4.6 Article

Hot Tensile Deformation Mechanism and Fracture Behavior of the ZW31/PMMC Laminate

Journal

MATERIALS
Volume 16, Issue 23, Pages -

Publisher

MDPI
DOI: 10.3390/ma16237446

Keywords

laminate; hot deformation mechanism; hot tensile fracture mechanism

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In this study, a Mg-Zn-Y alloy (ZW31) with good plasticity was introduced into SiCp/AZ91 composite materials via the extrusion compound method, and the ZW31/PMMC laminate was prepared through hot rolling. The high temperature deformation mechanism and tensile fracture mechanism of ZW31/PMMC laminates were studied.
In this work, a Mg-Zn-Y (ZW31) alloy with good plasticity was introduced into 10 mu m 10 vol% SiCp/AZ91 composite materials (PMMCs) via the extrusion compound method, and then the ZW31/PMMC laminate was prepared via multi-pass hot rolling. The hot deformation mechanism and elevated temperature tensile fracture mechanism of ZW31/PMMC laminates were studied using the elevated temperature tensile test. The elevated temperature deformation mechanism is influenced by the strain rate. At low strain rates, grain boundary slip is the primary elevated temperature deformation mechanism of the ZW31/PMMC laminate. However, at high strain rates, the activation of pipeline diffusion is facilitated by the particle deformation zone (PDZ) in the PMMC layer with a high dislocation density, leading to the dominance of dislocation climbing as the main mechanism for elevated temperature deformation of the laminate. Additionally, the implementation of a ZW31/PMMC laminate structure effectively inhibits the initiation and propagation of cavities and microcracks within the laminate layer along the normal direction (ND) while simultaneously blunting crack tips via lattice dislocation emission toward the ZW31 layer. Upon cracking of the PMMC layer, stress concentration occurs in the fracture area of the ZW31 layer, ultimately resulting in necking-induced detachment.

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