Inconel 718变形高温合金热加工组织演变与发展趋势
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  • 英文篇名:Microstructure Evolution of Inconel 718 Superalloy During Hot Working and Its Recent Development Tendency
  • 作者:刘永长 ; 张宏军 ; 郭倩颖 ; 周晓胜 ; 马宗青 ; 黄远 ; 李会军
  • 英文作者:LIU Yongchang;ZHANG Hongjun;GUO Qianying;ZHOU Xiaosheng;MA Zongqing;HUANG Yuan;LI Huijun;State Key Lab of Hydraulic Engineering Simulation and Safety,School of Materials Science and Engineering,Tianjin University;
  • 关键词:Inconel ; 718合金 ; 再结晶 ; 选区激光熔化 ; 位错剪切机制 ; g″-g'强化型合金
  • 英文关键词:Inconel 718 alloy;;recrystallization;;selective laser melting;;dislocation-shearing mechanism;;g″-g' strengthened superalloy
  • 中文刊名:JSXB
  • 英文刊名:Acta Metallurgica Sinica
  • 机构:天津大学材料科学与工程学院水利安全与仿真国家重点实验室;
  • 出版日期:2018-11-11
  • 出版单位:金属学报
  • 年:2018
  • 期:v.54
  • 基金:国家自然科学基金项目Nos.51474156;51604193和U1660201;; 国家高技术研究发展计划项目No.2015AA042504~~
  • 语种:中文;
  • 页:JSXB201811016
  • 页数:12
  • CN:11
  • ISSN:21-1139/TG
  • 分类号:185-196
摘要
本文首先针对Inconel 718合金的锻造工艺过程,较为系统地阐述了合金高温变形时的再结晶机制、晶粒长大、d相形态控制以及存在的残余应力问题。基于选区激光熔化技术在航空发动机材料增材制造领域的潜在优势和应用前景,分析了选区激光熔化技术制造Inconel 718合金凝固组织和性能的各向异性,探讨了热处理工艺在消除有害相、改变组织结构及力学行为等方面的重要作用和局限性。结合高温服役过程的组织演变,分析了Inconel 718合金变形时涉及位错滑移、孪生、g″相剪切方式的变形机制。最后,介绍了通过调整Inconel 718合金成分来改变强化相结构,从而进一步提高变形高温合金服役温度的有效尝试(如Allvac 718Plus合金的服役温度提高了55℃),指出了通过成分调整来获得热稳定性优异的g″-g'复合析出结构是新型变形镍基高温合金的重要发展方向。
        Here some critical issues existed during forging process of Inconel 718 disks involving recrystallization mechanisms, grain growth, d-phase morphology control and residual stress are explained.Based on the potential application prospect of selective laser melting in additive manufacture of aerocraft engine components, the specialized anisotropic microstructure and mechanical performance resulted from the rapid solidification process in selective laser melting are analyzed. Furthermore, the importance and difficulty of heat treatment in eliminating Laves-phase as well as tailoring substructure and related mechanical behavior are also discussed. The deformation mechanisms of Inconel 718 alloy at high temperature are illustrated in detail, comprising of dislocation planar slip, twinning and dislocation-shearing g″precipitates in complex modes. At last, a newly developed wrought nickel superalloy(Allvac 718 Plus, with a increase in service temperature of 55 ℃ as compared to that of Inconel 718) is introduced, and some recent progresses aimed at modifying chemical compositions and phase compositions to improve service temperature on the basis of Inconel 718 alloy are also reviewed. The results indicate that the more stable g″-g' composite structure is important for the further design of next-generation wrought nickel superalloys.
引文
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