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首页> 外文期刊>Materials & design >Compressive and wear behaviors of bulk nanostructured A12024 alloy
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Compressive and wear behaviors of bulk nanostructured A12024 alloy

机译:块状纳米结构A12024合金的压缩和磨损行为

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摘要

Compressive and wear properties of bulk nanostructured A12024 alloy prepared by mechanical milling and hot pressing methods were investigated. A12024 powders were subjected to high-energy milling for 30 h to produce nanostructured alloy. As-milled powders were compacted at 500℃ under 250 MPa in a uniaxial die. Consolidated sample had an average hardness and relative density values of 207.6 HV and 98%, respectively. Uniaxial compression tests at strain rates in the range of 1.67 × 10~(-4)-1.67 × 10~(-2) s~(-1) were performed using an Instron-type machine. The wear behavior of nanostructured sample was investigated using a pin-on-disk technique under an applied load of 20 N. The compression and wear experiments were also executed on samples of commercial coarse-grained A12024-0 (annealed) and A12024-T6 (artificially-aged) alloys, for comparison. The structure of consolidated A12024 was characterized by X-ray diffraction (XRD). The yield strength and compressive strength of nanostructured A12024 reached a value of ~698 MPa and ~712 MPa at strain rate of 1.67 × 10~(-4) s~(-1) respectively, which was considerably higher than those for coarse-grained A12024-O and A12024-T6 counterparts. Worn surfaces and the wear debris were analyzed by scanning electron microscopy (SEM), energy dispersive spec-troscopy (EDS) and XRD. Nanostructured A12024 revealed a low friction coefficient of 0.3 and a wear rate of ~12 × 10~(-3)mg/m, which are significantly lower than those obtained for A12024-O and A12024-T6 alloys. This enhanced wear resistance was mainly caused by nanocrystalline structure with high hardness value. The dominating wear mechanism of nanostructured AI2024 appeared to be delamination mechanism.
机译:研究了通过机械研磨和热压法制备的块状纳米A12024合金的压缩和磨损性能。将A12024粉末进行高能研磨30小时,以生产纳米结构合金。研磨后的粉末在单轴模具中在500℃,250 MPa下压实。固结样品的平均硬度和相对密度分别为207.6 HV和98%。使用Instron型机器进行应变率在1.67×10〜(-4)-1.67×10〜(-2)s〜(-1)范围内的单轴压缩试验。使用针盘技术在20 N的负载下研究了纳米结构样品的磨损行为。还对商品化的粗粒A12024-0(退火)和A12024-T6(退火)样品进行了压缩和磨损实验。人工时效)合金,以作比较。固结的A12024的结构通过X射线衍射(XRD)表征。纳米结构A12024的屈服强度和抗压强度分别在1.67×10〜(-4)s〜(-1)的应变速率下分别达到〜698 MPa和〜712 MPa,大大高于粗晶粒。 A12024-O和A12024-T6对应。通过扫描电子显微镜(SEM),能量色散光谱仪(EDS)和XRD分析磨损的表面和磨损碎片。纳米结构的A12024的摩擦系数低至0.3,磨损率约为12×10〜(-3)mg / m,明显低于A12024-O和A12024-T6合金。这种增强的耐磨性主要是由具有高硬度值的纳米晶体结构引起的。纳米结构AI2024的主要磨损机制似乎是分层机制。

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  • 来源
    《Materials & design》 |2010年第2期|663-669|共7页
  • 作者单位

    Department of Materials Engineering, Isfahan University of Technology, Isfahan 84156-83111, Iran;

    Department of Materials Engineering, Isfahan University of Technology, Isfahan 84156-83111, Iran;

    Department of Materials Engineering, Isfahan University of Technology, Isfahan 84156-83111, Iran;

    Department of Materials Engineering, Isfahan University of Technology, Isfahan 84156-83111, Iran;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    nano materials (A); mechanical properties (E); wear (E);

    机译:纳米材料(A);机械性能(E);我们是);

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