To provide co-curable and co-cured UV/visible light-resistant composite material assemblies comprising a co-curable UV/visible light-resistant lightning strike protection layer that can facilitate and streamline manufacture of composite material assemblies and sub-assemblies, including exterior assemblies and sub-assemblies for aircraft, vehicles, and objects exposed to electromagnetic effects including lightning strikes.SOLUTION: A co-curable composite material assembly (20a) comprises: a co-curable composite material substrate (22a); a co-curable ultraviolet (UV)/visible light-resistant lightning strike protection layer (23a). The co-curable composite material substrate is co-curable with the co-curable UV/visible light-resistant lightning strike protection layer at a temperature ranging from about 250°F to about 370°F.SELECTED DRAWING: Figure 2A

    【課題】雷電を含む電磁効果に曝露される航空機、ビークル、及び物体のための外部のアセンブリ及びサブアセンブリを含む複合材料アセンブリ及びサブアセンブリの製造を促進し合理化することが可能な、共硬化性の耐UV/可視光雷電保護層を含む共硬化性の耐UV/可視光複合材料アセンブリ及び共硬化された耐UV/可視光複合材料アセンブリが開示される。【解決手段】共硬化性の複合材料アセンブリ(20a)であって、共硬化性の複合材料基板(22a)と、共硬化性の耐紫外線(UV)/可視光雷電保護層(23a)と、を含み、前記共硬化性の複合材料基板が、約250°Fから約370°Fまでの範囲の温度で、前記共硬化性の耐UV/可視光雷電保護層と共硬化しうる、共硬化性の複合材料アセンブリ(20a)。【選択図】図2A


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    Title :

    CO-CURABLE AND CO-CURED UV/VISIBLE LIGHT-RESISTANT LIGHTNING STRIKE PROTECTION MATERIALS FOR COMPOSITE MATERIAL ASSEMBLIES


    Additional title:

    複合材料アセンブリのための共硬化性の耐UV/可視光雷電保護材料及び共硬化された耐UV/可視光雷電保護材料


    Contributors:

    Publication date :

    2024-02-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64U / B64G Raumfahrt , COSMONAUTICS / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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