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) __-_____


    Access

    Download


    Export, share and cite



    Title :

    Vertical takeoff and landing (VTOL) air vehicle



    Publication date :

    2019-02-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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. | European Patent Office | 2020

    Free access

    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | European Patent Office | 2019

    Free access

    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | European Patent Office | 2016

    Free access

    VERTICAL TAKEOFF AND LANDING VTOL AIR VEHICLE

    European Patent Office | 2020

    Free access

    Vertical takeoff and landing (VTOL) air vehicle

    TAYLOR DANA J / TOKUMARU PHILLIP T / HIBBS BART DEAN et al. | European Patent Office | 2021

    Free access