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Defect evolution during high temperature tension-tension fatigue of SLM AISi10Mg alloy by synchrotron tomography

机译:SYSCRON断层扫描中SLM AISI10MG合金高温张力张力疲劳期间的缺陷演变

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摘要

Lack of fusion defects and porosity are inevitable characteristics of additive manufacturing and these are expected to play a key role in determining fatigue life and fatigue failure when excluding the influence of inho-mogeneous microstructures. This work followed damage accumulation under tension-tension cyclic loading at 250 °C in situ by time-lapse synchrotron radiation X-ray micro-computed tomography (SR-uCT) for AISilOMg test-pieces, produced by selective laser melting (SLM) over their complete fatigue lives (ranging from 180 to 38,000 cycles). These samples were found to accumulate widespread plastic strain each cycle in common with ultra-low cycle fatigue (UCLF) at low levels of triaxial constraint. The defects were found to elongate plastically at a rate approximately 10 times larger than their growth rate laterally. This elongation behaviour at room and elevated temperature fatigue is proportional to the accumulated longitudinal strain increment each cycle. Rotation under the influence of shear is also observed for those defects close to the surface of samples. Some defect coalescence was observed, but final failure was found to be associated with the nucleation of a high density of secondary microvoids (occurring at eutectlc Si platelets) that form just prior to failure and link up by microvoid coalescence. These steps may take up approximate 90% of the fatigue life. The final stage of cyclic plasticity occurs when the longitudinal strain exceeds ~ 0.9. Our results are in line with previous models of strain accumulation and defect growth under ULCF conditions.
机译:缺乏融合缺陷和孔隙度是添加剂制造的不可避免的特征,预计在排除造型造型微观结构的影响时,这些预计在确定疲劳寿命和疲劳失效时发挥关键作用。这项工作遵循张紧张力循环加载下的损伤积累,在250°C时通过时间流逝同步辐射X射线微计算机断层扫描(SR-UCT)用于AisiLOMG测试件,通过选择性激光熔化(SLM)产生他们完全的疲劳生活(从180到38,000个周期)。发现这些样品在低水平的三轴限制下累积广泛的塑性菌株,每个循环与超低循环疲劳(UCLF)共同。发现缺陷以横向大约10倍的速度伸长速度。在室内和升高的温度疲劳时这种伸长行为与每个循环的累积的纵向应变增量成比例。对于靠近样品表面的缺陷,也观察到剪切的影响下的旋转。观察到一些缺陷聚结,但是发现最终失败与在失败之前形成的次级微毒性高密度的高密度(在eutectLC Si血小板上发生)相关联的副失败。这些步骤可能占据疲劳寿命的90%。当纵向应变超过〜0.9时,会发生循环可塑性的最终阶段。我们的结果符合先前的ulcf条件下的应变累积和缺陷生长模型。

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  • 来源
    《Materials Science and Engineering》 |2020年第5期|139809.1-139809.13|共13页
  • 作者单位

    Department of Mechanical Material and Manufacturing Engineering University of Nottingham Nottingham NG7 2RD United Kingdom Aircraft Strength Research Institute Xi'an Shaanxi 710065 China;

    State Key Laboratory of Traction Power Southwest Jiaotong University Chengdu 610031 China Henry Royce Institute Department of Materials University of Manchester Manchester M13 9PL United Kingdom;

    Henry Royce Institute Department of Materials University of Manchester Manchester M13 9PL United Kingdom;

    State Key Laboratory of Traction Power Southwest Jiaotong University Chengdu 610031 China;

    Department of Mechanical Material and Manufacturing Engineering University of Nottingham Nottingham NG7 2RD United Kingdom Chengdu Aircraft Industrial (Croup) CO. LTD Chengdu Sichuan 610092 China;

    Shanghai Synchrotron Radiation Facility Shanghai Advanced Research Institute Chinese Academy of Sciences Shanghai 201204 China;

    Department of Mechanical Material and Manufacturing Engineering University of Nottingham Nottingham NG7 2RD United Kingdom;

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

    Defect evolution; X-ray tomography; High temperature; AISilOMg alloys; Additive manufacturing;

    机译:缺陷进化;X射线断层扫描;高温;Aisilomg合金;添加剂制造;

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