A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vertical takeoff and landing (VTOL) air vehicle



    Erscheinungsdatum :

    27.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Vertical Takeoff and Landing (VTOL) Air Vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | Europäisches Patentamt | 2017

    Freier Zugriff