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    • 9. 发明申请
    • INTEGRATED ELECTRICAL POWER DISTRIBUTION SYSTEM USING COMMON BUILDING BLOCKS
    • 使用通用建筑块的集成电力分配系统
    • US20080234838A1
    • 2008-09-25
    • US12018670
    • 2008-01-23
    • Milind GhanekarRandy J. FullerZhenning Z. LiuTed J. Gayowsky
    • Milind GhanekarRandy J. FullerZhenning Z. LiuTed J. Gayowsky
    • G05B11/01G06F17/00G05B15/02
    • H02J4/00B64D2221/00Y02T50/54
    • An electrical power distribution system includes a data bus, separate from the main aircraft data bus, internal to the aircraft electrical power distribution system and an electric power control unit (EPCU) in communication with the internal data bus. Primary and emergency power distribution subsystems include line replaceable modules (LRM) connected in the aircraft electrical power distribution system as electrical load control units (ELCU), each having a common supervisory control interface in communication with the internal data bus, while a secondary power distribution subsystem includes LRMs connected in the aircraft electrical power distribution system as solid state power control (SSPC) units, each having the common supervisory control interface in communication with the internal data bus. The common supervisory control interfaces all execute a common supervisory control logic for receiving commutation commands from the EPCU and providing status back to the EPCU.
    • 电力分配系统包括与主飞机数据总线分离的数据总线,与飞机配电系统内部以及与内部数据总线通信的电力控制单元(EPCU)。 主要和应急配电子系统包括连接在飞机配电系统中的线路可更换模块(LRM)作为电力负载控制单元(ELCU),每个电气负载控制单元具有与内部数据总线通信的通用监控控制接口,而二次配电 子系统包括作为固态功率控制(SSPC)单元连接在飞机配电系统中的LRM,每个单元具有与内部数据总线通信的通用监控控制接口。 通用的监控控制接口都执行一个通用的监控控制逻辑,用于从EPCU接收换向指令,并向EPCU提供状态。