The use of carbon fibre composites is growing in many sectors but their use remains stronger in very high value industries such as aerospace where the demands of the application more easily justify the high energy input needed and the corresponding costs incurred. This energy and cost input is returned through gains over the whole life of the product, with for example, longer maintenance intervals for an aircraft and lower fuel burn. Thermoplastic composites however have a different energy and cost profile compared to traditional thermosets with notable differences in recyclability, but this profile for thermoplastics is not well quantified or documented. This study considers the key process control parameters and identifies an optimal window for processing thermoplastic composites, along with the effect this has on the final characteristics of the manufactured parts. Interactions between parameters and corresponding sensitivities are extracted from the results.
Keywords:Thermoforming, continuous fibre-reinforced thermoplastic, whole life modelling, composite material recycling-reuse.
* Corresponding author:Tel.: +44 (0) 28 9097 4178; fax: +44 (0) 28 9066 1729.E-mail address: m.price@qub.ac.uk (Mark Price).Page 2 of 24
Introduction
Designing with new materialsThe introduction of new materials, particularly for aerospace products, is not a simple, quick or cheap task. New materials and associated processes require extensive and high cost qualification and must meet challenging manufacturing, strength, stiffness, durability, inspection and maintenance requirements, as well as emerging recycling-reuse targets, obligations and directives. Considering the structural design process, a design is traditionally conceived using experience in combination with highly idealized performance models. This is true for the simplest of components and for the complete vehicle structure. Given commercial pressures for reduced time to market and available data within early design, the ability to fully explore and assess the potential design space is highly constrained. Consequently designs and materials tend to be limited to the most feasible of a few considered, or limited to a known and previously used design and material combination. Moreover, in cases were new materials have been selected, the structural design may not initially maximise the material potential. A good example of this is the introduction of thermosetting composite structures in aerospace which were initially designed as if they were traditional metal materials with isotropic properties. Such design constraints can only be overcome with new understanding and the adoption of new design methods which account for the range of materials, and material to part processes available, as well as the complex interactions between the materials and the ultimate whole life structural performance.In the case of composites this whole life aspect is fundamental in understanding the balance of energy and cost for a product. Each step in the manufacturing process consumes ene...