A reinforced composite laminate for an aircraft and a method of manufacture thereof. The laminate includes a set of stacked plies of pre-preg material laid up forming an XY plane, wherein the laminate further includes a plurality of elongated carbon pins including a round section with a diameter smaller than 0.5 mm. The pins are nailed through the stacked plies following the Z direction to withstand the out-of-plane loads.
REINFORCED COMPOSITE LAMINATE AND METHOD FOR MANUFACTURING THEREOF
2022-06-16
Patent
Electronic Resource
English
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