A method for joining a window frame to a fuselage skin of an aircraft made of a fiber composite material, includes providing the window frame, making a window opening in the fuselage skin, arranging a curable connecting layer around the window opening, pressing the window frame onto the connecting layer, hardening the composite of fuselage skin, connecting layer and window opening.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Method For Joining A Window Frame To A Fuselage Skin Of An Aircraft Made Of A Fiber Composite Material


    Beteiligte:

    Erscheinungsdatum :

    05.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



    Method for connecting window frame to fuselage skin of aircraft made of fibre composite material

    SCHOLLER JOCHEN / VRIJBERGEN MICHIEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Joining composite fuselage sections along window belts

    DOPKER BERNHARD / CHI-HUA CHAN WALLACE / OSTROFF HENRI MICHAEL | Europäisches Patentamt | 2016

    Freier Zugriff

    JOINING COMPOSITE FUSELAGE SECTIONS ALONG WINDOW BELTS

    Europäisches Patentamt | 2019

    Freier Zugriff

    Joining composite fuselage sections along window belts

    DOPKER BERNHARD / CHAN WALLACE CHI-HUA / OSTROFF HENRI MICHAEL | Europäisches Patentamt | 2021

    Freier Zugriff

    JOINING COMPOSITE FUSELAGE SECTIONS ALONG WINDOW BELTS

    DOPKER BERNHARD / CHAN WALLACE CHI-HUA / OSTROFF HENRI MICHAEL | Europäisches Patentamt | 2020

    Freier Zugriff