A method for fabricating a composite wing structural component for an aircraft is described. The method comprises extruding a filler material into each mold channel of a plurality of mold channels of a die to form a plurality of filler segments, removing the plurality of filler segments from the plurality of mold channels of the die, and arranging the plurality of filler segments in a space in the composite structural component, the space being defined by a radius of the composite structural component, such that the filler segments are in end-to-end contact. The method further comprises curing the plurality of filler segments in the space to fuse the plurality of filler segments.


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    Titel :

    AIRCRRAFT COMPRISING COMPOSITE STRUCTURAL COMPONENT, AND METHOD FOR FORMING COMPOSITE STRUCTURAL COMPONENT


    Weitere Titelangaben:

    FLUGZEUG MIT EINEM STRUKTURBAUTEIL AUS VERBUNDWERKSTOFF UND VERFAHREN ZUR HERSTELLUNG EINES STRUKTURBAUTEILS AUS VERBUNDWERKSTOFF
    DÉTECTION COMPRENANT UN COMPOSANT STRUCTURAL COMPOSITE ET PROCÉDÉ DE FORMATION D'UN COMPOSANT STRUCTURAL COMPOSITE


    Beteiligte:

    Erscheinungsdatum :

    2023-11-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand



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