Neale, GeoffreySaaran, VinodhenDahale, MonaliSkordos, Alexandros A.2024-03-272024-03-272024-03-24Neale G, Saaran V, Dahale M, Skordos AA. (2024) An evaluation of large diameter through-thickness metallic pins in composites, Composite Structures, Volume 337, June 2024, Article Number 1180660263-8223https://doi.org/10.1016/j.compstruct.2024.118066https://dspace.lib.cranfield.ac.uk/handle/1826/21093There is increasing demand for functional through-thickness reinforcement (TTR) in composites using elements whose geometry exceeds limitations of existing TTR methods like tufting, stitching, and z-pinning. Recently, static insertion of large diameter TTR pins into heated prepreg stacks has proven a feasible and robust reinforcement process capable of providing accurate TTR element placement with low insertion forces and lower tow damage compared with existing methods for similar element sizes (>1mm diameter) like post-cure drilling. Local mechanical performance and failure mechanics of these pinned laminates are reported here. Laminates with a single statically inserted pins (1.2, 1.5, and 2.0 mm) can mostly retain their in-plane integrity alongside a local improvement in mode I delamination toughness in carbon fibre-benzoxazine laminates. Tensile strength is mostly unaffected by the pins resulting from delamination suppression, whereas there is up to a doubling of Young’s modulus. Compressive strength is significantly diminished (up to 42 %) in pinned laminates. Interlaminar toughness is improved, and peak toughness is pushed ahead of the crack as pin diameter increases. The lack of significant deterioration in in-plane tensile properties in pinned laminates produced using static insertion can expand the range and forms of materials that can be inserted compared to existing TTR.en-UKAttribution 4.0 Internationalhttp://creativecommons.org/licenses/by/4.0/Through-thickness reinforcementCarbon fibreBenzoxazineDamage mechanicsFinite element analysis (FEA)An evaluation of large diameter through-thickness metallic pins in compositesArticle1879-1085