A multirotor aircraft that is adapted for vertical take-off and landing. The multirotor aircraft comprises a fuselage, a tail boom that is provided with a vertical fin, a thrust producing units assembly that is provided for producing thrust in operation, at least one lower wing which comprises a lower wing inboard section that is connected to the fuselage and a lower wing outboard section that forms a lower wing tip, and at least one upper wing which is connected to the vertical fin and which forms an upper wing tip. The at least one upper wing is joined to the at least one lower wing in a joined-wing configuration.


    Access

    Download


    Export, share and cite



    Title :

    Multirotor joined-wing aircraft with VTOL capabilities


    Contributors:
    FINK AXEL (author) / KIESEWETTER UWE (author) / KICKER KLAUS (author)

    Publication date :

    2021-04-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    MULTIROTOR JOINED-WING AIRCRAFT WITH VTOL CAPABILITIES

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

    Free access

    A MULTIROTOR JOINED-WING AIRCRAFT WITH VTOL CAPABILITIES

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

    Free access

    Free Wing Multirotor Transitional S/VTOL Aircraft

    DOLEJSI EDWARD | European Patent Office | 2022

    Free access

    Multirotor VTOL aircraft

    Kirchner, M.E. / Front, J.V. | Engineering Index Backfile | 1968


    VTOL box-wing multirotor aerial vehicle

    WANG XI | European Patent Office | 2023

    Free access