The invention provides an aircraft alternating current emergency power supply system with power compensation and a control method. The aircraft alternating current emergency power supply system comprises an alternating current emergency power supply, an alternating current emergency power compensation device, an alternating current normal bus bar 1, an alternating current normal bus bar 2, a three-phase alternating current emergency bus bar, a single-phase alternating current emergency bus bar, a static inverter and a direct current emergency bus bar. Wherein the three-phase alternating current interface end of the alternating current emergency power compensation device is respectively connected to the A phase, the B phase and the C phase of the three-phase alternating current emergency bus bar through the TPACEC, the single-phase alternating current interface end of the alternating current emergency power compensation device is connected to the single-phase alternating current emergency bus bar through the SPACEC3, and the neutral point of the alternating current emergency power compensation device is grounded; the three-phase alternating current emergency bus bar is connected with an alternating current emergency power supply through an EGLC, the three-phase alternating current emergency bus bar is connected with an alternating current normal bus bar 1 through an LACETR, and the three-phase alternating current emergency bus bar is connected with an alternating current normal bus bar 2 through an RAETR.

    本申请提供一种带功率补偿的飞机交流应急电源系统及控制方法,飞机交流应急电源系统包含交流应急电源、交流应急功率补偿装置、交流正常汇流条1、交流正常汇流条2、三相交流应急汇流条、单相交流应急汇流条、静止逆变器、直流应急汇流条,其中:交流应急功率补偿装置的三相交流接口端通过TPACEC分别连接到三相交流应急汇流条的A相、B相和C相,交流应急功率补偿装置的单相交流接口端通过SPACEC3连接到单相交流应急汇流条,交流应急功率补偿装置的中性点接地;三相交流应急汇流条通过EGLC与交流应急电源连接,三相交流应急汇流条通过LACETR与交流正常汇流条1连接,三相交流应急汇流条通过RACETR与交流正常汇流条2连接。


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    Titel :

    Aircraft alternating current emergency power supply system with power compensation and control method


    Weitere Titelangaben:

    一种带功率补偿的飞机交流应急电源系统及控制方法


    Beteiligte:
    YANG WEIPENG (Autor:in) / CHENG YAN (Autor:in) / WANG RUI (Autor:in) / XUE XIAODAN (Autor:in)

    Erscheinungsdatum :

    2024-04-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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