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 5 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). EFFECTOR GRAPHIC SYMMETRIC 100 130 100 PITCH PITCH CYCLIC (NOSE UP POSITIVE) 120-J ASYMMETRIC 130 125 2. ROLL ELEVON (RIGHT ROLL POSITIVE) POSTIE)120 110 115 ASYMMETRIC 125 110 COLLECTIVE 3. YAW (NOSE RIGHT 135 140 POSITIVE) 145 155 110 150 155 SYMMETRIC 155 125 155 130 4 THRUST COLLECTIVE (FORWARD 135 140 POSITIVE) __-_____


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vertical takeoff and landing (VTOL) air vehicle



    Erscheinungsdatum :

    07.02.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    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 | 2016

    Freier Zugriff

    VERTICAL TAKEOFF AND LANDING VTOL AIR VEHICLE

    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 | 2021

    Freier Zugriff