Apparatus for the production of an aircraft fuselage shell consisting of a fibre composite

An apparatus for the production of a fuselage shell for an aircraft consisting of a fiber composite, which is to be equipped with a plurality of stringers disposed spaced apart for reinforcement, comprising:

• a main frame forming a supporting sub-structure having an outwardly curved mounting surface for positive mounting having a plurality of longitudinal mounting grooves for receiving of a plurality of formed parts in a form-fit manner for deformably positioning the stringers relative to the mounting surface,
• wherein a plurality of short formed parts are disposed spaced apart from each other in each mounting groove;
• wherein the stringers are adjustable by an adjuster relative to the corresponding mounting groove in the transverse direction (Y) defined from a first side of the groove to a second side of the groove, and configured to be moved in the vertical direction (Z) in or out of the groove by at least first and second lifters for guiding the stringers in the direction of a laminating adhesive bonding unit brought over the mounting surface.