<p>The influence of heat treatment on the microstructure, phase evolution, mechanical properties, and fractography of Mg Elektron675 (E675) was thoroughly examined. The solid solution strengthening (T4 condition) at 525&#xa0;°C for 12&#xa0;hours dissolves rare-earth elements (REE) into the Mg matrix. After solutionizing, residual phases dissolve into the Mg matrix, with no significant grain growth observed. Results showed that aging (T6) at 225&#xa0;°C for 8, 12, 24, and 80&#xa0;hours leads to phase evolution of <i>α</i>-Mg, Mg<sub>5</sub>Gd, and Mg<sub>24</sub>Y<sub>5</sub>. During aging (T6), grains coarsen up to 54.8 ± 8 μm, and mechanical performance improves, indicating long-term heat treatment and precipitate hardening effects. Under all heat-treated conditions, high-angle grain boundaries have a greater impact on increasing yield strength than low-angle boundaries. Aging (T6) significantly enhances hardness from 119.3 HV0.05 to 153.1 HV0.05 and improves tensile properties. The alloy exhibits higher strength at T6-225&#xa0;°C for 80&#xa0;hours, with an ultimate tensile strength of 187.25 ± 6.17 MPa, yield strength of 163.3 ± 5.4 MPa, and ductility of 1.6 ± 0.5%. The alloy displays a mixed fracture mode at 8 and 12&#xa0;hours early in aging. The transition to brittle fracture occurs around 24&#xa0;hours of aging (T6), characterized by cleavage planes, fewer dimples, and tear ridges.</p> Graphical Abstract <p></p>

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Effects of Thermal Aging on Mechanical Properties and Microstructure Characteristics of Mg E675 Alloy

  • R. Suruthi Devi,
  • A. Raja Annamalai

摘要

The influence of heat treatment on the microstructure, phase evolution, mechanical properties, and fractography of Mg Elektron675 (E675) was thoroughly examined. The solid solution strengthening (T4 condition) at 525 °C for 12 hours dissolves rare-earth elements (REE) into the Mg matrix. After solutionizing, residual phases dissolve into the Mg matrix, with no significant grain growth observed. Results showed that aging (T6) at 225 °C for 8, 12, 24, and 80 hours leads to phase evolution of α-Mg, Mg5Gd, and Mg24Y5. During aging (T6), grains coarsen up to 54.8 ± 8 μm, and mechanical performance improves, indicating long-term heat treatment and precipitate hardening effects. Under all heat-treated conditions, high-angle grain boundaries have a greater impact on increasing yield strength than low-angle boundaries. Aging (T6) significantly enhances hardness from 119.3 HV0.05 to 153.1 HV0.05 and improves tensile properties. The alloy exhibits higher strength at T6-225 °C for 80 hours, with an ultimate tensile strength of 187.25 ± 6.17 MPa, yield strength of 163.3 ± 5.4 MPa, and ductility of 1.6 ± 0.5%. The alloy displays a mixed fracture mode at 8 and 12 hours early in aging. The transition to brittle fracture occurs around 24 hours of aging (T6), characterized by cleavage planes, fewer dimples, and tear ridges.

Graphical Abstract