A high-strength superalloy for thermal power units and its processing technology
A technology for superalloys and thermal power units, applied in the field of materials and material preparation, can solve the problems of poor structure stability and corrosion resistance, low thermal strength, high performance, etc., and achieve the effect of excellent high temperature strength performance
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[0028] The preparation process flow of the above alloy mainly includes alloy smelting, deformation, and heat treatment three steps, as follows:
[0029] (1) Smelting, homogenization treatment: The above-mentioned alloy is melting the induced electric arc furnace. The induction electric arc furnace is used to magnesium oxide alkaline furnace lining, and the pure nickel washing furnace is used before melting. Within 0.3-0.5Pa, CR, NI, W, Si, Mn, Mo, and Fe are completely melted after the alloy, and then GM, then Gas, Ti, B, Zr, and C, and cast; after solidification, the ingot is homogenized in the range of 1050-1120 ° C for 24-72 hours after air cooling to room temperature;
[0030] (2) Forging blank: The alloy of step (1) smelting and homogenization treatment is sanded over from γ 'precipitation temperature above 200-250 ° C, and the amount of deformation per second is not less than 30%, the final total deformation amount Not less than 70%;
[0031] (3) High temperature rolling: Th...
Embodiment 1
[0037] Thermal power according to the present embodiment is a high strength superalloy, in percentage by mass comprising: C: 0.06%, Cr: 16%, Mn: 0.2%, Si: 0.15%, W: 1.6%, Mo: 1.2%, Ti: 2.2 %, Al: 1.4%, B: 0.002%, Zr: 0.02%, Fe: 37%, the balance is Ni.
[0038] Basic lining alloy melting magnesium oxide, before the melting furnace using pure nickel washing, shot blasting treatment before addition of alloy materials. Induction arc melting the alloy, the degree of vacuum of 0.35 Pa at control, until Cr, Ni, W and other elements is completely melted and refined 40min, and prior to addition of Al, Ti, B, Zr, C into high purity argon gas protection. Cr, Ni, W, etc. alloy materials added after deoxidation coke completely melted, added mass does not exceed the alloy material containing 50% by mass of elements C, was added after completion of the second Ni-Mg alloy is deoxy, and finally adding Al, Ti, B , Zr, C and other elements easy burning, released after stirring for 5min, which castin...
Embodiment 2
[0042] High-strength superalloy according to the present embodiment, the percentage by mass comprising: C: 0.07%, Cr: 15%, Mn: 0.2%, Si: 0.15%, W: 2.2%, Mo: 0.4%, Ti: 2.2%, Al: 1.4%, B: 0.002%, Zr: 0.02%, Fe: 47%, the balance is Ni. Basic lining alloy melting magnesium oxide, before the melting furnace using pure nickel washing, shot blasting treatment before addition of alloy materials. Induction arc melting the alloy, the degree of vacuum of 0.35 Pa at control, until Cr, Ni, W and other elements is completely melted and refined 40min, and prior to addition of Al, Ti, B, Zr, C into high purity argon gas protection. Cr, Ni, W, etc. alloy materials added after deoxidation coke completely melted, added mass of not more than 40% C alloy material containing the element mass, after the completion of addition of the second Ni-Mg alloy was deoxygenated and finally Al, Ti, B , Zr, C and other elements easy burning, released after stirring for 5min, which casting temperature 1650 ℃. Alloy ...
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