Strength characterization of caryota urens fibre and aluminium 2024-T3 foil multi-stacking sequenced SiC-toughened epoxy structural composite

Biomass Conversion and Biorefinery - Tập 12 - Trang 4009-4019 - 2020
V. Antony Vincent1, C. Kailasanathan2, V. K. Shanmuganathan3, J. V. Sai Prasanna Kumar4, V. R. Arun Prakash3
1Department of Aeronautical Engineering, Noorul Islam Centre for Higher Education, Kumarakovil, India
2Department of Mechanical Engineering, Sethu Institute of Technology, Virudhunagar, India
3Department of Mechanical Engineering, J. N. N Institute of Engineering, Tiruvallur, India
4Department of Aeronautical Engineering, Veltech Dr. Rangarajan Dr. Sagunthala R&D Institute of Science and Technology, Chennai, India

Tóm tắt

High toughness and high-impact damage resistance fibre-metal hybrid laminate epoxy composites were prepared and characterized. In this present research, a hybrid fibre-metal laminate was reinforced into SiC-toughened epoxy resin for making high performance structural material for automobile and aircraft applications. Novel natural fibre caryota urens and silicon carbide (SiC) particles were surface-treated using 3-aminopropyltriethoxysilane (APTES) whereas the aluminium foil was sandblasted. The hybrid fibre-metal laminate with different stacking sequenced epoxy composites were prepared using vacuum bag moulding followed by post curing. A highest strength factor of 97 is observed for composite designation CAC1, which contains 0.5 vol.% of SiC. The drop load impact toughness of ACA1 composite gives the highest energy absorption of 20.6 J. Similarly, the CAC1 composite designation gives fracture toughness of 32.1 MPa. $$ \sqrt{\mathrm{m}} $$ and energy release rate of 1.557 mJ/m2. The scanning electron microscope images revealed highly reacted phase of surface-treated reinforcements with epoxy resin matrix.

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