PROCEDE DE FABRICATION D'UN TRONCON DE FUSELAGE D'AERONEF EN MATERIAU COMPOSITE

摘要

The disclosed embodiments relate to a method for manufacturing an aircraft fuselage section of composite material that comprises the following operations manufacturing a one-piece section; cutting the section longitudinally; spreading apart two edges located on the two sides of the cut; reassembling the section and making a longitudinal joint with the two edges overlapping. The disclosed embodiments also relate to a section made in accordance with this method.