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    • 1. 发明授权
    • Optimized locomotive traction system
    • 优化机车牵引系统
    • US07045981B2
    • 2006-05-16
    • US11156399
    • 2005-06-20
    • Mark Louis NicolussiPaul Robert HokansonAjith Kuttannair Kumar
    • Mark Louis NicolussiPaul Robert HokansonAjith Kuttannair Kumar
    • B61C3/00
    • B60L3/00B60L11/10B60L2200/26Y02T10/646Y02T10/70
    • A high-altitude railroad locomotive adapted for more reliable operation at high altitudes, wherein the high-altitude railroad locomotive includes a semiconductor electric power control component, and wherein due to the high altitude the locomotive would be exposed to high levels of cosmic radiation tending to damage the semiconductor electric power control component is provided. The high-altitude locomotive includes electric power generation equipment, a plurality of traction motors mechanically connected to wheels supporting the high altitude locomotive and an electric power transmission system for transmitting electrical power from the electric power generation equipment to the plurality of traction motors. A DC bus is also included and electrically connected to the traction motors and a power controller for controlling the transmission of power over the DC bus, the traction motors having a second active motor volume, wherein the second active motor volume is larger than the first active motor volume to enable the DC bus voltage of the high-altitude locomotive to be reduced relative to the first DC bus voltage while generating a range of mechanical power sufficient to propel the locomotive at high altitudes, whereby the combined effects on the semiconductor electric power control component caused by the DC bus voltage of the high-altitude locomotive and by the cosmic radiation correspond to these effects on the semiconductor electric power control components of the low-altitude locomotive when operating at low altitudes to reduce the likelihood of failure of the semiconductor electric power control component of the high-altitude locomotive.
    • 一种高空铁路机车,适用于高空作业的可靠运行,其中高空铁路机车包括半导体电力控制部件,其中由于高空,机车将暴露于高水平的宇宙辐射,趋向于 提供了半导体电力控制部件的损坏。 高空机车包括发电设备,机械地连接到支撑高空机车的车轮的多个牵引电动机和用于将电力从发电设备发送到多个牵引电动机的电力传输系统。 还包括DC总线并电连接到牵引电动机和用于控制通过DC总线的电力传输的功率控制器,所述牵引电动机具有第二主动电动机容积,其中所述第二主动电动机容积大于所述第一有效电动机容积 使得能够相对于第一DC总线电压降低高空机车的直流母线电压,同时产生足以在高海拔地推进机车的机械动力范围,由此对半导体电力控制的组合效应 由高空机车的直流母线电压和宇宙辐射引起的分量对应于低空机车半导体电力控制部件在低空操作时的影响,以减少半导体电气故障的可能性 高空机车的功率控制部件。
    • 8. 发明授权
    • Methods and systems for throttle control and coupling control for vehicles
    • 车辆节气门控制和联动控制的方法和系统
    • US09026284B2
    • 2015-05-05
    • US13570340
    • 2012-08-09
    • Ajith Kuttannair KumarBret D. Worden
    • Ajith Kuttannair KumarBret D. Worden
    • G05D1/00G05D3/00G06F7/00G06F17/00B61L3/00B61L17/00B61D17/12
    • B61L3/006B61D17/12B61L17/00Y02T30/30
    • A multi-mode control system for a locomotive includes a throttle control device having notch settings corresponding to, for a first, long haul mode, control signals for providing respective tractive effort or power from the locomotive, a master controller in communication with the throttle control device and adapted to receive said control signals from the throttle control device and to transmit respective command signals to power-train components of the locomotive to achieve the respective tractive effort or power, the master controller also adapted for sending alternative command signals when a user-operable mode selector is set to one of one or more alternative modes. The user-operable mode selector includes one or more user interface devices in communication with the master controller for selecting one alternative mode of the one or more alternative modes.
    • 一种用于机车的多模式控制系统包括节流控制装置,其具有对应于第一长距离模式的切口设置,用于提供来自机车的相应牵引力或功率的控制信号,与节气门控制器通信的主控制器 并且适于从所述节气门控制装置接收所述控制信号,并且将相应的命令信号发送到所述机车的功率列车部件以实现相应的牵引力或功率,所述主控制器还适于在用户 - 可操作模式选择器被设置为一种或多种替代模式中的一种。 用户可操作模式选择器包括与主控制器通信的一个或多个用户界面设备,用于选择一个或多个替代模式的一个备选模式。