ELECTRICAL SUPPLY SYSTEM FOR A MOTOR VEHICLE, AND CORRESPONDING ELECTRONIC CONTROL MODULE

    公开(公告)号:US20170259763A1

    公开(公告)日:2017-09-14

    申请号:US15594225

    申请日:2015-11-16

    发明人: Pierre CHASSARD

    摘要: The electrical supply system according to the invention is of the type comprising, on the one hand, an electrical power network having a first voltage electrically connecting first items of equipment comprising an electrical motor/generator, an inverter/rectifier and a first electrical energy store, and, on the other hand, an electrical service network having a second voltage that is less than the first voltage electrically connecting second items of equipment comprising a second electrical energy store, an electronic control unit controlling the energy transfers between the power network and the service network by means of at least one reversible DC/DC converter. The electronic unit comprises a first electronic module supplied by the power network exchanging information with the first items of equipment, and a second electronic module supplied by the service network exchanging information with the second items of equipment and electrically insulated from the first module.

    METHOD FOR STARTING AIRCRAFT ENGINES
    55.
    发明申请
    METHOD FOR STARTING AIRCRAFT ENGINES 有权
    启动飞机发动机的方法

    公开(公告)号:US20160208709A1

    公开(公告)日:2016-07-21

    申请号:US14915066

    申请日:2013-09-06

    发明人: Hao HUANG

    IPC分类号: F02C7/26 H02M7/68

    摘要: A method of starting an aircraft having at least a first starter/generator (S/G) and a second S/G using at least one inverter/converter and at least one of an AC power source and a first DC power source, the method includes selectively starting at least one of the first S/G or second S/G in an AC start mode and in a DC start mode.

    摘要翻译: 一种使用至少一个逆变器/转换器和至少一个AC电源和第一DC电源起动具有至少第一起动/发电机(S / G)和第二S / G的飞行器的方法,该方法 包括以交流启动模式和直流启动模式选择性地启动第一S / G或第二S / G中的至少一个。

    Engine autostart source selection
    56.
    发明授权
    Engine autostart source selection 有权
    引擎自动启动源选择

    公开(公告)号:US09376104B2

    公开(公告)日:2016-06-28

    申请号:US14173189

    申请日:2014-02-05

    摘要: A vehicle includes an engine, a transmission, and an electrical system. The electrical system has an auxiliary starter motor connected to a crankshaft of the engine, a high-voltage motor generator unit (MGU) connected to the crankshaft, and a controller. Execution of instructions by a processor causes the controller to determine a set of powertrain conditions in response to a requested autostart of the engine, e.g., state of charge and/or power limits of a high-voltage energy storage system (HV-ESS), torque limits of the MGU, and/or a crank angle of the engine. The controller determines whether the requested autostart may not succeed relative to a time or noise standard using the set of powertrain conditions, and transmits an autostart command to the MGU when the requested autostart may succeed. The controller transmits the autostart command to the auxiliary starter motor when the requested autostart will not succeed.

    摘要翻译: 车辆包括发动机,变速器和电气系统。 电气系统具有连接到发动机的曲轴的辅助起动电动机,连接到曲轴的高压电动发电机单元(MGU)和控制器。 执行处理器的指令使得控制器响应于所要求的发动机的自动启动来确定一组动力系条件,例如高压储能系统(HV-ESS)的充电状态和/或功率限制, MGU的扭矩极限和/或发动机的曲柄角。 控制器使用该组动力系条件来确定所请求的自动启动是否相对于时间或噪声标准不成功,并且当请求的自动启动可能成功时,将自动启动命令发送到MGU。 当所请求的自动启动不成功时,控制器将自动启动命令发送到辅助启动电机。

    ELECTRICAL APPARATUS
    60.
    发明申请
    ELECTRICAL APPARATUS 有权
    电气设备

    公开(公告)号:US20150198130A1

    公开(公告)日:2015-07-16

    申请号:US14420491

    申请日:2013-08-06

    发明人: Neil Dudley

    IPC分类号: F02N11/08

    摘要: An aircraft electrical apparatus includes an engine starter motor control unit configured to provide an AC input voltage to a transformer rectifier unit. The apparatus includes a transformer rectifier unit for supplying power to an aircraft DC supply bus. The engine starter motor control unit provides the AC input voltage to the transformer rectifier unit.

    摘要翻译: 飞机电气设备包括:发动机起动电动机控制单元,被配置为向变压器整流单元提供AC输入电压。 该装置包括用于向飞机DC电源总线供电的变压器整流单元。 发动机起动电机控制单元为变压器整流单元提供交流输入电压。