An open composite panel for an aircraft includes a composite skin having an inner face and an outer face, and a plurality of stiffening ribs, each rib extending over the inner face of the skin in a respective direction of extension and projecting from the inner face to a top that is opposite said inner face. The plurality of ribs includes at least one reinforced rib, each reinforced rib having at least one elongate stiffening portion extending along the top of the reinforced rib, said stiffening portion including fibers extending substantially in the direction of extension of the reinforced rib.
PANNEAU COMPOSITE OUVERT RIGIDE
RIGID OPEN COMPOSITE PANEL
STARRE OFFENE VERBUNDPLATTE
25.09.2024
Patent
Elektronische Ressource
Französisch
DISPOSITIF DE MANUTENTION D'UN PANNEAU RIGIDE ET PROCÉDÉ DE MANUTENTION UTILISANT UN TEL DISPOSITIF
Europäisches Patentamt | 2020
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