Window element for double-shelled skin field of fuselage cell of aircraft, has recess attached into double-shelled skin field for accommodating window frame, where window frame is connected with double-shelled skin field

摘要

The window element (1) has a window frame (2) with a window package (3) that is accommodated in the window frame. A recess (4) is attached into a double-shelled skin field (5) for accommodating the window frame, where the window frame is connected with the double-shelled skin field by a circulating soffit profile lying close to a core structure. The soffit profile exhibits C-shaped cross section geometry with inner and outer sides lying parallel to each other. The window frame has an inner flange and an outer flange connected by a flange bar.