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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    FINK AXEL (Autor:in) / KIESEWETTER UWE (Autor:in) / KICKER KLAUS (Autor:in)

    Erscheinungsdatum :

    2020-08-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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

    FINK AXEL / KIESEWETTER UWE / KICKER KLAUS | Europäisches Patentamt | 2023

    Freier Zugriff

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

    FINK AXEL / KIESEWETTER UWE / KICKER KLAUS | Europäisches Patentamt | 2021

    Freier Zugriff

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

    ARNOLD FELIX / TOMENENDAL MARTIN | Europäisches Patentamt | 2023

    Freier Zugriff

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

    ARNOLD FELIX / TOMENENDAL MARTIN | Europäisches Patentamt | 2021

    Freier Zugriff

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

    SHANG LIZHI / IVANTYSYNOVA MONIKA | Europäisches Patentamt | 2020

    Freier Zugriff