Two-stage solid solution heat treatment method of copper chromium zirconium system alloy
A heat treatment method, two-stage solid solution technology, applied in the field of high-strength and high-conductivity copper-chromium-zirconium alloy system, two-stage solution heat treatment, can solve problems such as difficulty in obtaining supersaturated solid solution
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Embodiment 1
[0031] The alloy compositions used in the present invention are shown in Example 1 in Table 1.
[0032] (1) Processing technology: hot extrusion, extruded from Φ45mm to Φ10mm, and the processing deformation is 95%.
[0033] (2) The first stage solid solution process: heat preservation at 940°C for 12h, and then quench.
[0034] (3) Second-stage solid solution process: heat preservation at 1010°C for 1 hour, and then quench.
[0035] (4) Comparative alloy solid solution process: heat preservation at 950°C for 1h, and then quench.
[0036] (5) Subsequent processing and aging process: direct aging, heat preservation at 450°C for 3 hours, and air cooling.
[0037] After the above-mentioned deformation heat treatment process, the comprehensive performance test results of the test alloy and the comparison alloy are shown in Example 1 in Table 2.
Embodiment 2
[0039] The alloy composition used in the present invention is shown in Example 2 in Table 1.
[0040] (1) Processing technology: hot rolling, rolling from thickness 100mm to 18mm, reduction 82%.
[0041] (2) The first stage solid solution process: heat preservation at 945°C for 24h, and then quench.
[0042] (3) Second-stage solid solution process: 1040°C heat preservation for 1.5h, quenching.
[0043] (4) Comparative alloy solid solution process: heat preservation at 1010°C for 0.5h, and quench.
[0044] (5) Subsequent processing and aging process: direct aging, heat preservation at 460°C for 4 hours, and air cooling.
[0045] After the above-mentioned deformation heat treatment process, the comprehensive performance test results of the test alloy and the comparison alloy are shown in Example 2 in Table 2.
Embodiment 3
[0047] The alloy composition used in the present invention is shown in Example 3 in Table 1.
[0048] (1) Processing technology: hot extrusion, extrusion from Φ45mm to Φ10mm, deformation 95%.
[0049] (2) The first-stage solid solution process: heat preservation at 915°C for 10 hours, and then quench.
[0050] (3) Second-stage solid solution process: heat preservation at 990°C for 1 hour, and then quench.
[0051] (4) Comparative alloy solid solution process: heat preservation at 940°C for 1h, and then quench.
[0052] (5) Subsequent processing and aging process: direct aging, heat preservation at 440°C for 3 hours, and air cooling.
[0053] After the above-mentioned deformation heat treatment process, the comprehensive performance test results of the test alloy and the comparison alloy are shown in Example 3 in Table 2.
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