The invention aims to make aircraft doors easier to open by preventing ice formation or, at the very least, favoring rapid breaking of the ice on the door edges connected to the skin of the fuselage. To that end, it is provided to supply energy along the door when specific conditions are met. According to one embodiment, an anti-icing/de-icing system for an aircraft door (1) according to the invention includes an excitation energy source and devices (81 to 83) for dissipating such energy extending parallel to a side surface (11) of the aircraft door (1), along a sealing gasket (4) support (5) secured to the door (1) across from a fuselage (2) side surface (21) framing (20) the door (1). The sealing gasket (4) of the door (1) is compressed against bearing (6) from a side surface (25) of the fuselage (2) when the door (1) is closed.


    Access

    Download


    Export, share and cite



    Title :

    Anti-icing / de-icing system for aircraft door and aircraft door equipped with such a system


    Contributors:

    Publication date :

    2018-07-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F16J Kolben , PISTONS



    ANTI-ICING / DE-ICING SYSTEM FOR AIRCRAFT DOOR AND AIRCRAFT DOOR EQUIPPED WITH SUCH A SYSTEM

    PERRIER CHRISTOPHE / BESSETTES CYRILLE / AMALRIC BERNARD et al. | European Patent Office | 2016

    Free access

    Aircraft anti-icing/de-icing system

    ZHU CHENGXIANG / LI QIANKUN / ZHU CHUNLING et al. | European Patent Office | 2025

    Free access


    Aircraft anti-icing system

    GREENBERG MICHAEL D / ZHENG ZHIJUN / BASZAK DAVID et al. | European Patent Office | 2019

    Free access