A landing method for a flight body capable of achieving both vertical takeoff and landing and improving fuel consumption while improving landing performance. A flight body, comprising: a plurality of rotary wing parts that generate at least lift; a thrust drive device; and a fixed wing, wherein the thrust drive device generates thrust on the opposite side of horizontal flight during landing. Furthermore, the thrust drive device is equipped with a propeller, which, when landing, rotates in the opposite direction to that of horizontal flight. Furthermore, the thrust drive system generates more thrust to the opposite side during an emergency crash than during a landing.


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    Titel :

    FLIGHT BODY, LANDING METHOD, AND PROGRAM


    Beteiligte:
    SUZUKI YOICHI (Autor:in)

    Erscheinungsdatum :

    20.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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