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
2015-05-27
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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