A method is proposed for connecting a window frame to a fuselage skin of an aircraft made of a fibre composite material, the method comprising providing the window frame, making a window in the fuselage skin, arranging a curable connecting layer around the window, pressing the window frame onto the connecting layer, and hardening the composite of the fuselage skin, the connecting layer and the window.
提出了一种用于将窗框连接到飞机的由纤维复合材料制成的机身蒙皮的方法,该方法包括提供窗框、在机身蒙皮中制作窗口、围绕窗口布置可固化的连接层、将窗框按压到连接层上、使机身蒙皮、连接层和窗口的复合物硬化。
Method for connecting window frame to fuselage skin of aircraft made of fibre composite material
用于将窗框连接到飞机的由纤维复合材料制成的机身蒙皮的方法
03.12.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2024
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