DEVICE FOR PRODUCING A FUSELAGE SHELL MADE OF FIBER COMPOSITE MATERIAL FOR AN AIRCRAFT

摘要

The invention relates to a device for producing a fuselage shell (14) made of fiber composite material for an aircraft, having a plurality of stringers (7) disposed spaced apart for reinforcement, comprising a main frame (1) for forming a supporting substructure having an outwardly curved mounting surface (2) for positive mounting, having longitudinal mounting grooves (3) for receiving formed parts (5) in a form-fit manner for deformably positioning the stringers (7) relative to the mounting surface (2), wherein a plurality of short formed parts (5) are disposed spaced apart from each other in each mounting groove (3) and adjustable relative to the corresponding mounting groove (3) in the transverse direction (Y) by means of adjusters, and that can be raised in the vertical direction (Z) by means of lifters for guiding the stringers (7) in the direction of a laminating adhesive unit that can be brought over the mounting surface (2).