This lightning discharge induction system includes a flying object (1) flying in the air, a discharge electrode (11) provided to the flying object, a ground electrode (3) provided on the ground, an electric wire (2) connecting the discharge electrode (11) and the ground electrode (11), and a voltage control device (4) controlling a voltage generated in the discharge electrode (11). The voltage control device (4) includes a pulse power supply (41) for generating a pulse voltage, and a trigger switch (S1). By turning on the trigger switch (S1), a pulse voltage is supplied to the discharge electrode (11), a dielectric breakdown is caused between a thundercloud (50) and the discharge electrode (11), and the thundercloud (50) induces a lightning discharge


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    Titel :

    LIGHTNING DISCHARGE INDUCTION SYSTEM, LIGHTNING DISCHARGE INDUCTION AIRCRAFT, VOLTAGE CONTROL DEVICE


    Beteiligte:
    MASUDA TOSHIHISA (Autor:in) / MARUYAMA MASATO (Autor:in) / AOKI NOBUE (Autor:in) / ISHIYAMA FUMIHIKO (Autor:in) / ARAI NARUTO (Autor:in) / KATO JUN (Autor:in)

    Erscheinungsdatum :

    07.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H05F STATIC ELECTRICITY , Statische Elektrizität / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01T SPARK GAPS , Funkenstrecken




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