An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle may have deployment mechanisms which deploy electric motor driven propellers from a forward facing to a vertical orientation. The wing mounted rotor assemblies may have split nacelles, wherein a forward portion of the nacelle deploys along with the electric motor and the propeller.


    Access

    Download


    Export, share and cite



    Title :

    AERODYNAMICALLY EFFICIENT LIGHTWEIGHT VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH DEPLOYABLE ROTORS


    Contributors:
    BEVIRT JOEBEN (author) / STOLL ALEX (author)

    Publication date :

    2022-05-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Aerodynamically efficient lightweight vertical take-off and landing aircraft with deployable rotors

    BEVIRT JOEBEN / STOLL ALEX | European Patent Office | 2023

    Free access

    Aerodynamically efficient lightweight vertical take-off and landing aircraft

    BEVIRT JOEBEN / STOLL ALEX | European Patent Office | 2024

    Free access

    Aerodynamically Efficient Lightweight Vertical Take-Off And Landing Aircraft

    BEVIRT JOEBEN / STOLL ALEX | European Patent Office | 2022

    Free access