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    • 13. 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。
    • 14. 发明申请
    • Optimized locomotive traction system
    • US20060022622A1
    • 2006-02-02
    • US11156399
    • 2005-06-20
    • Mark NicolussiPaul HokansonAjith Kumar
    • Mark NicolussiPaul HokansonAjith Kumar
    • H02P5/00
    • 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.