One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.


    Access

    Download


    Export, share and cite



    Title :

    VERTICAL TAKEOFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV)


    Contributors:

    Publication date :

    2017-08-17


    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) unmanned aerial vehicle (UAV)

    CREASMAN SON F | European Patent Office | 2019

    Free access

    VERTICAL TAKEOFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV)

    CREASMAN SON F | European Patent Office | 2018

    Free access

    VERTICAL TAKEOFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV)

    CREASMAN SON F | European Patent Office | 2016

    Free access

    Vertical Takeoff and Landing Unmanned Aerial Vehicle (VTOL-UAV)

    SIMIONESCU PETRU A | European Patent Office | 2019

    Free access

    VERTICAL TAKEOFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV)

    CREASMAN SON F | European Patent Office | 2016

    Free access