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首页> 外文期刊>International Journal of Fatigue >Evaluation of the effect of various prior creep-fatigue interaction damages on subsequent tensile and creep properties of 9%Cr steel
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Evaluation of the effect of various prior creep-fatigue interaction damages on subsequent tensile and creep properties of 9%Cr steel

机译:评估各种先前的蠕变-疲劳相互作用损伤对9%Cr钢随后的拉伸和蠕变性能的影响

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摘要

The degradation of tensile and creep properties is inevitable during high temperature service operation. Hence this work aims to evaluate the effect of prior creep-fatigue interaction damages on remnant tensile and creep properties of 9%Cr steel. Prior creep-fatigue tests interrupted at different lifetime fractions and different tensile hold times are performed at 650 degrees C. Afterwards, subsequent tensile and creep tests are conducted at the same temperature. Results reveal that high lifetime fraction of prior creep-fatigue loading leads to obvious reduction of remnant tensile strength and creep resistance. However, the increase in tensile hold time hardly alters the remnant properties. Microstructure and fracture surface observations indicate that the deterioration of remnant tensile strength is mainly ascribed to the decline of dislocation density occurred during prior creep-fatigue process, whereas the growth of martensite lath plays the dominated role in the reduction of remnant creep resistance. Moreover, surface crack also accelerates the decline of creep resistance at high lifetime fraction. To quantify the prior creep-fatigue interaction damage, a fatigue damage indicator is proposed. Determined relationships between remnant tensile, creep properties and defined fatigue damage are obtained.
机译:在高温使用过程中,拉伸性能和蠕变性能的降低是不可避免的。因此,这项工作旨在评估先前的蠕变-疲劳相互作用破坏对9%Cr钢的残余拉伸和蠕变性能的影响。先前的蠕变疲劳试验在650摄氏度下以不同的寿命分数和不同的拉伸保持时间中断。之后,在相同温度下进行后续的拉伸和蠕变试验。结果表明,先前蠕变疲劳载荷的高寿命分数导致残余抗拉强度和抗蠕变性的明显降低。但是,拉伸保持时间的增加几乎不会改变残余性能。显微组织和断裂表面的观察表明,残余抗拉强度的下降主要归因于先前蠕变疲劳过程中发生的位错密度的降低,而马氏体板条的生长在残余抗蠕变性能的降低中起着主导作用。此外,在高使用寿命时,表面裂纹还会加速抗蠕变性的下降。为了量化先前的蠕变-疲劳相互作用损伤,提出了疲劳损伤指标。获得了残余拉伸,蠕变性能和定义的疲劳损伤之间的确定关系。

著录项

  • 来源
    《International Journal of Fatigue》 |2019年第8期|440-453|共14页
  • 作者单位

    Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 211816, Jiangsu, Peoples R China|Jiangsu Key Lab Design & Manufacture Extreme Pres, Nanjing 211816, Jiangsu, Peoples R China|Univ Strathclyde, Dept Mech & Aerosp Engn, Glasgow G1 1XJ, Lanark, Scotland;

    Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 211816, Jiangsu, Peoples R China|Jiangsu Key Lab Design & Manufacture Extreme Pres, Nanjing 211816, Jiangsu, Peoples R China|Univ Ghent, Fac Engn & Architecture, B-9052 Zwijnaarde, Belgium;

    Univ Strathclyde, Dept Mech & Aerosp Engn, Glasgow G1 1XJ, Lanark, Scotland;

    Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 211816, Jiangsu, Peoples R China|Jiangsu Key Lab Design & Manufacture Extreme Pres, Nanjing 211816, Jiangsu, Peoples R China;

    Nanjing Tech Univ, Sch Mech & Power Engn, Nanjing 211816, Jiangsu, Peoples R China|Jiangsu Key Lab Design & Manufacture Extreme Pres, Nanjing 211816, Jiangsu, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Prior creep-fatigue loading; Remnant tensile and creep properties; Microstructure; Damage indicator;

    机译:事先蠕变疲劳载荷;残余拉伸和蠕变性能;微观结构;损伤指标;

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