TUBULAR COMPONENTS FOR FUSELAGES AND METHODS AND TOOLS FOR PRODUCING SAME

摘要

The invention relates to a tubular component (19) for a fuselage, which is made from composite materials and comprises a cylindrical or truncated-cone-shaped seamless outer casing (1), a plurality of stiffening elements (2) disposed longitudinally inside the outer casing (1) and a plurality of elements (3) for anchoring other elements to be incorporated later, which are disposed transversely between the stiffening elements (2). The invention also relates to a tool (18) comprising a supporting body (12) and a plurality of panels (9) that can be moved in both directions between an extended position (10) and a retracted position (10'). The invention further relates to a method for producing the above-mentioned component (19), including a final step in which the formed and cured tubular component (19) is separated from the tool (18) by means of a longitudinal movement after the obstructing elements of the tool (18) have been moved, in particular the movable panels (9).