METHOD AND SYSTEM FOR VARIABLY ADJUSTING VOLTAGE OF LDC FOR HYBRID VEHICLE
    2.
    发明申请
    METHOD AND SYSTEM FOR VARIABLY ADJUSTING VOLTAGE OF LDC FOR HYBRID VEHICLE 有权
    用于混合车辆的LDC的电压调节方法和系统

    公开(公告)号:US20160121725A1

    公开(公告)日:2016-05-05

    申请号:US14860956

    申请日:2015-09-22

    Abstract: A method and system are provided for variably adjusted voltage of the LDC applied with an IBS (Intelligent Battery Sensor). The LDC output voltage control mode is determined in each of three driving modes, and the high electric loads are separated into two or more groups. The LDC output voltage value and the order priority are differentiated based on the durability of the auxiliary battery. Additionally, an LDC output voltage order table is generated according to the driving mode and the SOC state based on the auxiliary battery SOC information obtained from an IBS. Thus, consumed energy of the LDC and an energy consumption amount of the auxiliary battery are minimized, thus improving fuel efficiency.

    Abstract translation: 提供了一种用于可变调节的施加IBS(智能电池传感器)的LDC电压的方法和系统。 在三种驱动模式中确定LDC输出电压控制模式,并且将高电负载分成两组或更多组。 基于辅助电池的耐久性,LDC输出电压值和顺序优先级不同。 此外,根据从IBS获得的辅助电池SOC信息,根据驱动模式和SOC状态生成LDC输出电压顺序表。 因此,LDC的消耗能量和辅助电池的能量消耗量被最小化,从而提高燃料效率。

    CONVERTER CIRCUIT AND METHOD FOR TRANSFERRING ELECTRICAL ENERGY
    4.
    发明申请
    CONVERTER CIRCUIT AND METHOD FOR TRANSFERRING ELECTRICAL ENERGY 审中-公开
    转换电路和转换电能的方法

    公开(公告)号:US20140225432A1

    公开(公告)日:2014-08-14

    申请号:US14241124

    申请日:2012-06-20

    Applicant: Hans Geyer

    Inventor: Hans Geyer

    Abstract: The invention relates to a converter circuit (50) for transferring electrical energy, in particular for application in a motor vehicle wiring system (38, 42), which converter circuit comprises an electromagnetic transfer unit (60) having three electromagnetic transfer members (62, 64, 66) that can be electromagnetically coupled to each other in order to transfer electromagnetic energy, wherein the first electromagnetic transfer member (62) is connected to a first bi-directional converter circuit that comprises a first voltage connection pole pair (80) for connecting an AC voltage source and/or sink (54), wherein the second electromagnetic transfer member (64) is connected to a rectifier converter circuit that is connected on the outlet side to an electrical energy store (88), and wherein the third electromagnetic transfer member (66) is connected to a second bi-directional converter circuit that comprises a second voltage pole pair (96) for connecting a DC voltage source and/or sink (98), and a control unit (100) that is connected to the first bi-directional converter circuit, the second bi-directional converter circuit and the rectifier converter circuit, in order to control the exchange of electrical energy between the AC voltage source and/or sink (54), the DC voltage source and/or sink (98) and/or the electrical energy store (88).

    Abstract translation: 本发明涉及一种用于转移电能的转换器电路,特别是用于机动车辆配线系统(38,42)中的转换器电路,该转换器电路包括具有三个电磁转移构件(62,62)的电磁转移单元(60) 64,66),其可以彼此电磁耦合以传递电磁能,其中所述第一电磁转移构件(62)连接到第一双向转换器电路,所述第一双向转换器电路包括第一电压连接极对(80),用于 连接AC电压源和/或接收器(54),其中所述第二电磁转移构件(64)连接到在出口侧连接到电能存储器(88)的整流器转换器电路,并且其中所述第三电磁 传输构件(66)连接到第二双向转换器电路,所述第二双向转换器电路包括用于连接DC电压源和/或接收器(9)的第二电压极对(96) 8)以及连接到第一双向转换器电路,第二双向转换器电路和整流器转换器电路的控制单元(100),以便控制交流电压源和 /或吸收器(54),直流电压源和/或吸收器(98)和/或电能存储器(88)。

    Electric drive-train for ships
    5.
    发明授权

    公开(公告)号:US09764727B1

    公开(公告)日:2017-09-19

    申请号:US13234583

    申请日:2011-09-16

    Abstract: An electric drive-train for a ship includes a first generator having a rotatable shaft structured to be driven by a first prime mover and an output providing a voltage; a second generator having a rotatable shaft structured to be driven by a second prime mover and an output providing a voltage; an electric machine including a rotatable shaft structured to drive a propeller; a first power electronic converter electrically interconnected with the output of the first generator and structured to power the electric machine; and a second power electronic converter electrically interconnected with the output of the second generator and structured to power the electric machine. A support structure replaces a reduction gear box and supports the first generator, the second generator, the electric machine, the first power electronic converter, and the second power electronic converter.

    Brake Resistor Control
    7.
    发明申请
    Brake Resistor Control 有权
    制动电阻控制

    公开(公告)号:US20110260661A1

    公开(公告)日:2011-10-27

    申请号:US12767191

    申请日:2010-04-26

    Applicant: Zimin W. Vilar

    Inventor: Zimin W. Vilar

    Abstract: An electric drive system comprises a generator, a traction motor, a brake resistor, a bus, and a control unit. The generator, the traction motor, and the brake resistor are coupled electrically to the bus. The control unit is configured to determine a pulse-width-modulation duty cycle for the brake resistor (“brake duty”) and control operation of the brake resistor according to the brake duty, wherein the brake duty can be a value intermediate of constant OFF and constant ON. A method of operating the electric drive system is also disclosed.

    Abstract translation: 电驱动系统包括发电机,牵引电动机,制动电阻器,总线和控制单元。 发电机,牵引电动机和制动电阻器与总线电连接。 控制单元被配置为根据制动负载确定制动电阻器的脉宽调制占空比(“制动负载”)和制动电阻器的控制操作,其中制动负载可以是常数OFF的值 并保持ON。 还公开了一种操作电驱动系统的方法。

    Optimized locomotive traction system
    9.
    发明授权
    Optimized locomotive traction system 失效
    优化机车牵引系统

    公开(公告)号:US07045981B2

    公开(公告)日:2006-05-16

    申请号:US11156399

    申请日:2005-06-20

    CPC classification number: B60L3/00 B60L11/10 B60L2200/26 Y02T10/646 Y02T10/70

    Abstract: 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.

    Abstract translation: 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。

    Optimized locomotive traction system

    公开(公告)号:US20060022622A1

    公开(公告)日:2006-02-02

    申请号:US11156399

    申请日:2005-06-20

    CPC classification number: B60L3/00 B60L11/10 B60L2200/26 Y02T10/646 Y02T10/70

    Abstract: 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.

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