Method For Joining A Window Frame To A Fuselage Skin Of An Aircraft Made Of A Fiber Composite Material
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United States of America
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Issued Date -
Dec 5, 2024
app pub date -
May 30, 2024
filing date -
May 30, 2024
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Abstract
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.
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