A method for joining a window frame to a fuselage skin of an aircraft made of a fiber composite material, includes providing the window frame, making a window opening in the fuselage skin, arranging a curable connecting layer around the window opening, pressing the window frame onto the connecting layer, hardening the composite of fuselage skin, connecting layer and window opening.
Method For Joining A Window Frame To A Fuselage Skin Of An Aircraft Made Of A Fiber Composite Material
05.12.2024
Patent
Elektronische Ressource
Englisch
Method for connecting window frame to fuselage skin of aircraft made of fibre composite material
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