An aircraft is described and includes an airframe including first and second wings each having first and second oppositely disposed wing tips; first and second booms respectively extending longitudinally between the first and second wings and having forward and aft ends; first and second tail assemblies respectively coupled to aft ends of the first and second booms; first and second forward propulsion assemblies respectively coupled to the forward ends of the first and second booms, wherein the first and second forward propulsion assemblies are tiltable between a vertical takeoff and landing (“VTOL”) flight mode orientation and a forward flight mode orientation; first and second aft propulsion assemblies respectively coupled to upper ends of the tail assemblies, wherein the first and second aft propulsion assemblies are tiltable between a VTOL flight mode orientation and a forward flight mode orientation; and a payload module removably coupled to the airframe.


    Access

    Download


    Export, share and cite



    Title :

    VERTICAL TAKEOFF AND LANDING DUAL-WING AERIAL VEHICLE


    Contributors:

    Publication date :

    2020-05-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    VERTICAL TAKEOFF AND LANDING DUAL-WING AERIAL VEHICLE

    CAMPBELL KIP GREGORY | European Patent Office | 2020

    Free access

    VERTICAL TAKEOFF AND LANDING FIXED-WING UNMANNED AERIAL VEHICLE

    XIAO XIANG | European Patent Office | 2022

    Free access

    VERTICAL TAKEOFF AND LANDING FIXED WING URMANNED AERIAL VEHICLE

    HEEWOO LEE / SUNGYOUL PARK | European Patent Office | 2021

    Free access


    VERTICAL TAKEOFF AND LANDING UNMANNED AERIAL VEHICLE HAVING FIXED WING

    SEUNG MYEONG HUN / JANG JONG TAI / HAN SANG HYUCK et al. | European Patent Office | 2016

    Free access