A panel for an aircraft wing, having a sandwich structure in which there is arranged a reinforcing part. When the panel is attached to a bracket so as to be articulated to another element, the reinforcing part is provided in order to distribute, over its entire surface, a force transmitted by the bracket to the panel.
PANNEAU DE VOILURE POUR AERONEF
2016-05-06
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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