A method is proposed for connecting a window frame to a fuselage skin of an aircraft made of a fibre composite material, the method comprising providing the window frame, making a window in the fuselage skin, arranging a curable connecting layer around the window, pressing the window frame onto the connecting layer, and hardening the composite of the fuselage skin, the connecting layer and the window.

    提出了一种用于将窗框连接到飞机的由纤维复合材料制成的机身蒙皮的方法,该方法包括提供窗框、在机身蒙皮中制作窗口、围绕窗口布置可固化的连接层、将窗框按压到连接层上、使机身蒙皮、连接层和窗口的复合物硬化。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    用于将窗框连接到飞机的由纤维复合材料制成的机身蒙皮的方法


    Beteiligte:

    Erscheinungsdatum :

    03.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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

    SCHOLLER JOCHEN / VRIJBERGEN MICHIEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Bonded aluminium window frame on fibre metal laminate fuselage skin

    PELLENKOFT FREDERIK / GENNAI ALESSANDRO | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft fuselage portion made of composite material

    BERNADET PHILIPPE / DELAHAYE ROMAIN | Europäisches Patentamt | 2015

    Freier Zugriff

    FUSELAGE SKIN WINDOW UNIT FOR AN AIRCRAFT

    ORLOV DIMITRI | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT FUSELAGE FRAME OF COMPOSITE MATERIAL WITH STABILISING RIBS

    AREVALO RODRIGUEZ ELENA / CRUZ DOMINIGUEZ FRANCISCO JOSE | Europäisches Patentamt | 2018

    Freier Zugriff