Preparation method of high temperature resistant Cu-Cr-Nb-Ce alloy for combustion chamber lining of aero-engine
A cu-cr-nb-ce, aero-engine technology, applied in the manufacturing field of aero-engine combustion chamber lining materials, can solve the problems of loss of strengthening effect, second phase coarsening, etc., and achieve no reduction in mechanical properties, low cycle Excellent fatigue performance and thermal conductivity, good ductility effect
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Embodiment 1
[0034] Such as figure 1 , 2 Shown, a kind of preparation method of high-temperature resistant Cu-Cr-Nb-Ce alloy for aero-engine combustor lining mainly comprises the following steps:
[0035] (1) Ingredients: The chemical composition and weight percentage of Cu-Cr-Nb-Ce alloy are: 6.45% Cr, 5.3% Nb, 0.05% Ce, 0.004% Fe, 0.004% Al, 0.003% C, 0.05% O, 0.001% N, the balance is copper, among which, Cu is added by electrolytic copper plate, Cr is added by CuCr10 master alloy, and Nb is added by pure Nb block;
[0036] (2) Vacuum induction smelting: the electrolytic copper plate of above-mentioned percentage by weight is packed in the vacuum induction furnace, vacuumizes, and after the electrolytic copper plate is melted, then respectively add CuCr10 master alloy and the Nb block that purity is 99.9% in the vacuum induction furnace, Heating up to 1600°C for smelting, finally adding rare earth Ce, feeding argon with a concentration of 99.999% for protection, and keeping it for 10 m...
Embodiment 2
[0041] Such as image 3 , 4 Shown, a kind of preparation method of high-temperature resistant Cu-Cr-Nb-Ce alloy for aero-engine combustor lining mainly comprises the following steps:
[0042] (1) Ingredients: The chemical composition and weight percentage of Cu-Cr-Nb-Ce alloy are: 6.65% Cr, 5.85% Nb, 0.065% Ce, 0.003% Fe, 0.003% Al, 0.002% C, 0.04% O, 0.001% N, the balance is copper, among which, Cu is added by electrolytic copper plate, Cr is added by CuCr10 master alloy, and Nb is added by pure Nb block;
[0043] (2) Vacuum induction smelting: the electrolytic copper plate of above-mentioned percentage by weight is packed in the vacuum induction furnace, vacuumizes, and after the electrolytic copper plate is melted, then respectively add CuCr10 master alloy and the Nb block that purity is 99.9% in the vacuum induction furnace, Heating up to 1600°C for smelting, finally adding rare earth Ce, feeding argon with a concentration of 99.999% for protection, and keeping it for 20...
Embodiment 3
[0048] Such as Figure 5 , 6 Shown, a kind of preparation method of high-temperature resistant Cu-Cr-Nb-Ce alloy for aero-engine combustor lining mainly comprises the following steps:
[0049] (1) Ingredients: The chemical composition and weight percentage of Cu-Cr-Nb-Ce alloy are: 7.4% Cr, 6.6% Nb, 0.065% Ce, 0.002% Fe, 0.002% Al, 0.001% C, 0.03% O, 0.001% N, the balance is copper, among which, Cu is added by electrolytic copper plate, Cr is added by CuCr10 master alloy, and Nb is added by pure Nb block;
[0050] (2) Vacuum induction smelting: the electrolytic copper plate of above-mentioned percentage by weight is packed in the vacuum induction furnace, vacuumizes, and after the electrolytic copper plate is melted, then respectively add CuCr10 master alloy and the Nb block that purity is 99.9% in the vacuum induction furnace, Heating up to 1600°C for smelting, finally adding rare earth Ce, feeding argon gas with a concentration of 99.999% for protection, and keeping the te...
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