Interlaminar properties of carbon fibre/epoxy laminates produced through a semi-curing process
The performance of semi-cured laminate interfaces with degrees of cure ranging from 0.3 to 0.9 was explored in Mode I and II, and compared to a baseline laminate produced through a single infusion and cure. The results showed that if the initially semi-cured element is kept to a degree of cure below the gel point prior to integration with the rest of the structure, average Mode I properties are retained to within 10 % of the baseline. At degrees of semi-cure above the gel point, a 33 % reduction in Mode I was measured, however, plasma pre-treatment mitigated this reduction to only 11 %. In Mode II, interlaminar properties are fully retained. Over the wide range of semi-cure studied, both resin flow and chemical cross-linking were observed, with the latter viewed as being more important when seeking to retain interfacial properties. The semi-curing process is considered a viable manufacturing method to produce composite laminates by resin infusion.
Authors
- Arjun Radhakrishnan (ORCID: https://orcid.org/0000-0002-1778-0715)
- James Kratz (ORCID: https://orcid.org/0000-0002-9060-2878)
- Turlough McMahon
- Robin Hartley (ORCID: https://orcid.org/0000-0003-0983-4282)
- Mark Mavrogordato (ORCID: https://orcid.org/0000-0002-3956-2866)
- Michael O’Leary
Institutions
- University of Bristol (GB)
- National Composites Centre (GB)
- University of Southampton (GB)
- Airbus (United Kingdom) (GB)
Publication Details
- Journal
- Composites Part A Applied Science and Manufacturing
- Published
- 2024-09-23
- DOI
- https://doi.org/10.1016/j.compositesa.2024.108488
- Citations
- 4
- Primary Topic
- Epoxy Resin Curing Processes
- Type
- article
- Field-Weighted Citation Impact
- 0.85
Funders
- Engineering and Physical Sciences Research Council