A method for manufacturing an aircraft window frame, the frame including a first surface that has a curved joining zone extending about the entire perimeter of the frame, this latter being made of composite material and including a stack of fiber layers, as well as at least one reinforcement positioned in the joining zone. The manufacturing method includes a step of assembling the different fiber layers and the reinforcement during which at least a first seam is made to join at least the reinforcement and some layers, the first seam including stitches offset from the first surface. A window frame is provided using this method, as well as an aircraft including the frame.
METHOD FOR MANUFACTURING AN AIRCRAFT WINDOW FRAME COMPRISING SEAMS OFFSET FROM A VISIBLE SURFACE, WINDOW FRAME OBTAINED FROM THIS METHOD AND AIRCRAFT COMPRISING AT LEAST ONE SUCH WINDOW FRAME
2024-06-20
Patent
Electronic Resource
English
European Patent Office | 2024
|European Patent Office | 2024
|European Patent Office | 2024
|