An anti-aircraft system is described and includes an unmanned aerial vehicle (UAV) comprising a body; a wing connected to the body; and propulsion systems associated with the wing, wherein the propulsion systems comprise pylons releasably connected to opposite ends of the wing such that the propulsion systems may be selectively released from the wing during flight of the UAV.


    Access

    Download


    Export, share and cite



    Title :

    Unmanned aerial vehicle for anti-aircraft applications


    Contributors:

    Publication date :

    2024-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



    UNMANNED AERIAL VEHICLE FOR ANTI-AIRCRAFT APPLICATIONS

    DEARMAN MICHAEL DEAN | European Patent Office | 2022

    Free access

    Anti-reflection unmanned aerial vehicle aircraft control equipment

    ZHU WENWU / LIN XIAO / DENG YINZHOU et al. | European Patent Office | 2022

    Free access

    Unmanned aerial vehicle/unmanned aircraft system

    OAKLEY JOHN ROBERT / HEATH DAVID SCOTT | European Patent Office | 2017

    Free access

    Unmanned aerial vehicle coaxial aircraft

    LIU DONGXING | European Patent Office | 2021

    Free access

    Unmanned aerial vehicle anti-overturning method and unmanned aerial vehicle

    HAO HUICHUAN / ZHANG WENLI / YANG XU | European Patent Office | 2023

    Free access