Composite material protection from UV degradation is disclosed by providing a co-cured composite material substrate co-cured with a UV/visible light-resistant fiberglass layer to form co-cured composite materials for exclusively imparting UV/visible light-resistant properties to co-cured composite material substrates for use in UV/visible light-resistant vehicle fuel tank assemblies.
Co-Cured UV-Resistant Fiberglass Coated Composite Material for Aircraft Wing Fuel Tank Assembly
2023-10-05
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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 |
CO-CURED UV-RESISTANT FIBERGLASS COATED COMPOSITE MATERIAL FOR AIRCRAFT WING FUEL TANK ASSEMBLY
European Patent Office | 2023
|CO-CURED UV-RESISTANT FIBERGLASS-COATED COMPOSITE MATERIAL FOR AIRCRAFT WING FUEL TANK ASSEMBLY
European Patent Office | 2023
|Co-Cured UV/Visible Light-Resistant Coated Composite Material for Aircraft Wing Fuel Tank Assembly
European Patent Office | 2023
|European Patent Office | 2023
|European Patent Office | 2023
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