An aircraft wing device having one or more numbered wing sets, each wing set further comprising: one or more internal wings, one or more external wings and a transition unit. The internal wings are used to structurally connect the wing set with the main aircraft body, and the external wings are capable of being positionally adjusted and maneuvered by way of vertical, horizontal, or angular movement. The device not only reduces the wingspan of the traditionally used aircraft wings, but also provides better stability and reduces the takeoff time. The wing sets may be positionally staggered on the aircraft body, height wise for aerodynamics efficiency and lift efficiency.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT WINGS WITH REDUCED WINGSPAN


    Contributors:

    Publication date :

    2021-08-19


    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



    SHORTENING WINGSPAN OF AN AIRCRAFT

    GLEASON-CHAPELL KEILY MADISON / GOOD MARK STEVEN | European Patent Office | 2024

    Free access

    SHORTENING WINGSPAN OF AN AIRCRAFT

    GLEASON-CHAPELL KEILY MADISON / GOOD MARK STEVEN / DEES PAUL | European Patent Office | 2024

    Free access

    Novel wingspan vehicle

    ZHANG GUOBING | European Patent Office | 2021

    Free access

    Wingspan type cargo compartment

    WANG MINGLIANG / HAN WENLAI / WEN GUANG et al. | European Patent Office | 2022

    Free access