由于GH4065A合金的强化相γ'相的体积分数为43.0%,显微组织演化规律不同于传统的变形高温合金与粉末高温合金.系统分析了GH4065A合金的锻态组织特点与演化机制,发现其显微组织是一种不完全的动态再结晶(DRX)组织,动态再结晶晶粒被大尺寸γ '相限制长大,同时这些γ'相因晶界短路扩散而粗化,而未动态再结晶(unDRX)晶粒内弥散分布的小尺寸γ'相阻碍位错运动,进而形成大量由位错胞壁构成的亚结构.基于合金的锻态组织特点,可以通过固溶处理,利用动态回复(DRV)机制基本消除残留的未动态再结晶组织.根据GH4065A合金γ'相的固溶温度,可将热处理制度分为亚固溶处理与过固溶处理2种,亚固溶处理后的晶粒度为8.0级,过固溶处理的晶粒度为4.0级.经亚固溶处理后,GH4065A合金涡轮盘锻件的力学性能达到了第2代粉末涡轮盘的水平.
参考文献
[1] | Tresa M.Pollock;Sammy Tin .Nickel-Based Superalloys for Advanced Turbine Engines:Chemistry,Microstructure,and Properties[J].Journal of Propulsion & Power,2006(2):361-374. |
[2] | Rick Martin;Daniel Evans .Reducing costs in aircraft: the metals affordability initiative consortium[J].JOM,2000(3):24-28. |
[3] | Furrer D. .Ni-Based Superalloys for Turbine Discs[J].JOM,1999(1):0-0. |
[4] | Gerard Raisson .Evolution of PM nickel base superalloy processes and products[J].Powder Metallurgy,2008(1):10-13. |
[5] | Zhang G Q .Research and development of high temperature structural materials for aero-engine applications[J].Acta Metallurgica Sinica:English Letters,2009,18(04):443. |
[6] | Preliand F R;Furrer D.Lessons learned from the development,application and advancement of alloy 718[A].Pittsburgh:TMS,2014:3. |
[7] | Laurence A;Cormier J;Villechaise P.Impact of the solution cooling rate and of thermal aging on the creep properties of the new cast & wrought René 65 Ni-based superailoy[A].Pittsburgh:TMS,2014:297. |
[8] | Krueger D D;Kissinger R D;Menzies R G.Development and introduction of a damage tolerant high temperature nickel-base disk alloy[A].Pennsylvania:TMS,1992:277. |
[9] | Devaux A;Helstroffer A;Cormier J.Effect of aging heat-treatment on mechanical properties of AD730TM superalloy[A].Pittsburgh:TMS,2014:485. |
[10] | Devaux A;Picqué B;Gervais M F.AD730TM-a new nickel-based superalloy for high temperature engine rotative parts[A].Pennsylvania:TMS,2012:911. |
[11] | Wlodek S T;Kelly M;Alden D A.The structure of Rene 88DT[A].Pennsylvania:TMS,1996:129. |
[12] | 张北江,赵光普,胥国华,冯涤.GH742合金热变形行为与微观组织演化[J].金属学报,2005(11):1207-1214. |
[13] | Hutchinson B .Nucleation of recrystallisation[J].Scripta Metallurgica et Materialia,1992,27(11):1471. |
[14] | Hillert M .On the theory of normal and abnormal grain growth[J].ACTA METALLURGICA,1965,13(03):227. |
[15] | N. Moelans;B. Blanpain;P. Wollants .A phase field model for the simulation of grain growth in materials containing finely dispersed incoherent second-phase particles[J].Acta materialia,2005(6):1771-1781. |
[16] | Vengrenovitch R D .On the Ostwald ripening theory[J].ACTA METALLURGICA,1982,30(06):1079. |
[17] | Speight M V .Growth kinetics of grain-boundary precipitates[J].ACTA METALLURGICA,1968,16(01):133. |
[18] | James D W;Leak G M .Grain boundary diffusion of iron,cobalt and nickel in alpha-iron and of iron in gamma-iron[J].Philosophical Magazine,1965,12(117):491. |
[19] | F. Alexandre;S. Deyber;A. Pineau .Modelling the optimum grain size on the low cycle fatigue life of a Ni based superalloy in the presence of two possible crack initiation sites[J].Scripta materialia,2004(1):25-30. |
[20] | 张西锋,袁守谦,魏颖娟.超细晶粒钢的制备原理及技术[J].钢铁研究学报,2008(04):1-7. |
[21] | Siddall R J;Eggar J W .Production and quality control of superalloy forging-quality billet[J].Materials Science and Technology,1986,2(07):728. |
[22] | Mourer D P;Williams J L.Dual heat treat process development for advanced disk applications[A].Pennsylvania:TMS,2004:401. |
[23] | 师昌绪;颜鸣皋;刘伯操.中国航空材料手册[M].北京:中国标准出版社,2001 |
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