A compound rotorcraft with a fuselage and at least one main rotor, the fuselage comprising a lower side and an upper side that is opposed to the lower side, the at least one main rotor being arranged at the upper side, wherein at least one propeller is provided and mounted to a fixed wing arrangement that is laterally attached to the fuselage, the fixed wing arrangement comprising at least one upper wing that is arranged at an upper wing root joint area provided at the upper side of the fuselage and at least one lower wing that is arranged at a lower wing root joint area provided at the lower side of the fuselage, the upper and lower wings being at least interconnected at an associated interconnection region.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    COMPOUND ROTORCRAFT


    Beteiligte:
    FINK AXEL (Autor:in) / BLACHA MARTIN (Autor:in)

    Erscheinungsdatum :

    2017-07-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    COMPOUND ROTORCRAFT

    DR FINK AXEL / BLACHA MARTIN | Europäisches Patentamt | 2017

    Freier Zugriff

    Compound rotorcraft

    FINK AXEL / BLACHA MARTIN | Europäisches Patentamt | 2018

    Freier Zugriff

    COMPOUND ROTORCRAFT

    Europäisches Patentamt | 2018

    Freier Zugriff

    Compound type rotorcraft

    WANG ZHICHENG | Europäisches Patentamt | 2016

    Freier Zugriff

    COMPOUND ROTORCRAFT WITH PROPELLER

    CARTER JR JAY W / LEWIS JEFFREY R / PERYEA MARTIN | Europäisches Patentamt | 2022

    Freier Zugriff