To disclose a co-curable composite fuselage assembly.SOLUTION: An aircraft fuselage includes: a co-curable and co-cured UV/visible light resistant fiberglass-coated UV/visible light composite structural material substrate; and a co-cured UV/visible light resistant fiberglass-coated composite material substrate.SELECTED DRAWING: Figure 2A

    【課題】共硬化可能な複合材料胴体アセンブリが開示される。【解決手段】航空機胴体は、共硬化可能な及び共硬化されたUV/可視光耐性繊維ガラスでコーティングされたUV/可視光複合材構造材料基板、及び共硬化されたUV/可視光耐性繊維ガラスでコーティングされた複合材料基板を含む。【選択図】図2A


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    Titel :

    COMPOSITE MATERIAL COATED WITH CO-CURED UV/VISIBLE LIGHT RESISTANT FIBERGLASS FOR AIRCRAFT FUSELAGE ASSEMBLY


    Weitere Titelangaben:

    航空機胴体アセンブリ用の共硬化されたUV/可視光耐性繊維ガラスでコーティングされた複合材料


    Beteiligte:

    Erscheinungsdatum :

    17.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B05D PROCESSES FOR APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TO SURFACES, IN GENERAL , Verfahren zum Aufbringen von Flüssigkeiten oder von anderen fließfähigen Stoffen auf Oberflächen allgemein / B64C AEROPLANES , Flugzeuge



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