B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/12 (2006.01) B64C 1/06 (2006.01)
Patent
CA 2701690
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.
L'invention concerne une structure de fuselage (10) pour fuselage d'aéronef en matériau composite et un aéronef comprenant une telle structure. Le but de l'invention est d'obtenir une structure de fuselage (10) présentant une économie de masse tout en permettant une mise à la masse des systèmes électriques, et de garantir des caractéristiques mécaniques de raideur importantes. Ce but est atteint en utilisant des modules de fixation (20) qui assurent une fonction d'assemblage ainsi qu'une fonction électrique.
Aguera Damien
Gallant Guillaume
Giuseppin Laurent
Airbus Operations
Goudreau Gage Dubuc
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