A frame (1) for fuselage shells of an aircraft, the fuselage comprising a skin (3) and stringers (4), the frame (1) including: 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
09.04.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
FRAME FOR FUSELAGE SHELLS OF AN AIRCRAFT AND FUSELAGE SHELL
Europäisches Patentamt | 2021
|Frame for fuselage shells of an aircraft and fuselage shell
Europäisches Patentamt | 2022
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