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。
Co-cured uv/visible light resistant glass fiber coated composites for aircraft fuselage components
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
2023-10-17
Patent
Electronic Resource
Chinese
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 |
Co-Cured UV/Visible Light-Resistant Coated Composite Material for Aircraft Fuselage Assembly
European Patent Office | 2023
|European Patent Office | 2023
|European Patent Office | 2023
|European Patent Office | 2023
|Co-cured uv/visible light resistant composites for structural aircraft components
European Patent Office | 2023
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