SHELL SEGMENT FOR PRODUCING A FUSELAGE CELL SECTION FOR A FUSELAGE CELL OF AN AIRPLANE

摘要

The invention relates to a shell segment (19) for producing a fuselage cell section for a fuselage cell of an airplane, comprising at least one skin field (20) and a plurality of longerons disposed thereon, in particular stringers (21-24), and at least one transverse reinforcement element running substantially transversely to the longerons, in particular at least one frame (26). Because the connection of the at least one transverse reinforcement element to the at least one skin field (20) is established by way of at least one connection bracket (1, 27-29), wherein the at least one connection bracket (1, 27-29) comprises at least one bead (9), the angle brackets required for previously known embodiments of shell segments for absorbing tilting moments of the frames can be eliminated. In this way, it is possible to considerably lower the weight, and also reduce the manufacturing complexity.