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Al元素对20Cr25NiNb耐热钢热老化行为的影响研究

舒茗 周钦 李刚 刘肖 孙永铎 赵可 肖军

舒茗, 周钦, 李刚, 刘肖, 孙永铎, 赵可, 肖军. Al元素对20Cr25NiNb耐热钢热老化行为的影响研究[J]. 核动力工程, 2023, 44(6): 140-147. doi: 10.13832/j.jnpe.2023.06.0140
引用本文: 舒茗, 周钦, 李刚, 刘肖, 孙永铎, 赵可, 肖军. Al元素对20Cr25NiNb耐热钢热老化行为的影响研究[J]. 核动力工程, 2023, 44(6): 140-147. doi: 10.13832/j.jnpe.2023.06.0140
Shu Ming, Zhou Qin, Li Gang, Liu Xiao, Sun Yongduo, Zhao Ke, Xiao Jun. Effect of Al Element on Thermal Aging Behavior of 20Cr25NiNb Heat-Resistant Steel[J]. Nuclear Power Engineering, 2023, 44(6): 140-147. doi: 10.13832/j.jnpe.2023.06.0140
Citation: Shu Ming, Zhou Qin, Li Gang, Liu Xiao, Sun Yongduo, Zhao Ke, Xiao Jun. Effect of Al Element on Thermal Aging Behavior of 20Cr25NiNb Heat-Resistant Steel[J]. Nuclear Power Engineering, 2023, 44(6): 140-147. doi: 10.13832/j.jnpe.2023.06.0140

Al元素对20Cr25NiNb耐热钢热老化行为的影响研究

doi: 10.13832/j.jnpe.2023.06.0140
基金项目: 四川省自然科学基金(2022NSFSC1191);中国核动力研究设计院原创基金(YF9722003)
详细信息
    作者简介:

    舒 茗(1990—),男,助理研究员,现主要从事先进反应堆结构材料研究,E-mail:shum09@163.com

  • 中图分类号: TG14;TL424

Effect of Al Element on Thermal Aging Behavior of 20Cr25NiNb Heat-Resistant Steel

  • 摘要: 为深入研究超临界气冷堆包壳材料的高温热老化行为以及Al元素对力学性能退化的影响,本文对添加Al元素和不含Al元素的2种20Cr25NiNb奥氏体耐热钢进行了750℃热老化试验,并开展了相应的微观组织分析和力学性能测试。研究发现,固溶态合金基体为奥氏体相,并含有少量微米级NbC。热老化后合金基体中析出了Laves相和σ相,而含Al钢中还观察到了NiAl相的析出。Al元素对20Cr25NiNb的热老化行为产生了双重影响,一方面,Al元素具有固溶强化效果,同时使得热老化后析出的Laves相尺寸更小、数密度更高,从而提升了高温拉伸强度;另一方面,蠕变裂纹主要沿晶界萌生并扩展,热老化后含Al合金中σ相体积分数更高,粗化更严重,严重降低了蠕变断裂寿命。不含Al合金晶界处析出的细小Laves相能有效阻止σ相生长,提升材料的蠕变性能。因此,本研究为超临界气冷堆包壳材料的成分优化提供了有力的支持。

     

  • 图  1  固溶态2025WMo的基体组织和析出相

    Figure  1.  Matrix and Precipitates of As-solutionized 2025WMo      

    图  2  固溶态和热老化态合金XRD图像

    Figure  2.  XRD Pattern of Solid Solution and Aged Alloys

    图  3  750℃下1000 h热老化后微观组织形貌

    Figure  3.  Microstructure after Thermal Aging at 750℃ for 1000 h      

    图  4  热老化后改进型20Cr25NiNb不锈钢主要析出相能谱分析结果

    Figure  4.  Energy Dispersive Spectroscopy Analysis of Precipitated Phases for Advanced 20Cr25NiNb Stainless Steels after Thermal Aging

    图  5  750℃、3000 h热老化后微观组织形貌

    Figure  5.  Microstructure after Thermal Aging at 750℃ for 3000 h      

    图  6  750℃、3000 h热老化后2025AFA基体中析出相伴生(BSE)

    Figure  6.  Accompanying Precipitation Behavior in Matrix of 2025AFA after Thermal Aging at 750℃ for 3000 h (BSE)

    图  7  750℃下合金工程应力-工程应变曲线图

    Figure  7.  Engineering Stress vs. Engineering Strain Curves of Alloys Tested at 750℃

    图  8  不同状态下2025WMo和2025AFA材料强度对照

    Figure  8.  Comparison of Strength for 2025WMo and 2025AFA Alloys under Different Heat Treatment State

    图  9  750℃蠕变应变-试验时间曲线图

    Figure  9.  Creep Strain versus Test Time Curves of Tested Alloys at 750℃

    图  10  2025AFA试样蠕变后微观组织图像

    Figure  10.  Microstructure of 2025AFA Sample after Creep       

    图  11  750℃、3000 h热老化后2025WMo析出相分布

    Figure  11.  Precipitates Distribution of 2025WMo after Thermal Aging at 750℃ for 3000 h

    图  12  750℃下试验合金热力学稳定相

    Figure  12.  Thermodynamically Stable Phases of Alloys Tested at 750℃

    表  1  试验用合金化学成分

    Table  1.   Chemical Composition of Alloys for Test

    编号 元素质量分数/%
    Ni Cr Nb Si Mn W Mo C Al Fe 其他
    2025WMo 23.50 20.0 0.76 0.5 0.7 2 1.0 0.047 余量
    2025AFA 23.44 19.4 0.83 0.2 0.6 2 1.1 0.057 2.5 余量 B<0.0025
    下载: 导出CSV

    表  2  热老化后合金Laves相和σ相尺寸和体积分数

    Table  2.   Size and Volume Fraction of Laves and σ Phases of the Tested Alloys after Thermal Aging

    样品 2025WMo 2025AFA
    热老化时间/h 1000 3000 1000 3000
    Laves相 平均尺寸d/μm 0.2823 0.4107 0.2315 0.2480
    f /% 1.03 1.82 1.28 1.34
    σ相 平均尺寸d /μm 1.2779 1.2536 1.2251 1.4899
    f /% 1.52 2.92 9.65 17.04
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-06-20
  • 修回日期:  2023-07-31
  • 网络出版日期:  2023-12-11
  • 刊出日期:  2023-12-15

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