-
摘要: 采用气淬炉模拟了粉末高温合金Udimet720Li经空冷、风冷及油冷等不同冷却路径的固溶处理过程,测试了经过两级时效处理的合金在650 ℃的拉伸性能,研究了拉伸变形后的位错组态,分析了冷却速率对γ′强化相析出规律及力学性能的影响。结果表明:粉末高温合金Udimet720Li的析出相强化机制为位错切过机制,二次γ′相尺寸越小,合金强度越高。合金二次γ′相的形核析出温度区间为900~1000 ℃,其尺寸与合金在该温度范围内的冷却速率成反比,冷却速率越大,γ′相尺寸越小,当冷速高于100 ℃/min时,合金强度达到应用要求。推荐粉末Udimet720Li合金盘件固溶处理的冷却方式为:在1000 ℃以上保持低冷却速率来降低淬火应力,然后选择油浴作为盘件淬火的冷却方式,入油温度应在1000 ℃左右。Abstract: P/M superalloy Udimet720Li specimens were solutioned and quenched at the different cooling rates in gas quenching furnace, following by the double aging treatment. The microstructures and elevated temperature tensile properties at 650 ℃ were investigated, and the γ′ precipitation behavior and strengthening mechanism were analysed. The effect of cooling rates on the microstructures and properties of γ′ phase were discussed. Results show that the secondary γ′ phases mainly precipitate between 900 ℃ and 1000 ℃ for the P/M superalloy Udimet720Li, and the size of the secondary γ′ phases are inversely proportional to the cooling rates. The secondary γ′ phase interacts with the dislocations by shearing mechanism, enhancing the strength of P/M superalloy Udimet720Li. The strengthening effect increases with the decrease of the secondary γ′ phase size. To meet the strength requirement in practical application, the cooling rate should be more than 100 ℃/min. Therefore, the recommended solution cooling path for P/M superalloy Udimet720Li is shown as follow: the cooling rate should be slow to reduce the quenching stress above 1000 ℃, then the specimen can be quenched in oil at 1000 ℃ to obtain enough strength.
-
Key words:
- P/M superalloy /
- cooling rate /
- strengthening phase /
- mechanical property /
- solution treatment
-
表 1 粉末高温合金Udimet720Li名义成分(质量分数)
Table 1. Nominal composition of the P/M Udimet720Li alloys
% Cr Co Al Ti W Mo Zr B C Ni 16.000 14.750 2.500 5.000 1.250 3.000 0.035 0.020 0.015 余量 表 2 粉末高温合金Udimet720Li试样冷却路径
Table 2. Cooling paths of the P/M Udimet720Li specimens
试样编号 冷却路径 1 以30 ℃/min的速率从1100 ℃冷却至500 ℃ 2 以100 ℃/min的速率从1100 ℃冷却至500 ℃ 3 以250 ℃/min的速率从1100 ℃冷却至500 ℃ 4 以100 ℃/min的速率从1100 ℃冷却至1000 ℃,再以250 ℃/min的速率从1000 ℃冷却至500 ℃ 5 以100 ℃/min的速率从1100 ℃冷却至900 ℃,再以250 ℃/min的速率从900 ℃冷却至500 ℃ 表 3 两级时效处理后的粉末高温合金Udimet720Li试样γ′相尺寸及含量(体积分数)
Table 3. γ′ size and volume fraction of the P/M Udimet720Li specimens experiencing the double aging treatment
试样编号 二次γ′相平均尺寸 / nm 二次γ′相含量,
体积分数 / %1 149.7 48 2 127.8 45 3 87.7 47 4 90.3 46 5 131.2 44 表 4 两级时效处理后的粉末高温合金Udimet720Li试样的650 ℃拉伸性能
Table 4. Tensile properties of the P/M Udimet720Li specimens experiencing the double aging treatment at 650 ℃
试样编号 Rm / MPa Rp / MPa A / % Z / % 1 1282 980 35 35 2 1354 1041 30 34 3 1375 1091 28 30 4 1382 1095 24 24 5 1369 1037 27 28 注:Rm为抗拉强度;Rp为屈服强度;A为断后伸长率;Z为断面收缩率。 -
[1] Aba-Perea P E, Pirling T, Withers P J, et al. Determination of the high temperature elastic properties and diffraction elastic constants of Ni-base superalloys. Mater Des, 2016, 89: 856 doi: 10.1016/j.matdes.2015.09.152 [2] Jackson M P, Reed R C. Heat treatment of UDIMET 720Li: the effect of microstructure on properties. Mater Sci Eng A, 1999, 259(1): 85 doi: 10.1016/S0921-5093(98)00867-3 [3] Zou J W, Wang W X. Development and application of P/M superalloy. J Aeronaut Mater, 2006(3): 244 doi: 10.3969/j.issn.1005-5053.2006.03.051邹金文, 汪武祥. 粉末高温合金研究进展与应用. 航空材料学报, 2006(3): 244 doi: 10.3969/j.issn.1005-5053.2006.03.051 [4] Wang X F, Yang J, Zou J W, et al. Study on oxide inclusions of nickel-based P/M superalloy FHG96 by computed tomography technology. Powder Metall Technol, 2019, 37(4): 264王晓峰, 杨杰, 邹金文, 等. FGH96镍基粉末高温合金氧化物夹杂的计算机断层扫描研究. 粉末冶金技术, 2019, 37(4): 264 [5] Tian G F, Chen Y, Wang Y. Research on microstructure characterization in residual dendrite zones of FGH96 alloy with gradient microstructure. Powder Metall Technol, 2018, 36(6): 403田高峰, 陈阳, 汪煜. 梯度组织FGH96合金残留枝晶区的组织特征研究. 粉末冶金技术, 2018, 36(6): 403 [6] Zhou X M, Feng Y F, Zeng W H, et al. Effect of aging treatment on the behavior of room temperature tensile of P/M superalloys used for inertia friction welding joints. Powder Metall Technol, 2021, 39(1): 41周晓明, 冯业飞, 曾维虎, 等. 