In a fuselage portion for an aircraft, in order to reduce the assembly clearance between the soleplate (120) of a circumferential frame and a fuselage skin (112) in composite material while limiting the mass of the fuselage portion, a ply drop-off (118) is used comprising two portions (124, 126) oriented in the circumferential direction and having different respective slopes.
Aircraft fuselage portion made of composite material
27.05.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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