Methods and systems for surge control
    21.
    发明授权
    Methods and systems for surge control 有权
    浪涌控制的方法和系统

    公开(公告)号:US09551276B2

    公开(公告)日:2017-01-24

    申请号:US14460304

    申请日:2014-08-14

    Abstract: Systems and methods are provided for reducing surge in a boosted engine system. One method comprises adjusting an opening of a compressor recirculation valve to allow a compressor recirculation flow based on a combination of a nominal compressor recirculation flow and a filtered nominal compressor recirculation flow. The nominal compressor recirculation flow may be calculated as a difference between a desired compressor flow rate based on a surge limit of compressor and an estimated throttle mass flow rate.

    Abstract translation: 提供的系统和方法用于减少升压发动机系统的浪涌。 一种方法包括调整压缩机再循环阀的开口,以允许基于标称压缩机再循环流和经过滤的标称压缩机再循环流的组合的压缩机再循环流。 标称压缩机再循环流量可以计算为基于压缩机浪涌极限的所需压缩机流量与估计的节气门质量流量之间的差值。

    Vehicle Having Engine Control system With Power Boost In Response To Torque Demand
    25.
    发明申请
    Vehicle Having Engine Control system With Power Boost In Response To Torque Demand 审中-公开
    具有发动机控制系统的车辆具有响应于扭矩需求的动力提升

    公开(公告)号:US20160305313A1

    公开(公告)日:2016-10-20

    申请号:US14686110

    申请日:2015-04-14

    Abstract: An engine system configured to adjust an output torque generated by the engine system in response to anticipated changes in a condition of a load. The engine system includes a load predictor, an air supply system, a fuel supply system, and an electronic control unit. The electronic control unit is configured to adjust the quantity of air and/or exhaust provided to an inlet manifold of an engine and to thereafter adjust the quantity of fuel delivered to the engine for a predetermined period of time. The delivery of the quantity of fuel is delayed from the adjustment to the quantity of air and/or exhaust to provide a torque boost responsive to the anticipated changes in the condition of the load. Fuel costs are reduced and the engine operates more smoothly in response to load changes.

    Abstract translation: 发动机系统,其构造成响应于负载状况中的预期变化来调节由发动机系统产生的输出转矩。 发动机系统包括负载预测器,供气系统,燃料供应系统和电子控制单元。 电子控制单元被配置为调节提供给发动机的入口歧管的空气和/或排气量,此后调节输送到发动机的燃料量达预定时间段。 燃料量的输送从调节延迟到空气和/或排气量,以响应于负载条件的预期变化提供转矩提升。 燃料成本降低,发动机响应负载变化更平稳运行。

    Turbocharger and Method
    26.
    发明申请
    Turbocharger and Method 有权
    涡轮增压器和方法

    公开(公告)号:US20160281645A1

    公开(公告)日:2016-09-29

    申请号:US14641665

    申请日:2015-03-09

    Abstract: A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes first and second bearings formed between an outer bearing race element disposed within the bearing bore an inner bearing race element disposed within the outer bearing race element and between the outer bearing race element and the shaft. The inner bearing race element rotates with the shaft and forms an extension segment having an open channel that, together with an annular surface on an inner side of a back of the compressor wheel, forms a U-shaped channel into which a ring seal is disposed. The ring seal sealably engages the inner bearing race element and also slidably and sealably engages the inner bore of the bearing retainer.

    Abstract translation: 涡轮增压器包括涡轮机,压缩机和形成轴承孔的轴承壳体。 轴承装置设置在连接涡轮和压缩机叶轮之间的轴与轴承壳体之间。 轴承装置包括形成在设置在轴承孔内的外轴承座圈元件之间的第一和第二轴承,设置在外轴承座圈内的内轴承座圈元件和外轴承座圈元件与轴之间。 内部轴承座圈与轴一起旋转并形成具有开放通道的延伸段,该通道与压缩机叶轮后部的内侧上的环形表面一起形成U形通道,环形密封件设置在该U形通道中 。 环形密封件可密封地接合内部轴承座圈元件,并且还可滑动地且可密封地接合轴承保持器的内孔。

    EVACUATOR WITH MOTIVE FIN
    29.
    发明申请
    EVACUATOR WITH MOTIVE FIN 审中-公开
    EVACUATOR WITH MOTION FIN

    公开(公告)号:US20160245236A1

    公开(公告)日:2016-08-25

    申请号:US14631287

    申请日:2015-02-25

    Abstract: An evacuator is disclosed, and includes a body defining a central axis, a converging motive section, a diverging discharge section, at least one suction port, and at least one Venturi gap. The Venturi gap is located between an outlet end of the converging motive section and an inlet end of the diverging discharge section. The evacuator also includes a fin positioned within the motive section of the body. The fin extends in the direction of the central axis.

    Abstract translation: 抽真空器被公开,并且包括限定中心轴线的主体,会聚动力部分,发散排放部分,至少一个吸入口和至少一个文氏管间隙。 文丘里间隙位于会聚动力部分的出口端和发散排放部分的入口端之间。 排气管还包括位于主体的动力部分内的翅片。 翅片沿着中心轴线的方向延伸。

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