An unmanned aerial vehicle according to an aspect of the present invention includes: an aerial vehicle body capable of flying; a winding machine provided to the aerial vehicle body and capable of winding and unwinding a linear member an end of which is connectable to a delivery target; and a fall prevention mechanism provided to the aerial vehicle body and capable of holding the delivery target disconnected from the linear member.


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    Titel :

    UNMANNED AERIAL VEHICLE, AERIAL VEHICLE CONTROL SYSTEM AND TRANSPORTATION METHOD


    Beteiligte:
    INUMA TAKAYOSHI (Autor:in) / TAZUME TOSHIAKI (Autor:in)

    Erscheinungsdatum :

    2021-07-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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