Method for applying a cover (1) to an aircraft wing (2) comprising placing a skin (3) provided with one or more manholes (4) on the aircraft wing (2); placing a gasket (5) for the, or each, manhole (4) of the skin (3); placing a plug (6) in the, or each, manhole (4); and curing the aircraft wing (2) with the cover (1), the cover (1) comprising the skin (3), the gasket or gaskets (5) and the plug or plugs (6).The aircraft wing (2) comprises a cover (1) applied by said method including a skin (3), one or more gaskets (5) and one or more plugs (6).It reduces the application time, the recurrent costs and has a positive environmental footprint impact.


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    Titel :

    METHOD FOR APPLYING A COVER TO AN AIRCRAFT WING AND AIRCRAFT WING OBTAINED BY SAID METHOD


    Weitere Titelangaben:

    VERFAHREN ZUM AUFBRINGEN EINER ABDECKUNG AUF EINEN FLUGZEUGFLÜGEL UND DURCH DIESES VERFAHREN ERHALTENER FLUGZEUGFLÜGEL
    PROCÉDÉ D'APPLICATION D'UN CAPOT SUR UNE AILE D'AÉRONEF ET AILE D'AÉRONEF OBTENUE PAR LEDIT PROCÉDÉ



    Erscheinungsdatum :

    05.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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