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    • 2. 发明授权
    • Compressor impeller with stress riser
    • 压缩机叶轮与应力提升
    • US07001155B2
    • 2006-02-21
    • US10439075
    • 2003-05-14
    • Jose CabralesGerald Duane LaRueJohn M. WilsonAngus Lemon
    • Jose CabralesGerald Duane LaRueJohn M. WilsonAngus Lemon
    • F04B35/00
    • F01D21/045F01D5/025F01D5/048F04D25/04F04D29/266F05D2250/281F05D2260/941
    • A compressor impeller for use with a boreless turbocharger is provided in accordance with this invention. The compressor impeller comprises an integral hub projecting axially therefrom that includes a partial bore therein that extends from an open to a close bore end. The bore includes a threaded portion that is configured to accommodate threaded engagement with an end of a common shaft disposed through a turbocharger housing and attached at an opposite end to a turbine wheel. The hub is specially configured so that the threaded portion has a relatively increased wall thickness when compared to a remaining portion of the bore disposed between the threaded portion and the end of the bore. The bore is configured providing a section having a reduced wall thickness, between the threaded portion and the bore closed end, for purposes of providing a preferential stress relief mechanism. Configured in this manner, the compressor impeller operates to ensure that, in the event of a stress-related compressor impeller failure, the shaft will be contained in its proper placement within the turbocharger.
    • 根据本发明提供了一种与无孔涡轮增压器一起使用的压缩机叶轮。 压缩机叶轮包括从其轴向突出的整体式轮毂,其包括其中从一开放到一孔径端延伸的部分孔。 所述孔包括螺纹部分,所述螺纹部分被配置为容纳与通过涡轮增压器壳体设置的公共轴的端部的螺纹接合,并且在相对端附接到涡轮机叶轮。 轮毂是特别构造的,使得与设置在螺纹部分和孔的端部之间的孔的剩余部分相比,螺纹部分具有相对增加的壁厚。 为了提供优先的应力消除机构,孔被配置成在螺纹部分和孔封闭端之间提供具有减小的壁厚的部分。 以这种方式配置,压缩机叶轮操作以确保在压力相关的压缩机叶轮故障的情况下,轴将被包含在其在涡轮增压器内的适当位置。
    • 4. 发明授权
    • Turbocharger fatigue life monitor
    • 涡轮增压器疲劳寿命监测仪
    • US06209390B1
    • 2001-04-03
    • US09312380
    • 1999-05-14
    • Gerald Duane LaRueDonald Ervin Baker
    • Gerald Duane LaRueDonald Ervin Baker
    • G01M1500
    • G07C3/00
    • Turbocharger fatigue life monitors comprise at least one sensor that measures an actual operating condition of the turbocharger, e.g., turbine rotational speed or turbine inlet temperature. The device comprises a central processing unit for receiving information from each sensor and processing the information, using programs and predetermined turbocharger information, e.g., turbocharger material and stress data stored in one or more storage device in communication with the central processing unit, to provide an actual probability of turbocharger failure. The central processing unit compares the calculated probability of turbocharger failure to a predetermined specified probability of turbocharger failure stored in a storage device to determine whether turbocharger service is needed. The central processing unit provides a signal that operates an annunciator to indicate recommended or necessary turbocharger service when the actual probability of turbocharger failure exceeds the specified probability of turbocharger failure. The central processing unit and storage devices can be packaged independent of or as part of an existing turbocharged application system, e.g., an engine control module when the turbocharged application is a vehicle.
    • 涡轮增压器疲劳寿命监测器包括至少一个测量涡轮增压器的实际操作状态的传感器,例如涡轮机转速或涡轮机入口温度。 该装置包括中央处理单元,用于从每个传感器接收信息并使用程序和预定的涡轮增压器信息(例如,存储在与中央处理单元通信的一个或多个存储设备中的涡轮增压器材料和压力数据)来处理信息,以提供 涡轮增压器故障的实际概率。 中央处理单元将计算出的涡轮增压器故障概率与存储在存储装置中的预定的涡轮增压器故障概率进行比较,以确定是否需要涡轮增压器服务。 当涡轮增压器故障的实际概率超过涡轮增压器故障的指定概率时,中央处理单元提供操作报警器以指示推荐或必要的涡轮增压器服务的信号。 当涡轮增压应用是车辆时,中央处理单元和存储装置可以与现有的涡轮增压应用系统(例如,发动机控制模块)独立地或作为其一部分进行包装。