Thermosets vs thermoplastics
One of the limitations of composites is the joining of pre-fabricated parts. Thermoplastic composites (TPCs) lend themselves better to joining, but there is always difficulty in ensuring that only the interface is heated without a foreign material left at the bond line. Recent years have seen a renewed interest in TPCs. The predicted production rates for single-aisle aircraft exceed the current economic production capabilities of thermoset composites. Compared to thermosets, TPCs can offer shorter processing times. Thermoset composites must go through a lengthy chemical cure process; TPCs can be processed more rapidly by thermo-forming. This makes TPCs an attractive option, but as yet there has not been a significant uptake for structural applications.
One reason behind this has been joining; TPCs can be joined by fusion bonding (welding), a process that heats the interface under pressure to a temperature above the glass transition temperature, Tg (for amorphous polymers), or the melting point, Tm (for semi-crystalline polymers), forming a welded joint on cooling.
In induction welding, heat is generated through Joule losses from the induced eddy currents. The magnetic field is produced by an alternating electric current passed through a conducting coil. Implants are frequently made of metal, although they can be non-metallic materials such as carbon fibres, or even the carbon fibres in the parent composite materials.
Objective
TWI’s aim was to demonstrate a novel induction welding technique that provides improved control through focused heating of thermoplastic composites.