VEHICLE PROPULSION SYSTEM HAVING AN ENERGY STORAGE SYSTEM AND OPTIMIZED METHOD OF CONTROLLING OPERATION THEREOF
    26.
    发明申请
    VEHICLE PROPULSION SYSTEM HAVING AN ENERGY STORAGE SYSTEM AND OPTIMIZED METHOD OF CONTROLLING OPERATION THEREOF 有权
    具有能源储存系统的车辆推进系统和控制其运行的优化方法

    公开(公告)号:US20160052410A1

    公开(公告)日:2016-02-25

    申请号:US14480002

    申请日:2014-09-08

    Inventor: Zhi Zhou

    Abstract: A charging system for a vehicle includes a first energy storage device, a first DC-DC converter coupled between a DC bus and the first energy storage device, and a controller. The controller is programmed to identify charging parameters of a charging source coupleable to the first energy storage device through the first DC-DC converter, apply an optimization algorithm to iteratively define a charging power allocation to charge the first energy storage device using the charging source, and selectively control the first DC-DC converter to recharge the first energy storage device in accordance with the charging power allocation. The charging power allocation optimizes at least one of a state of charge (SOC) and a state of health (SOH) of the first energy storage device.

    Abstract translation: 一种用于车辆的充电系统包括第一能量存储装置,耦合在DC总线和第一能量存储装置之间的第一DC-DC转换器和控制器。 控制器被编程为通过第一DC-DC转换器来识别可耦合到第一能量存储装置的充电源的充电参数,应用优化算法来迭代地定义充电功率分配以使用充电源对第一能量存储装置充电, 并且根据充电功率分配选择性地控制第一DC-DC转换器对第一能量存储装置再充电。 充电功率分配优化了第一能量存储装置的充电状态(SOC)和健康状态(SOH)中的至少一个。

    System and method for aircraft power management

    公开(公告)号:US10202206B2

    公开(公告)日:2019-02-12

    申请号:US14560555

    申请日:2014-12-04

    Abstract: A method implemented using at least one of the processor includes disposing a power source on a vehicle, wherein the power source is configured to power auxiliary loads of the aircraft. The method also includes connecting a power source disposed on a vehicle configured to engage an aircraft for ground operation, to auxiliary loads of the aircraft via an on-board power system. The method also includes performing energy management of the aircraft during the period of ground operation. The method further includes disconnecting the power source when an alternate electrical power is available to the on-board power system.

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