The present disclosure relates to vertical takeoff and landing aerial vehicles configured to transport a payload. The vehicle comprises a main lifting body and a propulsion assembly coupled to the main lifting body. The main lifting body comprises a substantially airfoil shaped cross-section, and extends laterally from a first tip to a second tip having a pressure side and a suction side. Further, the propulsion assembly comprises two central thrusters located at the suction side and two lateral thrusters located at the pressure side. Additionally, the lateral thrusters are located closer to the respective tips than the central thrusters.


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    Title :

    VERTICAL TAKEOFF AND LANDING AERIAL VEHICLES


    Additional title:

    LUFTFAHRZEUGE MIT VERTIKALEM STARTEN UND LANDEN
    VÉHICULES AÉRIENS À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX



    Publication date :

    2024-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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