STRUCTURAL ASSEMBLY FOR AN AIRCRAFT FUSELAGE WITH DOUBLE CURVATURE INCLUDING FRAMES WITH AN OPTIMIZED ORIENTATION

摘要

In order to allow an aircraft fuselage structure to provide optimum resistance to pressurization loads in a fuselage region with a double curvature, the fuselage structure includes a circumferential frame oriented so that the web of the circumferential frame has an orientation close to the local normal to the skin of the fuselage.