A flying wing vertical take-off and landing (VTOL) aircraft is provided and includes an empennageless-fuselage from which foldable wings extend outwardly, an empennageless-nacelle supported on each of the wings and a rigid rotor propeller disposed on each empennageless-nacelle, each of the propellers being drivable to rotate about only a single rotational axis defined along a longitudinal axis of the corresponding empennageless-nacelle and being fully cyclically controllable.


    Access

    Download


    Export, share and cite



    Title :

    FLYING WING VERTICAL TAKE-OFF AND LANDING AIRCRAFT


    Contributors:

    Publication date :

    2018-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    FLYING WING VERTICAL TAKE-OFF AND LANDING AIRCRAFT

    BOWER GEOFFREY C | European Patent Office | 2022

    Free access

    Flying wing vertical take-off and landing aircraft

    BOWER GEOFFREY C | European Patent Office | 2024

    Free access

    FLYING WING VERTICAL TAKE-OFF AND LANDING AIRCRAFT

    SCOTT MARK W / BUNTING COLIN KEMATER | European Patent Office | 2016

    Free access

    Flying wing vertical take-off and landing aircraft

    SCOTT MARK W / BUNTING COLIN KEMATER | European Patent Office | 2020

    Free access

    FLYING WING VERTICAL TAKE-OFF AND LANDING AIRCRAFT

    BOWER GEOFFREY C | European Patent Office | 2022

    Free access