A multirotor aircraft 10 that is adapted for vertical take-off and landing, comprising a fuselage, a thrust producing units assembly that is provided for producing thrust in operation, and a forward-swept wing that comprises a portside half wing and a starboard side half wing. Each one of the portside and starboard side half wings comprises an inboard section that is connected to the fuselage and an outboard section that forms a wing tip. The inboard sections of the portside and starboard side half wings form a central wing region. The portside and starboard side half wings are respectively connected in the region of their wing tips to an associated outboard wing pod that supports at least two non-tiltably mounted thrust producing units of the thrust producing units assembly.


    Access

    Download


    Export, share and cite



    Title :

    Multirotor aircraft that is adapted for vertical take-off and landing


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

    Publication date :

    2023-07-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    MULTIROTOR AIRCRAFT THAT IS ADAPTED FOR VERTICAL TAKE-OFF AND LANDING

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

    Free access

    A MULTIROTOR AIRCRAFT THAT IS ADAPTED FOR VERTICAL TAKE-OFF AND LANDING (VTOL)

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

    Free access

    Method for controlling a multirotor aircraft for the vertical take-off and landing as well as multirotor aircraft

    ARNOLD FELIX / TOMENENDAL MARTIN | European Patent Office | 2023

    Free access

    Method for Controlling a Multirotor Aircraft for the Vertical Take-Off and Landing as well as Multirotor Aircraft

    ARNOLD FELIX / TOMENENDAL MARTIN | European Patent Office | 2021

    Free access

    DISPLACEMENT CONTROL HYDROSTATIC PROPULSION SYSTEM FOR MULTIROTOR VERTICAL TAKE OFF AND LANDING AIRCRAFT

    SHANG LIZHI / IVANTYSYNOVA MONIKA | European Patent Office | 2020

    Free access