An aircraft wing is provided having a wing leading edge, a cut-out opening in the wing leading edge, a telescopic tube extending through the cut-out opening and connected to an internal duct of a wing leading edge slat to establish fluid communication with heated air associated with an aircraft anti-icing system, wherein the telescopic tube is moveable between retracted and extended conditions in response to the wing leading edge slat being moved between slat retraction and deployment positions, respectively, and a cover assembly comprising a cover member operatively connected to the telescopic tube to close the cut-out opening and allow synchronous movement of the cover member with the telescopic tube in response to the telescopic tube being moved between the retracted and extended conditions thereof.


    Access

    Download


    Export, share and cite



    Title :

    Articulated cover assembly for wing leading edge slat telescopic tube duct


    Contributors:

    Publication date :

    2023-08-01


    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



    ARTICULATED COVER ASSEMBLY FOR WING LEADING EDGE SLAT TELESCOPIC TUBE DUCT

    ANTUNES MARCO ANTONIO | European Patent Office | 2020

    Free access

    SHUTTERING MECHANISM FOR WING SLAT TELESCOPIC TUBE DUCT

    ANTUNES MARCO ANTONIO / MINO ERIK KEITI | European Patent Office | 2020

    Free access

    Shuttering mechanism for wing slat telescopic tube duct

    ANTUNES MARCO ANTONIO / MINO ERIK KEITI | European Patent Office | 2022

    Free access

    Leading edge slat and wing of aircraft

    LI YAN / CHEN MENGYING / WANG BO | European Patent Office | 2024

    Free access

    Leading edge slat

    COMMIS BEN / LYONS NEIL / KAY EDMUND | European Patent Office | 2022

    Free access