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首页> 外文期刊>International Journal of Fatigue >Compression fatigue properties of open-cell aluminum foams fabricated by space-holder method
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Compression fatigue properties of open-cell aluminum foams fabricated by space-holder method

机译:空间保持器法制备的开孔泡沫铝的压缩疲劳性能

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摘要

The compression-compression fatigue properties of open-cell Al foams fabricated by space-holder method with different porosities were investigated. The epsilon-N curves of the Al foams show two types based on the stress levels (k). The first type shows a three-stages for low stress level (k 0.9), while the second type only presents stage I and stage III for high stress level (k = 0.9). The quasi-static compression tests were performed to determine the yield strength (sigma(s)) of Al foams. The fatigue strengths of Al foams with porosities of 50%, 60% and 70% are 12.77 MPa (0.75 sigma(s)), 7.61 MPa (0.68 sigma(s)) and 3.02 MPa (0.66 sigma(s)) respectively, showing a linear decrease with the increment of porosity. The macroscopic deformation observation shows that the local deformation regions during fatigue tests emerge earlier than those during quasi-static compression tests. The initiation and propagation of fatigue cracks are the main failure mechanism of Al foams subjected to compression fatigue loading.
机译:研究了不同孔隙率的空间支架法制备的开孔Al泡沫的压缩-压缩疲劳性能。铝泡沫的ε-N曲线根据应力水平(k)显示两种类型。第一种显示低应力水平的三个阶段(k <0.9),而第二种仅呈现高应力水平的第一阶段和第三阶段(k> = 0.9)。进行准静态压缩试验以确定Al泡沫的屈服强度(σ)。孔隙率为50%,60%和70%的Al泡沫的疲劳强度分别为12.77 MPa(0.75 sigma(s)),7.61 MPa(0.68 sigma)和3.02 MPa(0.66 sigma)。随着孔隙率的增加呈线性下降。宏观变形观察表明,疲劳试验中的局部变形区域比准静态压缩试验中的局部变形区域更早出现。疲劳裂纹的萌生和扩展是承受压缩疲劳载荷的Al泡沫的主要破坏机理。

著录项

  • 来源
    《International Journal of Fatigue》 |2019年第4期|272-280|共9页
  • 作者单位

    Civil Aviat Univ China, Sinoeuropean Inst Aviat Engn, Tianjin 300300, Peoples R China;

    Civil Aviat Univ China, Sinoeuropean Inst Aviat Engn, Tianjin 300300, Peoples R China;

    Civil Aviat Univ China, Sinoeuropean Inst Aviat Engn, Tianjin 300300, Peoples R China;

    Civil Aviat Univ China, Sinoeuropean Inst Aviat Engn, Tianjin 300300, Peoples R China;

    Civil Aviat Univ China, Airworthiness Inst, Tianjin 300300, Peoples R China;

    Tianjin Univ, Sch Mat Sci & Engn, Tianjin 300350, Peoples R China;

    Tianjin Univ, Sch Mat Sci & Engn, Tianjin 300350, Peoples R China;

    Tianjin Univ, Sch Mat Sci & Engn, Tianjin 300350, 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

    Quasi-static compression; Porosity; Fatigue property; Failure mechanism;

    机译:准静态压缩孔隙率疲劳性能破坏机理;

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