A flight object included in a Faraday cage, a power supply unit included in the Faraday cage and supplies power to the flight object, a first voltage-dependent switch connected between the Faraday cage and one of power supply lines that supplies power to the power supply unit, a second voltage-dependent switch connected between the Faraday cage and the other of power supply lines, a power supply device provided at an end of the power supply line on the ground surface side, a third voltage-dependent switch connected between one output terminal of the power supply device and the ground, and a fourth voltage-dependent switch connected between the other output terminal of the power supply device and the ground.


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    Titel :

    LIGHTNING STRIKE INDUCTION SYSTEM AND METHOD


    Beteiligte:
    MASUDA TOSHIHISA (Autor:in) / KATO JUN (Autor:in) / MARUYAMA MASATO (Autor:in)

    Erscheinungsdatum :

    23.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen / H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen



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