As advanced composite structures become larger and more complex, there is a corresponding need to improve methods of joining and assembly. Current methods of joining composite materials for aerospace applications, that is, adhesive bonding and mechanical fastening, present some design and manufacturing limitations. The mechanical fastening method cannot be effectively applied to composite structures because of stress concentration, the effects of drilling on the structural integrity, and localized delamination. Poor bonding properties between adhesives and polymers make the adhesive bonding methods less desirable for most structural applications. The fact that thermoplastic materials can be remelted provides the opportunity of welding (or fusion bonding) of thermoplastic composite parts as an alternative to joining and assembly. Fusion bonding, in principle, consists of surface preparation, heating the polymer at the weld interface to a viscous state, physically causing polymer chains to interdiffuse across the interface, and cooling the polymer for consolidation. The polymer chains are intertwined across the interface during the welding process, resulting in disappearance of the bonded surface and improving the ability of transferring loads through the welded area. The quality of the welded parts is usually compared to that of autoclave consolidated or compression molded parts.