Abstract
Interlaminar delamination is the most prevalent failure mode for carbon fiber reinforced epoxy (CF/EP) composites, which limits its applications. In this work, the interlaminar fracture toughness of CF/EP composites has been enhanced by the self-interlocked network arisen from Ti3C2Tx/polyvinyl alcohol (PVA) aerogel (TPA). The failure mode and toughening mechanism of interlocked TPA/CF/EP laminates has been explored from crack path behaviour and fracture morphology. The results show that the surface-modified MXene effectively improved the mechanical properties of TPA aerogels. The optimized loading of Ti3C2TX (7.69 wt%) and TPA areal density (27 g/mm2) can significantly enhance the GIC Init, GIC Prop and GIIC by 76%, 40% and 32%, respectively, without appreciably reducing the in-plane mechanical properties. The enhanced fracture toughness can be ascribed to cohesive failure at the interface facilitated by stitching-like effect of TPA, deflection and twisting of the main crack, the generation of numerous microcracks and pull-out of TPA skeleton and Ti3C2Tx, etc. Compared with the traditional interleave toughening, interlocked TPA not only achieves a comprehensive balanced mechanical enhancement of CF/EP laminates, but also avoids the toxicity of organic solvents.
| Original language | English |
|---|---|
| Pages (from-to) | 60-70 |
| Number of pages | 11 |
| Journal | Carbon |
| Volume | 201 |
| DOIs | |
| Publication status | Published - 5 Jan 2023 |
Keywords
- Carbon fibres
- Cohesive failure
- Hybrid composites
- Interlaminar fracture toughness
- Synergism
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