时效处理对粉末高温合金惯性摩擦焊接头室温拉伸行为的影响. 粉末冶金技术, 2021, 39(1): 41 [7] Goff S D L, Couturier R, Guétaz L, et al. Effect of the microstructure on the creep behavior of PM Udimet 720 superalloy—experiments and modeling. Mater Sci Eng A, 2004, 387-389: 599 doi: 10.1016/j.msea.2004.01.094 [8] Luo J, Bowen P. Statistical aspects of fatigue behaviour in a PM Ni-base superalloy Udimet 720. Acta Mater, 2003, 51(12): 3521 doi: 10.1016/S1359-6454(03)00171-X [9] Jiang R, Song Y D, Reed P A. Fatigue crack growth mechanisms in powder metallurgy Ni-based superalloys—A review. Int J Fatigue, 2020, 141: 105887 doi: 10.1016/j.ijfatigue.2020.105887 [10] Luo J, Bowen P. Small and long fatigue crack growth behaviour of a PM Ni-based superalloy, Udimet 720. Int J Fatigue, 2004, 26(2): 113 doi: 10.1016/S0142-1123(03)00139-7 [11] Goto M, Knowles D M. Initiation and propagation behaviour of microcracks in Ni-base superalloy Udimet 720 Li. Eng Fract Mech, 1998, 60(1): 1 doi: 10.1016/S0013-7944(98)00003-4 [12] Deng W K, Zhang D, Wu H Y, et al. Prediction of yield strength in a polycrystalline nickel base superalloy during interrupt cooling. Scr Mater, 2020, 183: 139 doi: 10.1016/j.scriptamat.2020.03.034 [13] Li J, Zhao Z Y, Bai P K, et al. Microstructural evolution and mechanical properties of IN718 alloy fabricated by selective laser melting following different heat treatments. J Alloys Compd, 2019, 772: 861 doi: 10.1016/j.jallcom.2018.09.200 [14] Li M, Coakley J, Isheim D, et al. Influence of the initial cooling rate from γ′ supersolvus temperatures on microstructure and phase compositions in a nickel superalloy. J Alloys Compd, 2018, 732: 765 doi: 10.1016/j.jallcom.2017.10.263 [15] He D G, Lin Y C, Tang Y, et al. Influences of solution cooling on microstructures, mechanical properties and hot corrosion resistance of a nickel-based superalloy. Mater Sci Eng A, 2019, 746: 372 doi: 10.1016/j.msea.2019.01.015 [16] Zhang L, Tian S G. Effect of long-term aging on γ′ phase and lattice constant of FGH95 P/M Ni-based superalloy. Powder Metall Technol, 2019, 37(3): 191张磊, 田素贵. 长期时效对FGH95镍基粉末高温合金γ'相及晶格常数的影响. 粉末冶金技术, 2019, 37(3): 191 [17] Yu Q Y, Dong J X, Zhang M C, et al. Thermodynamic calculation on equilibrium precipitated phases in GH720Li superalloy. Rare Met Mater Eng, 2010, 39(5): 857于秋颖, 董建新, 张麦仓, 等. 难变形高温合金GH720Li平衡析出相的热力学计算. 稀有金属材料与工程, 2010, 39(5): 857 [18] Kuo Y L, Horikawa S, Kakehi K. The effect of interdendritic δ phase on the mechanical properties of alloy 718 built up by additive manufacturing. Mater Des, 2017, 116: 411 doi: 10.1016/j.matdes.2016.12.026 [19] Shin K Y, Kim J H, Terner M, et al. Effects of heat treatment on the microstructure evolution and the high-temperature tensile properties of Haynes 282 superalloy. Mater Sci Eng A, 2019, 751: 311 doi: 10.1016/j.msea.2019.02.054 [20] Peng Z C, Tian G F, Jiang J, et al. Mechanistic behaviour and modelling of creep in powder metallurgy FGH96 nickel superalloy. Mater Sci Eng A, 2016, 676: 441 doi: 10.1016/j.msea.2016.08.101 [21] Reed R. The Superalloys: Fundamentals and Applications. London: Cambridge University Press, 2006 [22] Liu J, Peng Q, Xie J X. Grain structure and metallurgical defects regulation of selective laser melted René 88DT superalloy. Acta Metall Sinica, 2021, 57(2): 191刘健, 彭钦, 谢建新. 选区激光熔化René88DT高温合金的晶粒组织及冶金缺陷调控. 金属学报, 2021, 57(2): 191 [23] Luo X J, Wang X F, Ma G J, et al. Effect of heat treatment on microstructure and properties of FGH95 alloy. Powder Metall Technol, 2012, 30(1): 12 doi: 10.3969/j.issn.1001-3784.2012.01.003罗学军, 王晓峰, 马国军, 等. 热处理对FGH95合金组织和性能的影响研究. 粉末冶金技术, 2012, 30(1): 12 doi: 10.3969/j.issn.1001-3784.2012.01.003 [24] Zhong Z Y, Liu J T, Zhang Y W, et al. Effect of solution and aging temperature on microstructure and properties of a new powder superalloy. Powder Metall Ind, 2021, 31(1): 56钟治勇, 刘建涛, 张义文, 等. 固溶与时效温度对新型粉末高温合金组织和性能的影响. 粉末冶金工业, 2021, 31(1): 56