Effect of extrusion temperature on microstructure and mechanical properties of ZTM631 magnesium alloy

Magnesium alloys are widely used in the fields of aviation, electronics, and automotive manufacturing due to their advantages of lightweight and high specific strength. Studying high-performance and low-cost deformed magnesium alloys to adapt to more application scenarios has important value. In the present work, the effect of extrusion temperature on the microstructure and mechanical properties of Mg-6Zn-3Sn-0.9Mn (ZTM631) alloy was investigated. Besides, the ultra -high cycle fatigue (VHCF) performance and fatigue failure mechanism of ZTM631 alloy was explored. Results show that extrusion temperature significantly affect the microstructure of ZTM631 alloys. Firstly, alloys extruded at 300 degrees C possess a relatively fine grain size, because the lower extrusion temperature prevent the grain growth. Secondly, phases precipitate at 300 degrees C and 350 degrees C with a large size (more than 1 mu m) are mainly alpha-Mn phase. while for the alloys extruded at 400 degrees C, both alpha-Mn and Mg 2 Sn phases with the size larger than 1 mu m can be found in the matrix. Thirdly, alloys extruded at 400 degrees C exhibit the best mechanical properties, due to the combination of the grain refinement and precipitation strengthening. Fourthly, during the VHCF failure process, the crack preferentially generates at the densely distributed alpha-Mn phases for the alloy extruded at 300 degrees C and 350 degrees C, while the crack initiate near the Mg 2 Sn particles for the alloy extruded at 400 degrees C. Also, undynamic recrystallized (un-DRXed) grains with severe deformation exist in the alloys extruded at 300 degrees C and 350 degrees C, thus accelerating the crack initiation. This fundamental investigation provides theoretical information for developing high-performance Mg-Zn-Sn alloys with high strength and expanded their application fields.