IMPROVED COMPOSITE RESIN WINDOW FRAME CONSTRUCTION FOR AIRPLANES AND METHOD OF PRODUCING THE SAME

摘要

A composite resin window frame for installation in a composite resin airplane fuselage has an inner flange for receiving and securely affixing an aircraft window transparency and an outer flange adapted for connection to the airplane fuselage structure. The frame has a generally flat configuration which does not require any additional strength enhancing member such as an additional flange perpendicular to the structure. The composite resin window frame has sufficient strength to securely affix a window transparency to a composite resin fuselage.