FUSELAGE STRUCTURE FOR AIRCRAFT FUSELAGE MADE OF COMPOSITE MATERIAL AND AIRCRAFT EQUIPPED WITH SUCH FUSELAGE STRUCTURE

摘要

The invention relates to a fuselage structure (10) for an aircraft fuselage made of a composite material, and to an aircraft including such a structure. The purpose of the invention is to obtain a fuselage structure (10) having a reduced mass while allowing for the grounding of the electrical systems, and to provide high mechanical stiffness characteristics. The aim can be achieved by using fastening modules (20) that provide an assembling function and an electrical function.