DC POWER ARCHITECTURE FOR REMOTE APU START
    1.
    发明申请
    DC POWER ARCHITECTURE FOR REMOTE APU START 有权
    用于远程APU启动的直流电源架构

    公开(公告)号:US20130334875A1

    公开(公告)日:2013-12-19

    申请号:US13526553

    申请日:2012-06-19

    申请人: Phuoc D. Nguyen

    发明人: Phuoc D. Nguyen

    IPC分类号: H02J9/00 B60L1/00

    摘要: A circuit and methods for remote auxiliary power unit startup are presented. A first node is coupled to a ground by action of a momentary switch to initiate an activation, and the first node is coupled to the ground by action of a latching relay in response to the activation. An auxiliary power unit is coupled to a hot battery by action of a bi-polar relay in response to the activation.

    摘要翻译: 提出了远程辅助电源单元启动的电路和方法。 第一节点通过瞬时开关的动作耦合到地面以启动激活,并且响应于激活,第一节点通过锁存继电器的动作耦合到地面。 响应于激活,辅助动力单元通过双极继电器的动作耦合到热电池。

    DC power architecture for remote APU start
    3.
    发明授权
    DC power architecture for remote APU start 有权
    用于远程APU启动的直流电源架构

    公开(公告)号:US09024467B2

    公开(公告)日:2015-05-05

    申请号:US13526553

    申请日:2012-06-19

    申请人: Phuoc D. Nguyen

    发明人: Phuoc D. Nguyen

    IPC分类号: B60L1/00 B64D41/00 F02N11/08

    摘要: A circuit and methods for remote auxiliary power unit startup are presented. A first node is coupled to a ground by action of a momentary switch to initiate an activation, and the first node is coupled to the ground by action of a latching relay in response to the activation. An auxiliary power unit is coupled to a hot battery by action of a bi-polar relay in response to the activation.

    摘要翻译: 提出了远程辅助电源单元启动的电路和方法。 第一节点通过瞬时开关的动作耦合到地面以启动激活,并且响应于激活,第一节点通过锁存继电器的动作耦合到地面。 响应于激活,辅助动力单元通过双极继电器的动作耦合到热电池。

    Power control system pseudo power-up, aircraft including the power control system and method of controlling power in an aircraft
    4.
    发明授权
    Power control system pseudo power-up, aircraft including the power control system and method of controlling power in an aircraft 有权
    电力控制系统伪上电,飞机包括电源控制系统和飞机控制电源的方法

    公开(公告)号:US07656637B2

    公开(公告)日:2010-02-02

    申请号:US11554433

    申请日:2006-10-30

    IPC分类号: H01H73/00

    摘要: A power control system with a pseudo-power up, an aircraft including the power control system and a method of controlling power in an aircraft. On-board wiring is protected from faults by electronic circuit breakers (ECBs), which may also control AC/DC electrical power supplies of on-board electrical/electronic equipment. A computer processor operating a user interface, e.g., a graphical user interface (GUI), through a display. An on-board store stores the GUI, other computer applications and the current state of each ECB, e.g., in a breaker state table. In a pseudo-power mode up, the stored circuit breaker state is available without providing power to the ECBs and, correspondingly to the coupled on-board electrical systems. When terminated, the system can power off, or proceed to normal power where each ECB is configured according to the breaker state table prior to providing power to protected systems.

    摘要翻译: 具有伪加电功率的功率控制系统,包括功率控制系统的飞机和控制飞机中的功率的方法。 电路断路器(ECB)也可以保护车载接线不受故障影响,也可以控制车载电气/电子设备的交流/直流电源。 通过显示器操作用户界面(例如,图形用户界面(GUI))的计算机处理器。 车载存储器将GUI,其他计算机应用程序和每个ECB的当前状态存储在断路器状态表中。 在伪功率模式下,存储的断路器状态可用,而不向ECB提供电力,并且相应于耦合的车载电气系统。 当终端时,系统可以关闭电源,或者在向受保护的系统提供电源之前,根据断路器状态表配置每个ECB的正常电源。