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
COMPOSITE MATERIAL COATED WITH CO-CURED UV/VISIBLE LIGHT RESISTANT FIBERGLASS FOR AIRCRAFT FUSELAGE ASSEMBLY
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
17.10.2023
Patent
Elektronische Ressource
Japanisch
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