Method for reducing quenching residual stress of 7000 series aluminum alloy thick sheet and aluminum alloy sheet
A residual stress and aluminum alloy technology, which is applied to a method of reducing the residual stress of 7000 series aluminum alloy thick plate quenching and the field of aluminum alloy sheet, can solve the problem of weakening, excavation and optimization without considering the mechanical properties of aluminum alloy thick plate at the same time, etc. problems, to achieve the effect of reducing residual stress, improving mechanical properties, and simple process
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Embodiment 1
[0030] A method for reducing quenching residual stress of 7000 series aluminum alloy thick plate, comprising the following steps:
[0031] (1) After smelting and rolling the 7050 aluminum alloy, it is subjected to solution treatment at 470°C for 30 minutes;
[0032] (2) Intermittently cooling the 7050 aluminum alloy plate obtained in step (1), the first cooling rate is 25°C / s, cooled to 120°C, and then cooled to room temperature at a cooling rate of 2°C / min;
[0033] (3) Perform 0.2% pre-strain treatment and pre-aging treatment at 120°C for 10 minutes;
[0034] (4) Carry out 0.2% secondary pre-strain treatment, and artificial aging treatment at 160°C for 8h.
[0035] figure 2 is the final TEM fine structure map of 7050 aluminum alloy, by figure 2 It can be seen that the structure treated by the present invention has a high density of precipitated phases in the crystal, and the yield strength and tensile strength reach 625MPa and 690MPa respectively, as shown in Table 1. ...
Embodiment 2
[0037] A method for reducing quenching residual stress of 7000 series aluminum alloy thick plate, comprising the following steps:
[0038] (1) After smelting and rolling the 7055 aluminum alloy, it is subjected to solution treatment at 460°C for 45 minutes;
[0039] (2) Intermittently cooling the 7055 aluminum alloy thick plate obtained in step (1), the first cooling rate is 30°C / s, cooled to 100°C, and then cooled to room temperature at a cooling rate of 1°C / min;
[0040] (3) Perform 0.3% pre-strain treatment and pre-aging treatment at 100°C for 40 minutes;
[0041] (4) Carry out 0.2% secondary pre-strain treatment, and artificial aging treatment at 180°C for 6h.
[0042] image 3 is the final TEM fine structure map of 7050 aluminum alloy, by image 3 It can be seen that the structure treated by the present invention has a high density of precipitated phases in the crystal, and the yield strength and tensile strength reach 675MPa and 715MPa respectively, as shown in Table ...
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