Host Institution: University of Southampton
Lead Investigator: Janice Barton
Co-Investigator: Daniel Bull, Ian Sinclair, Ole Thomsen
To save time and reduce wastage it was essential that an inspection technology was developed that can be used to intervene at the manufacturing stage and provide high fidelity data for model based prognostic capability (beyond simply sizing defects) to further inform the decision process of ‘accept’, ‘rework’, ‘repair’ or ‘scrap’. To this end a novel inspection procedure for cured composite components needed to be developed, and the overarching aim of the project was a system deployed alongside current inspection approaches in the production environment. This procedure has the ability to simultaneously measure the strain and a stress measure in the vicinity of a manufacturing defect or intrinsic subsurface artefact (including the variability of fibre volume fraction and fibre orientation, not just the geometry and size), and provide high fidelity data to inform model-based prognostics, and define how a given defect will evolve under service load.
The objectives of the of the feasibility study were:
The feasibility study is completed. It has been fully demonstrated that DIC and TSA can be used simultaneously to collect data from composite components. The approach has been demonstrated on a high value carbon fibre aircraft component and shown that the results can be linked to the findings of high fidelity prognostic models, with defect geometry defined by X-ray CT.
The approach has also been demonstrated on materials typical of those used in high volume manufacturing made from carbon fibre/epoxy discontinuous compression moulded preforms. The work has linked observations from X-ray CT to the mechanical response and the combination of DIC and TSA for assessment of the material has shown great promise. In particular it is possible to predict the localised stiffness variations, linked to local variability of fibre volume fraction and fibre orientation, throughout the preform. As a result, the manufacturing control process can be directly informed/updated using the technique. It has also been demonstrated that the technique can be protable (i.e. no need for a test machine to load the components) by exciting the component briefly at its resonant frequency.
The PhD study focused on developing a low cost infra-red camera for TSA. The work has revealed scientific challenges in developing the technology further, and provided steps in developing signal processing routines that have addressed these challenges.
Fully integrated DIC and TSA: the key challenge was in collecting the data simultaneously. This was done by using lock-in processing for the DIC. Although the technique was developed at University of Southampton previously, the key challenge was deploying this on a realistic component.
The strain measurements from the DIC and the thermoelastic response, which is dependent on the local fibre orientations and fibre volume fractions have provided a strong indication of identification of stiffness distribution and resin-rich volumes. Initial demonstration of vibration based technique on panels.
Through the feasibility study, technology was developed which provided practical demonstrations based on a realistic high volume manufactured and high value manufactured components loaded either naturally or by excitation at their resonant frequency. There was a focus towards manufacturing of composite components both high value and high volume and an aim to develop the study into a Core Project.