Quasi-crystal reinforced multi-element magnesium alloy and preparation method thereof
A magnesium alloy and quasicrystal technology, applied in the field of quasicrystal reinforced magnesium alloy and its preparation, to achieve the effects of high tensile strength, good comprehensive mechanical properties, and improved comprehensive mechanical properties
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Embodiment 1
[0016] Alloy composition (mass percentage): 6.69% Zn, 1.46% Y, 0.14% Ho, 0.12% Er, 0.08% Mn, 0.06% Ti, 0.23% Zr, and the rest is magnesium.
[0017] Put pure Mg in a crucible and heat it, and start to pass CO from 350°C 2 +SF 6 Mix the protective gas, and after the pure magnesium is completely melted, put the pure Zn and Mg-Y, Mg-Ho, Mg-Er, Mg-Mn, Mg-Ti, Mg-Zr master alloys in the pure magnesium melt according to the designed composition ratio. When the alloy melt rises to 760°C, it is stirred for 3 minutes, then refined and left to stand for 10 minutes, and cast into an alloy ingot at 720°C. The alloy ingot was homogenized and annealed at 390°C for 16h, and then hot-extruded at a temperature of 360°C and an extrusion ratio of 81.
[0018] The extruded alloy was aged at 180°C for 16 hours. The tensile strength of the obtained alloy was 395MPa, the yield strength was 353MPa, and the elongation was 24.2%.
[0019] The extruded alloy was aged at 180°C for 20 hours. The tensile...
Embodiment 2
[0021] Alloy composition (mass percentage): 11.42% Zn, 3.13% Y, 0.32% Ho, 0.26% Er, 0.11% Mn, 0.09% Ti, 0.34% Zr, and the rest is magnesium.
[0022] Put pure Mg in a crucible and heat it, and start to pass CO from 350°C 2 +SF 6 Mix the protective gas, and after the pure magnesium is completely melted, put the pure Zn and Mg-Y, Mg-Ho, Mg-Er, Mg-Mn, Mg-Ti, Mg-Zr master alloys in the pure magnesium melt according to the designed composition ratio. When the alloy melt rises to 760°C, it is stirred for 3 minutes, then refined and left to stand for 10 minutes, and cast into an alloy ingot at 720°C. The alloy ingot was homogenized and annealed at 390°C for 16h, and then hot-extruded at a temperature of 360°C and an extrusion ratio of 81.
[0023] The extruded alloy was aged at 175°C for 16 hours. The tensile strength of the obtained alloy was 413MPa, the yield strength was 348MPa, and the elongation was 19.4%.
Embodiment 3
[0025] Alloy composition (mass percentage): 6.82% Zn, 1.38% Y, 0.13% Ho, 0.12% Er, 0.12% Mn, 0.08% Ti, 0.48% Zr, and the rest is magnesium.
[0026] Put pure Mg in a crucible and heat it, and start to pass CO from 350°C 2 +SF 6 Mix the protective gas, and after the pure magnesium is completely melted, put the pure Zn and Mg-Y, Mg-Ho, Mg-Er, Mg-Mn, Mg-Ti, Mg-Zr master alloys in the pure magnesium melt according to the designed composition ratio. When the alloy melt rises to 760°C, it is stirred for 3 minutes, then refined and left to stand for 10 minutes, and cast into an alloy ingot at 720°C. The alloy ingot was homogenized and annealed at 390°C for 16h, and then hot-extruded at a temperature of 360°C and an extrusion ratio of 81.
[0027] The extruded alloy was aged at 180°C for 16 hours. The tensile strength of the obtained alloy was 406MPa, the yield strength was 358MPa, and the elongation was 23.8%.
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