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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    Title :

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


    Additional title:

    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



    Publication date :

    2024-06-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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