Thermoset Composite Welding (TCW)
UQ Composites was involved in the development of a new technology, which allows the rapid joining of epoxy composite components for applications in commercial aircraft’s primary structures. The process involves the incorporation of a thin thermoplastic film prior to curing of the composite, enabling the subsequent welding of additional components via a common thermoplastic layer.
UQ Composites’ work focused on understanding the complex interfacial mechanisms occurring at a molecular level between the dissimilar materials and developing a simulation tools for predicting the melt flow during the secondary welding stage. The technology is patented by the Cooperative Research Centre for Advanced Composite Structures (CRC-ACS) and was developed in collaboration with Airbus in Toulouse.
Adhesive Bonding of Composites
Damage detection in composite joints assembled through adhesive bonding can be challenging as laminar damage may not be visible. Non-visible damage can be in the form of internal delamination or in some instances due to disbonding or weakly bonded interface (also referred as ‘kissing bonds’).
These damages are currently below the detection limit of conventional non-destructive techniques and cannot be detected. The UQ Composites Group is conducting research on being able to reproduce these ‘kissing bonds’ on a laboratory scale and on the use of non-linear ultrasonic techniques to overcome these issues. In the presence of non-linearity the interaction of ultrasonic and vibrational waves give rise to new frequency components, which can provide information on the laminar damage of composite parts.