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
2017-12-22
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
ENSEMBLE STRUCTUREL D'AERONEF ET PROCEDE D'ASSEMBLAGE ASSOCIE
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