An element including a leading edge forming a box delimited by a skin forming a lower surface and an upper surface and pierced with holes, in which the skin includes an inner wall and an outer wall that are electrically conductive and an electrically insulating intermediate wall, a pump for expelling or injecting air from or into the box. Each hole is equipped with an anti-clogging system including a conductive base, a needle made of piezoelectric material, one end of which is secured to the base, an electrical generator generating an electrical current in the needle, in which the form of the needle is such that a space is created between the needle and the edges of the hole, and in which the base has a recess in the extension of the space. Such an installation makes it possible to eliminate the residues which are lodged in the holes.


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    Titel :

    ELÉMENT D'AÉRONEF COMPORTANT UN BORD D'ATTAQUE PRÉSENTANT UN SYSTÈME POUR PRÉVENIR LE COLMATAGE DE TROUS RÉALISÉS DANS LE BORD D'ATTAQUE


    Weitere Titelangaben:

    AIRCRAFT ELEMENT COMPRISING A LEADING EDGE HAVING A SYSTEM FOR PREVENTING CLOGGING OF HOLES MADE IN THE LEADING EDGE
    ELEMENT EINES LUFTFAHRZEUGS, DAS EINE VORDERKANTE MIT EINEM SYSTEM UMFASST, UM EINE VERSCHMUTZUNG DER IN DIESER VORDERKANTE AUSGEFÜHRTEN LÖCHER ZU VERMEIDEN


    Beteiligte:

    Erscheinungsdatum :

    22.07.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten / H05H Plasmatechnik , PLASMA TECHNIQUE / H10N