In a fuselage portion for an aircraft, in order to reduce the assembly clearance between the soleplate of a circumferential frame and a fuselage skin in composite material while limiting the mass of the fuselage portion, a ply drop-off is used comprising two portions oriented in the circumferential direction and having different respective slopes.
Partie de fuselage pour aéronef en matériau composite comprenant des lâchers de plis à faible pente
Aircraft fuselage portion made of composite material including low slope let folds
Rumpfteil für Luftfahrzeug aus Verbundmaterial mit Falten mit niedriger Neigung
2016-06-15
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
PARTIE DE FUSELAGE POUR AERONEF EN MATERIAU COMPOSITE COMPRENANT DES LACHERS DE PLIS A FAIBLE PENTE
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