期刊文献+

变形参数对FGH4113A粉末高温合金微观组织演化的影响

Effect of Deformation Parameters on Microstructure Evolution of FGH4113A Powder Metallurgy Superalloy
原文传递
导出
摘要 针对一种新型粉末高温合金FGH4113A(WZ-A3)进行了一系列热压缩实验,探究了变形温度、应变速率、应变量对微观组织演化的影响规律,并提出了获得细小均匀γ+γ′双相晶粒组织的热变形参数。结果表明:在温度1100℃、应变速率0.1 s^(-1)、真应变0.1~0.7范围内,应变增大有利于促进动态再结晶以及细化晶粒。随应变增加,γ’相体积分数先减小后增大,随后保持稳定,并且在热变形过程中γ’相形貌逐渐趋于球形。在温度1100℃、变形量50%、应变速率0.01~1 s^(-1)范围内,应变速率增大能够提高动态再结晶程度并细化晶粒。应变速率由0.01~0.1 s^(-1)增大至1 s^(-1)时,由于绝热温升以及位错滑移加剧,γ’相体积分数减小约2%。在应变速率0.1s^(-1)、变形量50%、温度1070~1160℃范围内,变形温度的提升有利于促进动态再结晶和晶粒长大。随着变形温度升高至1130℃,γ’相已大量溶解,钉扎晶界能力大幅减弱,平均晶粒尺寸增大至12.1μm。在变形温度1100℃、应变速率1 s^(-1)、50%变形量条件下可以获得均匀细小的γ+γ′双相晶粒组织,晶粒度能够达到12级以上。 Through a series of hot compression tests on a novel powder metallurgy superalloy FGH4113A(WZ-A3),the effects of deformation temperature,strain rate and strain on the microstructure evolution were investigated.The results demonstrate that when the temperature is 1100℃,the strain rate is 0.1 s^(-1) and the true strain is between 0.1 and 0.7,the increase in strain is beneficial to promoting dynamic recrystallization and grain refinement.With the increase in strain,the volume fraction ofγ'phase first decreases,then increases,and eventually remains stable.The morphology ofγ'phase gradually becomes spherical during the thermal deformation process.Under the conditions of temperature 1100℃,deformation 50%and strain rate of 0.01-1 s^(-1),the increase in strain rate can improve the degree of dynamic recrystallization and refine the grains.With the increase in strain rate from 0.01-0.1 s^(-1) to 1 s^(-1),the adiabatic temperature rises and dislocation slip intensifies,reducing the volume fraction ofγ'phase by about 2%.When the strain rate is 0.1 s^(-1) and the deformation is 50%,the increase in deformation temperature can promote dynamic recrystallization and grain growth in the temperature range of 1070-1160℃.With the deformation temperature rising to 1130℃,a large quantity ofγ'phase has dissolved,the ability to pin the grain boundary has been significantly weakened,and the average grain size has increased to 12.1μm.At the deformation temperature of 1100℃,strain rate of 1 s^(-1) and deformation of 50%,fine and uniformγ+γ′dual-phase structure with the grain size above ASTM 12 can be obtained.
作者 何英杰 马向东 李远 肖磊 杨金龙 郭建政 冯干江 He Yingjie;Ma Xiangdong;Li Yuan;Xiao Lei;Yang Jinlong;Guo Jianzheng;Feng Ganjiang(Shenzhen Wedge Central South Research Institute Co.,Ltd,Shenzhen 518000,China;State Key Laboratory of Powder Metallurgy,Central South University,Changsha 410083,China;Shenzhen Wedge Aviation Technology Co.,Ltd,Shenzhen 518000,China)
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2024年第1期223-233,共11页 Rare Metal Materials and Engineering
基金 国家科技重大专项(2017-Ⅵ-0009-0080) 广东省重点领域研发计划(2019B010935001) 深圳市海外高层次人才资金(KQTD2015032716463668) 深圳市科技计划(JSGG20210802093205015)。
关键词 粉末高温合金 热变形 γ′相 动态再结晶 晶粒尺寸 powder metallurgy superalloy hot deformation γ′phase dynamic recrystallization grain size
  • 相关文献

参考文献10

二级参考文献64

  • 1王淑云,李惠曲,计晟,杨洪涛,谭勇,李辉忠.等温锻造FGH96合金超塑性研究[J].航空材料学报,2003,23(z1):25-28. 被引量:9
  • 2国为民,董建新,吴剑涛,张凤戈,陈淦生,陈生大.FGH96镍基粉末高温合金的组织和性能[J].钢铁研究学报,2005,17(1):59-63. 被引量:36
  • 3贾建,陶宇,张义文,张莹,刘建涛.第三代粉末冶金高温合金René104的研究进展[J].粉末冶金工业,2007,17(3):36-43. 被引量:27
  • 4Rao K P,Hawbolt E B.Development of Constitutive Relationships Using Compression Testing of a Medium Carbon Steel.Transactions of ASME,1992,114(1):116-123.
  • 5Brand A J,Karhauson K,Kopp R.Microstructural Simulation of Nickel Base Alloy Inconed 718 in Production of Turbine Disks.Materials Science and Technology,1996,12(11):963-969.
  • 6Park Nho-Kwang,Yoem Jong-Taek,Na Young-Sang.Characterization of Deformation Stability in Hot Forging of Conventional Ti-6Al-4V Using Processing Maps.Journal of Materials Processing Technology,2002,130-131:540-545.
  • 7Gronostajski Z.The Deformation Processing Map for Control of Microstructure in CuAl9.2Fe3 Aluminium Bronze.Journal of Materials Processing Technology,2002,125-126:119-124.
  • 8Cavaliere P,et al.Isothermal Forging of AA2618+20% Al2O3 by Means of Hot Torsion and Hot Compression Tests.Materials Science and Engineering A,2004,387-389:857-861.
  • 9Ramanathan S,et al.Hot Deformation Behavior of 2124 Al Alloy.Journal of Materials Science and Technology,2006,22(5):611-615.
  • 10刘莹莹,姚泽坤,郭鸿镇.航空发动机用双性能盘的制造技术研究进展[J].材料导报,2007,21(12):95-98. 被引量:23

共引文献60

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部