Procedure and useful for producing tubular components for aeronautical fuselages

Tubular-shaped component (19) for an aircraft fuselage made of composite materials comprising an outer shell (1) jointless cylindrical shape or frustoconical, a plurality of stiffeners (2) arranged longitudinally within said outer shell (1) and a plurality of anchoring elements (3) further incorporate other elements transversally arranged between said stiffening elements (2). The invention also comprises a tool (18) comprising a support body (12) and a plurality of panels (9) movable between an extended position (10) and a posicionretraida (10 '') in both directions and a process for making such component (19) in which fine stage! the tubular component (19) after shaping and curing is separated from the tool (18) by a longitudinal movement upon displacement of the elements of the tool (18) and in particular Io prevent panelesdesplazables ios (9).