This invention discloses an aerial device (AD) for manned or unmanned flight, comprising a fuselage main body coupled with two or more aerodynamic units via bearings. Each aerodynamic unit is independently moveable and controllable, and thus able to create their own unique aerodynamic vectors, all of which are combined in varying manners to control the flight of the AD. Each unit comprises a structural part, a thruster with a propeller, and a servo wing positioned behind the propeller. More aerodynamic units may be combined with the main body in order to create more control. The units may be programmed or controlled manually to offset or otherwise account for varying environmental conditions such as slope, wind, and turbulence. The apparatus may further be coupled with a PID controller with a multidimensional field of input and output parameters.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Stabilized VTOL flying apparatus and aircraft


    Beteiligte:
    BONDAREV DMITRIY (Autor:in) / RAKHIN TIMOFEY (Autor:in) / BORISOV EVGENII (Autor:in)

    Erscheinungsdatum :

    28.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Flying-wing and VTOL flying-wing aircraft

    CHEN FRANKLIN Y K | Europäisches Patentamt | 2015

    Freier Zugriff

    VTOL flying wing and flying wing aircraft

    CHEN FRANKLIN Y K | Europäisches Patentamt | 2022

    Freier Zugriff

    BLOWN FLYING-WING CTOL/VTOL TAILSITTER AIRCRAFT

    DIETRICH CARL / LOZANO BRIAN / MYJAK JEFF et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Blown flying wing CTOL/VTOL tailsitter aircraft

    DIETRICH CARL / LOZANO BRIAN / MYJAK JEFF et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Tailsitter VTOL flying wing aircraft attitude control

    Liang, Jianjian / Fei, Qing / Wang, Bo et al. | IEEE | 2016