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.


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    Titel :

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


    Beteiligte:
    PERRIER CHRISTOPHE (Autor:in) / BESSETTES CYRILLE (Autor:in) / AMALRIC BERNARD (Autor:in) / FLORENTZ BERTRAND (Autor:in) / TORRIS ANTOINE (Autor:in) / COME OLIVIER (Autor:in)

    Erscheinungsdatum :

    28.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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