Patent ID: 8720826

Claim:
A window element for a double-shell skin field of an aircraft fuselage cell, the double-shell skin field including a core structure disposed between an inner covering layer and an outer covering layer and having an opening, the window element comprising: a window frame disposed within the opening of the double-shell skin field; having a window module disposed in the window frame; and, wherein the frame is disposed in an opening of the double-shell skin field, and wherein the frame is connected to the double-shell skin field by a surrounding an embrasure profile surrounding the window frame, the embrasure profile connecting the window frame to the double-shell skin field and being positioned against a the core structure of the skin field at least in some regions, wherein the core structure includes an inner and an outer covering layer, wherein the embrasure profile includes a C-shaped cross-sectional geometry with an inner and an outer arm running parallel to one another, and wherein the inner and the outer arms are connect connected by a profile web, wherein the frame has an inner and an outer flange connected to one another by a flange web, wherein the outer flange includes a recess, and wherein the outer covering layer is positioned against the outer flange at least regions.