STRUCTURAL COMPONENT, AIRCRAFT OR SPACECRAFT, AND METHOD

摘要

The present invention provides a structural component (1) for an aircraft or spacecraft (2), comprising: a planar member (3); a reinforcing member (4, 4') which projects (H) from the planar member (3) and is rigidly connected thereto; the reinforcing member (4, 4') comprising at least a foam layer (13) and a cover layer (11), a plurality of pins (16) extending at least through the foam layer (13) and the cover layer (11), and at least the pins (16) and the cover layer (11) comprising a curable matrix.