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
2023-10-17
Patent
Electronic Resource
Japanese
European Patent Office | 2023
|Co-Cured UV/Visible Light-Resistant Coated Composite Material for Aircraft Fuselage Assembly
European Patent Office | 2023
|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-RESISTANT FIBERGLASS COATED COMPOSITE MATERIAL FOR AIRCRAFT WING FUEL TANK ASSEMBLY
European Patent Office | 2023
|