A flight vehicle includes a driver, a battery, a main body, a leg, and an annular power receiving coil. The driver is operable to rotate a rotor blade about a rotation axis. The battery is chargeable/dischargeable and supplies power to the driver. The main body accommodates the battery. The leg supports the main body during landing. The power receiving coil is electrically connected to the battery. The leg includes a landing portion that contacts the landing surface during landing. At the time of landing, the central axis of the power receiving coil extends parallel or substantially parallel to a normal direction of the landing surface. The power receiving coil is located on or in the landing portion.


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    Titel :

    FLIGHT VEHICLE AND FLIGHT VEHICLE SYSTEM


    Beteiligte:
    FUJITA NAOKI (Autor:in) / SHIMIZU JUNICHI (Autor:in)

    Erscheinungsdatum :

    16.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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