METHOD FOR REINFORCING COMPOSITE STRUCTURES

摘要

A method for creating a structural joint for an aircraft. A first composite component (402) and a second composite component (404) are co-joined to form the structural joint for the aircraft. A hole (628) through the first composite component and the second composite component is created. A composite shear pin (626) is placed through the hole. A composite collar (622) is bonded to the composite shear pin with an adhesive.