A power supply circuit of an aircraft includes: a first power transmission path and a second power transmission path each configured to supply electric power from power generation units to one or more drive modules; and a third power transmission path configured to supply electric power from a charging device to the first power transmission path. When one or more batteries are charged with the electric power supplied from the charging device, the electric power is supplied from the charging device to the batteries via the first power transmission path, and the electric power is supplied from the charging device to the batteries via the second power transmission path.


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    Titel :

    POWER SUPPLY CIRCUIT OF AIRCRAFT


    Beteiligte:
    MITANI MANABU (Autor:in) / SHINOHARA SADAO (Autor:in) / YOSHIDA MASATAKA (Autor:in)

    Erscheinungsdatum :

    2023-08-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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