A structure (10) for aircrafts, includes a part (20) including a metal leading edge (30), the leading edge (30) being covered by a coating (40) having a thickness which is less than or equal to ten micrometers and having a hardness higher than six hundred in the Vickers hardness test (HV). According to a mode of embodiment, the coating (40) is a multilayer stainless steel coating consisting of a superposition of layers with a low nitrogen gradient and layers with a high nitrogen gradient, the layers having a thickness essentially equal to a micrometer. An aircraft including such a structure is also described.


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    Titel :

    STRUCTURE ANTI-EROSION POUR AERONEFS


    Beteiligte:
    LUISET BENJAMIN (Autor:in) / NAVARRE THOMAS (Autor:in) / BOSCHET PATRICK (Autor:in) / BILLARD ALAIN (Autor:in)

    Erscheinungsdatum :

    2016-04-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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