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Influence of Hot Rolling on Mechanical Behavior and Strengthening Mechanism in Boron Carbide Reinforced Aluminum Matrix Composites

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TMS 2018 147th Annual Meeting & Exhibition Supplemental Proceedings (TMS 2018)

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Abstract

Boron carbide reinforced aluminum matrix composites are widely used as neutron absorption materials. Here we report that mechanical alloying has been successfully employed to synthesize metal matrix composite powders with Al as the matrix and B4C, Al4Gd and Al4Sm as the reinforcement. The effects of hot rolling on the morphology, mechanical properties as well as the strengthening mechanisms are investigated. Hot rolling results in improving particle distribution and less agglomeration, improving the bonding between particles and matrix and decreasing voids. Thermomechanical processing can increase the density and remove the defects. As increasing rolling deformation to 50%, both YS and UTS of composites are enhanced significantly, showing 25.8 and 27.0% improvement in comparison with composites after sintered, but the elongation changes little. The increase in the yield strength after hot rolling can be attributed to two primary strengthening mechanisms in this work: The coefficient of thermal expansion (CTE) mismatch between B4C, Al4Gd and Al4Sm reinforced particles and Al matrix and the existence of load transfer from Al matrix to the hard reinforced particles.

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Acknowledgements

This work was supported by the NSFC Funding (51371062 and U1460102), NSFHLJ (ZD201411). Hao Guo is benefited from the International Exchange Program of Harbin Engineering University for Innovation-oriented Talents Cultivation.

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Correspondence to ZhongWu Zhang .

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Guo, H. et al. (2018). Influence of Hot Rolling on Mechanical Behavior and Strengthening Mechanism in Boron Carbide Reinforced Aluminum Matrix Composites. In: & Materials Society, T. (eds) TMS 2018 147th Annual Meeting & Exhibition Supplemental Proceedings. TMS 2018. The Minerals, Metals & Materials Series. Springer, Cham. https://doi.org/10.1007/978-3-319-72526-0_81

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