Multiple thermal fatigue resistance zinc-base alloy
A heat-resistant and fatigue-resistant technology, which is applied in the field of zinc-aluminum alloy materials, can solve the problems that the thermal fatigue problem has not been completely solved, the quantitative research on thermal fatigue of zinc-based alloys is backward, and the thermal fatigue of zinc-based alloys is not very comprehensive.
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Embodiment 1
[0009] The zinc-aluminum alloy composition is selected as (No. 1 sample), Si: 2.5%, RE: 0.1%, Ni-Ti (Ni50%, Ti50%): 0.1%, Cr: 0.1%, Al: 40%, Cu: 2.0 %, Mg: 0.01%, and the balance is Zn. The smelting process is as follows: first add aluminum ingots, aluminum-copper master alloys, aluminum-chromium master alloys, zinc ingots and an appropriate amount of Si and Ni-Ti alloys to the induction melting electric furnace. After complete melting, fully stir, add an appropriate amount of RE, and Keep warm for 5 minutes at 700-750°C to homogenize each element, and then use a bell jar to press the magnesium strips to reduce the burning loss rate. Use 0.2% zinc alloy degassing refining agent for degassing and refining, let it stand for 10 minutes, remove the slag, pour it when the temperature is 650-670°C, and then make it as figure 1 The sample shown.
[0010] The thermal fatigue test was carried out using a resistance furnace heating self-constraining thermal fatigue testing machine. T...
Embodiment 2
[0012] The zinc-aluminum alloy composition is selected as (No. 2 sample), Si: 3.5%, RE: 0.27%, Ni-Ti (Ni50%, Ti50%): 0.2%, Cr: 0.2%, Al: 46%, Cu: 3.0 %, Mg: 0.02%, and the balance is Zn. Melting process and thermal fatigue test are the same as embodiment 1, and the test results are shown in Table 1 and figure 2 .
Embodiment 3
[0014] The zinc-aluminum alloy composition is selected as (No. 3 sample), Si: 3.0%, RE: 0.2%, Ni-Ti (Ni50%, Ti50%): 0.15%, Cr: 0.15%, Al: 43%, Cu: 2.5 %, Mg: 0.015%, and the balance is Zn. Melting process and thermal fatigue test are the same as embodiment 1, and the test results are shown in Table 1 and figure 2 .
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