Aluminum alloy with high heat stability and fatigue resistance and heat treatment technology
A thermal stability and anti-fatigue technology, which is applied in the field of aluminum alloy and heat treatment process, can solve the problems of low elongation, inability to achieve thermal stability and fatigue performance of structural properties, and inability to reach high temperature conditions of 200°C, and achieve thermal stability Improvement of resistance and fatigue performance, satisfying high strength and thermal stability, and excellent strengthening effect
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Embodiment 1(T8
[0045] The alloy composition is: 4.10%Cu, 1.27%Mg, 0.47%Mn, 0.10%Ti, 0.2%Ni, 0.5%Fe, 0.5%Si, and the balance is Al at 490°C for 12 hours for homogenization After chemical treatment, the ingot was extruded into a material at 410°C with an extrusion ratio of 27, then solidified at 505°C for 1 hour and quenched in water, with a pre-stretch deformation of 4%, and aged at 185°C for 2 hours. The tensile mechanical properties at room temperature reach: the tensile strength is 555MPa, the yield strength is 472MPa, and the elongation is 14%. The elongation rate is 10%. Under the alternating load of 280MPa stress level and stress ratio of 0.1, the number of fatigue cycles reaches 1.25×10 7 .
Embodiment 2(T8
[0047] The alloy composition is: 3.80%Cu, 1.80%Mg, 0.90%Mn, 0.15%Ti, 0.10%Ni, 0.70%Fe, 0.70%Si, and the balance is Al at 460°C for 36 hours for uniform After chemical treatment, the ingot was extruded into a material at 380°C with an extrusion ratio of 20, then solidified at 510°C for 0.5 hour and water quenched, 4% pre-stretch deformation was applied, and then aged at 150°C for 12 hours The final mechanical properties reach: the tensile strength is 541MPa, the yield strength is 437MPa, and the elongation is 16%. The rate is 13%. Under the alternating load of 350MPa stress level and stress ratio of 0.1, the fatigue cycle reaches 5.0×10 5 .
Embodiment 3(T8
[0049] The alloy composition is: 4.90%Cu, 1.20%Mg, 0.30%Mn, 0.05%Ti, 0.35%Ni, 0.30%Fe, 0.30%Si, the balance is Al alloy ingot at 475℃ for 24 hours for uniform After chemical treatment, the ingot was extruded into a material at 360°C with an extrusion ratio of 27, then solidified at 515°C for 50 minutes and water quenched, 8% pre-stretch deformation was applied, and then aged at 120°C for 20 hours The final mechanical properties reach: the tensile strength is 542MPa, the yield strength is 463MPa, and the elongation is 15%. The rate is 9%. Under the alternating load of 280MPa stress level and stress ratio of 0.1, the number of fatigue cycles reaches 1.0×10 7 .
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