A VTOL (vertical take-off and landing) box-wing aerial vehicle with multirotor to provide VTOL flight includes a detachable cabin, centered fuselage, a pair of first wings extending outward from the upper portion of the fuselage and a pair of second wings extending outwardly and from the lower portion of the fuselage. The first and second wings are spaced apart longitudinally and vertically. The pylon joints the first wing and second wing at the tip to form the box-wing. The pylon includes heading control rudder. Secured to the wing or pylon or both wing and pylon, an overhead boom extending longitudinally to support a plurality of lift rotors or tiltable rotors for VTOL flight. Finally, the fuselage mounted push rotor or the overhead boom mounted tiltable rotors propel the vehicle forward to generate lift from the wings. Furthermore, the wings are equipped with elevators and ailerons for flight control.


    Access

    Download


    Export, share and cite



    Title :

    VTOL BOX-WING MULTIROTOR AERIAL VEHICLE


    Contributors:
    WANG XI (author)

    Publication date :

    2022-12-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    VTOL box-wing multirotor aerial vehicle

    WANG XI | European Patent Office | 2023

    Free access

    MULTIROTOR JOINED-WING AIRCRAFT WITH VTOL CAPABILITIES

    FINK AXEL / KIESEWETTER UWE / KICKER KLAUS | European Patent Office | 2020

    Free access

    Free Wing Multirotor Transitional S/VTOL Aircraft

    DOLEJSI EDWARD | European Patent Office | 2022

    Free access

    Multirotor joined-wing aircraft with VTOL capabilities

    FINK AXEL / KIESEWETTER UWE / KICKER KLAUS | European Patent Office | 2021

    Free access

    MULTIROTOR VTOL DRONE

    GOLOSHCHAPOV VLADLEN MIKHAJLOVICH / BAKLIN ANDREJ ALEKSANDROVICH / ASANINA DAR JA ANDREEVNA et al. | European Patent Office | 2015

    Free access