending along a longitudinal axis. The camshaft assembly further includes an axially movable structure mounted on the base shaft and axially movable relative to the base shaft. The axially movable structure includes a plurality of lobe packs. Each lobe pack includes a plurality of cam lobes. The axially movable structure includes a barrel cam defining a control groove. The camshaft assembly additionally includes an actuator including an actuator body and a pin movably coupled to the actuator body between a retracted position and an extended position. The axially movable structure can move axially relative to the base shaft when the base shaft rotates about the longitudinal axis and the pin is in the extended position and at least partially disposed in the control groove.

    Abstract translation: 凸轮轴组件可以控制内燃机的进气门或排气门的运动,并且包括沿着纵向轴线延伸的基轴。 凸轮轴组件还包括可轴向移动的结构,其安装在基座轴上并相对于基轴可轴向移动。 可轴向移动的结构包括多个叶片组。 每个凸角组件包括多个凸轮凸角。 轴向可移动结构包括限定控制槽的筒形凸轮。 凸轮轴组件另外包括致动器,该致动器包括致动器主体和在缩回位置和延伸位置之间可动地联接到致动器本体的销。 当基轴围绕纵向轴线旋转并且销处于伸出位置并且至少部分地设置在控制槽中时,可轴向移动的结构可相对于基部轴线轴向移动。

    TURBINE HOUSING
    7.
    发明申请
    TURBINE HOUSING 有权
    涡轮外壳

    公开(公告)号:US20140212278A1

    公开(公告)日:2014-07-31

    申请号:US13750291

    申请日:2013-01-25

    Inventor: Joel Cowgill

    Abstract: A turbine housing comprises an exhaust port flange, a turbine discharge flange, a crossover flange, and a bearing support ring. The exhaust port flange is configured for mechanically coupling the turbine housing to a mating structure providing a source of working fluid. The turbine discharge flange is configured for mechanically coupling the turbine housing to an exhaust system. The crossover flange is configured for mechanically coupling the turbine housing to a crossover duct. The bearing support ring is configured for mechanically supporting a bearing, on which a turbine output shaft is supported. The turbine housing defines an inlet plenum, a turbine shroud, and a discharge vent. The exhaust port flange defines an inlet port configured to provide fluid communication between the inlet plenum and the source of working fluid. The turbine shroud defines a fluid expansion flow path for expansion of the stream of working fluid.

    Abstract translation: 涡轮壳体包括排气口凸缘,涡轮排出凸缘,交叉凸缘和轴承支撑环。 排气口法兰被构造成将涡轮机壳体机械地联接到提供工作流体源的配合结构。 涡轮排出法兰被构造成将涡轮机壳体机械地联接到排气系统。 交叉法兰被配置为将涡轮机壳体机械地联接到交叉管道。 轴承支撑环被构造成用于机械地支撑支撑涡轮机输出轴的轴承。 涡轮壳体限定入口气室,涡轮罩和排气口。 排气口法兰限定入口端口,该入口端口被配置为提供入口通风室和工作流体源之间的流体连通。 涡轮机罩限定了用于膨胀工作流体流的流体膨胀流动路径。

    Turbo speed control for mode transitions in a dual turbo system
    8.
    发明授权
    Turbo speed control for mode transitions in a dual turbo system 有权
    用于双涡轮增压系统中模式转换的Turbo速度控制

    公开(公告)号:US09303553B2

    公开(公告)日:2016-04-05

    申请号:US14097587

    申请日:2013-12-05

    Abstract: A system for controlling an engine having a first turbocharger, a second turbocharger and a cutoff valve that regulates exhaust flow through a turbine of the second turbocharger, the system comprising: a speed determination module that determines a current speed of the first turbocharger, determines a current speed of the second turbocharger, and determines a target speed of the second turbocharger based on the current speed of the first turbocharger; and a boost control module that compares the target speed of the second turbocharger with the current speed of the second turbocharger, and that selectively adjusts a position of a cutoff valve to adjust the current speed of the second turbocharger based on the comparison.

    Abstract translation: 一种用于控制发动机的系统,所述发动机具有调节通过所述第二涡轮增压器的涡轮机的排气流的第一涡轮增压器,第二涡轮增压器和截止阀,所述系统包括:速度确定模块,其确定所述第一涡轮增压器的当前速度, 第二涡轮增压器的当前速度,并且基于第一涡轮增压器的当前速度确定第二涡轮增压器的目标速度; 以及升压控制模块,其将第二涡轮增压器的目标速度与第二涡轮增压器的当前速度进行比较,并且基于该比较选择性地调节截止阀的位置以调节第二涡轮增压器的当前速度。

    PHASER CONTROL SYSTEMS AND METHODS FOR BALANCING MEAN EFFECTIVE PRESSURE
    9.
    发明申请
    PHASER CONTROL SYSTEMS AND METHODS FOR BALANCING MEAN EFFECTIVE PRESSURE 有权
    相位控制系统和平衡有效压力平衡方法

    公开(公告)号:US20140278009A1

    公开(公告)日:2014-09-18

    申请号:US13833269

    申请日:2013-03-15

    Abstract: An engine control system includes a mean effective pressure (MEP) module, an imbalance module, and a phaser control module. The MEP module determines MEPs for combustion cycles of cylinders, respectively, of an engine. The imbalance module selectively determines whether first and second banks of the cylinders are imbalanced based on the MEPs. When the first and second banks of cylinders are imbalanced, the phaser control module selectively adjusts at least one of: a first phaser of an intake camshaft of the second bank of cylinders; and a second phaser of an exhaust camshaft of the second bank of cylinders.

    Abstract translation: 发动机控制系统包括平均有效压力(MEP)模块,不平衡模块和相位器控制模块。 MEP模块分别确定发动机气缸的燃烧循环的MEP。 不平衡模块基于MEP选择性地确定气瓶的第一和第二组是不平衡的。 当第一和第二气缸组不平衡时,相位器控制模块选择性地调节以下中的至少一个:第二气缸组的进气凸轮轴的第一相位器; 以及第二气缸组的排气凸轮轴的第二相位器。

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