A ferrite-based high-strength corrosion-resistant dual-phase alloy and its preparation method
A dual-phase alloy and ferrite technology, which is applied in the field of high-temperature alloy steel, can solve the problem that it is difficult to meet the high-temperature strength of the alloy hot-end parts of the unit, the resistance to steam oxidation and corrosion, the corrosion resistance and oxidation resistance cannot be effectively guaranteed, The problems such as the decline of the peak-shaving operation ability of the boiler to achieve the effect of promoting carbide growth, excellent strength performance, and improved dispersion and precipitation
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Embodiment 1
[0037] The high-strength corrosion-resistant alloy material of this embodiment includes, by mass percentage: C: 0.08%, B: 0.005%, Cr: 18%, Ni: 8%, Co: 0.5%, Mn: 10%, Si: 0.4%, Nb: 0.5%, Mo: 0.5%, W: 1.0%, Ti: 1.4%, Al: 1.2%, and the balance is Fe.
[0038] The preparation method of this embodiment comprises the following steps:
[0039]1) Raw material preparation: The ingredients include by mass percentage: C: 0.08%, B: 0.005%, Cr: 18%, Ni: 8%, Co: 0.5%, Mn: 10%, Si: 0.4%, Nb: 0.5% , Mo: 0.5%, W: 1.0%, Ti: 1.4%, Al: 1.2%, and the balance is Fe.
[0040] 2) Smelting and forming: The alloy is smelted by vacuum, and the pouring temperature of the alloy is controlled to be 1600 ℃. After completion, the ingot was homogenized at 1000°C for 16h. The alloy is processed and deformed by hot rolling, the rolling temperature is 1000 °C, the final rolling temperature is 700 °C, and the deformation amount in a single pass is 30%.
[0041] 3) Heat treatment: The alloy is solution-treated...
Embodiment 2
[0043] The high-strength corrosion-resistant alloy material of this embodiment includes, by mass percentage: C: 0.08%, B: 0.005%, Cr: 18%, Ni: 8%, Co: 0.5%, Mn: 10%, Si: 0.4%, Nb: 0.5%, Mo: 0.5%, W: 1.0%, Ti: 1.4%, Al: 1.2%, and the balance is Fe.
[0044] The preparation method of this embodiment comprises the following steps:
[0045] 1) Raw material preparation: The ingredients include by mass percentage: C: 0.08%, B: 0.005%, Cr: 18%, Ni: 8%, Co: 0.5%, Mn: 10%, Si: 0.4%, Nb: 0.5% , Mo: 0.5%, W: 1.0%, Ti: 1.4%, Al: 1.2%, and the balance is Fe.
[0046] 2) Smelting and forming: The alloy is smelted by vacuum, and the pouring temperature of the alloy is controlled to be 1600 ℃. After completion, the ingot was homogenized at 1000°C for 16h. The alloy is processed and deformed by hot rolling, the rolling temperature is 1000 °C, the final rolling temperature is 700 °C, and the deformation amount in a single pass is 30%.
[0047] 3) Heat treatment: The alloy is solution-treate...
Embodiment 3
[0049] The preparation method of this embodiment comprises the following steps:
[0050] 1) Raw material preparation: The ingredients include by mass percentage: C: 0.07%, B: 0.007%, Cr: 17%, Ni: 10%, Co: 0.5%, Mn: 12%, Si: 0.2%, Nb: 0.8% , Mo: 0.3%, W: 1.5%, Ti: 1%, Al: 1%, and the balance is Fe.
[0051] 2) Smelting and forming: the alloy is smelted by vacuum, the vacuum degree is not higher than 0.5Pa, and the pouring temperature of the alloy is controlled to be 1620℃. After completion, the ingot was homogenized at 1000°C for 24h. The alloy is processed and deformed by hot rolling, the rolling temperature is 1000°C, the final rolling temperature is 700°C, and the deformation amount per pass is 30%.
[0052] 3) Heat treatment: The alloy is solution-treated at 1000°C, holding time for 1.5h, and water-cooled after the treatment is completed. The aging treatment temperature is 650°C, the holding time is 12h, and the water is cooled after the treatment is completed.
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