The invention relates to a co-cured UV/visible light resistant glass fiber coated composite for aircraft fuselage components. Disclosed are co-curable and co-curable anti-UV/visible glass fiber coated UV/visible composite structural material substrates, as well as aircraft fuselages comprising co-curable anti-UV/visible glass fiber coated composite material substrates, and methods of making the same.

    本发明的标题为“用于飞行器机身组件的共固化的抗UV/可见光玻璃纤维涂覆的复合材料”。公开了可共固化和共固化的抗UV/可见光玻璃纤维涂覆的UV/可见光复合结构材料基材,以及包括共固化的抗UV/可见光玻璃纤维涂覆的复合材料基材的飞行器机身及其制造方法。


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    Titel :

    Co-cured uv/visible light resistant glass fiber coated composites for aircraft fuselage components


    Weitere Titelangaben:

    用于飞行器机身组件的共固化的抗UV/可见光玻璃纤维涂覆的复合材料


    Beteiligte:
    ADORO ALAN A (Autor:in) / ACKERMAN PATRICK K (Autor:in) / POWERS JAMES A (Autor:in)

    Erscheinungsdatum :

    17.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge / C08J Verarbeitung , WORKING-UP / C09D Überzugsmittel, z.B. Anstrichstoffe, Firnisse oder Lacke , COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS



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