Frame (1) for fuselage shells of an aircraft, the fuselage comprising a skin (3) and stringers (4), the frame (1) comprising:- a plurality of sections (5), the sections (5) being separated by intermediate gaps corresponding to the position of the stringers (4) in the fuselage, each section (5) having a multi-cell configuration constituted by several modular elements (6) of composite material arranged in longitudinal direction, and- a continuous inner cap (7) on top of the sections (5) and the intermediate gaps.
FRAME FOR FUSELAGE SHELLS OF AN AIRCRAFT AND FUSELAGE SHELL
RAHMEN FÜR RUMPFSCHALEN EINES FLUGZEUGS UND RUMPFSCHALE
CADRE POUR COQUES DE FUSELAGE D'UN AÉRONEF ET COQUE DE FUSELAGE
2021-06-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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