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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    Title :

    STRUCTURE ANTI-ÉROSION POUR AÉRONEFS


    Additional title:

    ANTI-EROSION STRUCTURE FOR AIRCRAFTS
    EROSIONSBESTÄNDIGE STRUKTUR FÜR FLUGZEUGE


    Contributors:

    Publication date :

    2018-07-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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    LUISET BENJAMIN / NAVARRE THOMAS / BOSCHET PATRICK et al. | European Patent Office | 2016

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    DIAGNOSTIC PERFECTIONNE POUR AERONEFS

    DUNSDON JONATHAN MARK | European Patent Office | 2018

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    SYSTEMES ET PROCEDES D'ALIMENTATION POUR AERONEFS

    RAJASHEKARA KAUSHIK / PONTONES GEORGE A | European Patent Office | 2017

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    Alternateurs-demarreurs pour les aeronefs

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