Component manufacturing method for e.g. aircraft, involves impregnating added reinforcement fibers with polymer matrix for forming component from elements, where reinforcement fibers are disrupted along parting plane

摘要

The method involves impregnating reinforcement fibers (10) of an element e.g. stringer, partially with a polymer matrix, where the reinforcement fibers include continuous fibers that are provided as multi-ply fabric and braided fabric or knitted fabric. The added reinforcement fibers are impregnated with another polymer matrix for forming a component from the element and another element, where the former component is made of a composite material. The reinforcement fibers are disrupted along a parting plane or cutting parting planes. An independent claim is also included for an element comprising an adding region.