In order to allow an aircraft fuselage structure to provide optimum resistance to pressurization loads in a fuselage region with a double curvature, the fuselage structure includes a circumferential frame oriented so that the web of the circumferential frame has an orientation close to the local normal to the skin of the fuselage.
ENSEMBLE STRUCTUREL POUR FUSELAGE D'AERONEF A DOUBLE COURBURE COMPRENANT DES CADRES A ORIENTATION OPTIMISEE
22.12.2017
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
ENSEMBLE STRUCTUREL D'AERONEF ET PROCEDE D'ASSEMBLAGE ASSOCIE
Europäisches Patentamt | 2018
|Ensemble propulsif pour arrière de fuselage d’aéronef
Europäisches Patentamt | 2025
|Europäisches Patentamt | 2025
|Europäisches Patentamt | 2025
|Europäisches Patentamt | 2016
|