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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ANTI-EROSION STRUCTURE FOR AIRCRAFTS


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

    Erscheinungsdatum :

    2016-02-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL



    Anti-erosion structure for aircrafts

    LUISET BENJAMIN / NAVARRE THOMAS / BOSCHET PATRICK et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFTS OEPRATING SYSTEM AIRCRAFTS OF AIRCRAFTS OPERATING SYSTEM AND OPERATIONG METHOD OF AIRCRAFTS

    HWANG SUN YU / LIM SEUNG HAN / HONG JIN SUNG et al. | Europäisches Patentamt | 2016

    Freier Zugriff


    SYNERGETIC NOISE ABSORPTION AND ANTI-ICING FOR AIRCRAFTS

    KHOZIKOV VYACHESLAV / FOLLET JESSE I / LAN JUSTIN H et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    SYNERGETIC NOISE ABSORPTION AND ANTI-ICING FOR AIRCRAFTS

    KHOZIKOV VYACHESLAV / FOLLET JESSE I / LAN JUSTIN H et al. | Europäisches Patentamt | 2020

    Freier Zugriff