[Problem] To provide a flying vehicle that can achieve both vertical takeoff and landing and improve fuel efficiency, while achieving a stable landing. [Solution] A flying vehicle with a flight part connected to a plurality of rotor wing parts and a main wing, wherein the main wing is configured such that the lift produced by the main wing during landing is reduced compared to the lift produced by the main wing during cruising. Furthermore, the main wing is fixed at a forward tilt with respect to the flight part. Furthermore, the rotor wing is connected at an angle that produces propulsion and lift during cruise. Furthermore, the rotor blades are connected at an angle that generates propulsive force during cruise. Furthermore, the flight part is configured so that the rotary wing do not interfere with the flight part or the main wing during landing. Furthermore, the main wing is connected to the flight part via a rotary axis, and the main wing is configured to tilt forward about the rotary axis at an angle relative to the flight part during landing than during cruising.


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    Titel :

    FLYING VEHICLE


    Weitere Titelangaben:

    FLUGGERÄT
    VÉHICULE VOLANT


    Beteiligte:
    SUZUKI YOICHI (Autor:in)

    Erscheinungsdatum :

    26.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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