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.


    Access

    Download


    Export, share and cite



    Title :

    FLIGHT VEHICLE AND FLIGHT VEHICLE SYSTEM


    Contributors:

    Publication date :

    2025-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    FLIGHT VEHICLE, FLIGHT VEHICLE SYSTEM, FLIGHT VEHICLE CONTROL METHOD, AND MANIPULATOR

    WAKE CHIHIRO / SAITO ATSUNORI / KATO HIROKI | European Patent Office | 2021

    Free access

    FLIGHT SYSTEM FOR FLIGHT VEHICLE, AND FLIGHT METHOD FOR FLIGHT VEHICLE

    OKIDAN KAZUMA | European Patent Office | 2017

    Free access

    FLIGHT VEHICLE AND FLIGHT VEHICLE CONTROL SYSTEM

    ATSUMI KAZUYA | European Patent Office | 2020

    Free access


    FLIGHT VEHICLE AND FLIGHT VEHICLE POSITIONING SYSTEM

    KOMATSU NOBUAKI / ITO TOMOKO | European Patent Office | 2021

    Free access