A METHOD OF REINFORCING A LAMINATED MEMBER SUCH AS A SKIN FOR AN AIRCRAFT

摘要

A method of reinforcing a laminated wing skin (10) for an aircraft. The method comprises laying-up a plurality of fibres to form the laminated wing skin (10). A composite reinforcement member (14) is positioned on a surface (16) of the laminated skin (10) and one or more further layers are laid up so as to enclose the composite reinforcing member (14) at a position adjacent one surface of the laminated skin (10).