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On the characterisation of subsurface deformation microstructures in aerostructural titanium alloys

机译:关于航空结构钛合金表面下变形组织特征的研究

摘要

A research programme has been undertaken to investigate the subsurface deformation microstructures in aerostructural titanium alloys that result from industrial surface finishing processes. Microstructural analysis of the region immediately below the treated surface has been performed for high speed machined and shot peened material, with emphasis placed on characterising the mode of plastic deformation through high resolution scanning electron microscopy and electron backscatter diffraction. Both shot peening and high-speed machining result in a plastically deformed subsurface layer, with experimental evidence collected through electron backscatter diffraction suggesting that the mode of plastic deformation is influenced by local textural heterogeneities (microtexture) in addition to alloy chemistry and substrate temperature. The stability of the deformed subsurface microstructure following exposure to elevated temperature is investigated for the near-alpha titanium alloy Ti-834. Here, shot peening leads to an increase in oxygen uptake kinetics during exposure to laboratory air in the temperature range 600°C to 700°C. The increased levels of subsurface oxygen versus the non-shot peened condition were measured by secondary ion mass spectrometry and fatigue testing has suggested a lowering of the high cycle endurance limit in shot peened Ti-834 following prolonged thermal exposure in air. The outcomes of this research suggest that the mode (and magnitude) of the residual plastic strain introduced by shot peening and high speed machining may be predicted; should an improved understanding of microtexture evolution during the primary processing (such as hot-working) of titanium alloys be achieved.
机译:已经进行了一项研究计划,以研究由工业表面精加工过程产生的航空结构钛合金中的亚表面变形微观结构。对于高速加工和喷丸处理的材料,已经对处理过的表面以下区域进行了微结构分析,重点放在通过高分辨率扫描电子显微镜和电子反向散射衍射表征塑性变形的模式上。喷丸处理和高速加工都会导致塑性变形的表面层,通过电子反向散射衍射收集的实验证据表明,塑性变形的模式除了合金化学性质和基材温度外,还受局部组织异质性(微观组织)的影响。对于接近α的钛合金Ti-834,研究了暴露于高温后变形的亚表面微观结构的稳定性。在这里,喷丸处理会导致在600°C至700°C的温度范围内暴露于实验室空气中时,氧气吸收动力学增加。通过二次离子质谱法测量了相对于未喷丸处理的条件,地下氧气含量的增加,疲劳测试表明,长时间暴露在空气中后,喷丸处理的Ti-834的高循环耐久性极限降低。这项研究的结果表明,可以预测通过喷丸处理和高速加工引入的残余塑性应变的模式(和大小);应该更好地了解钛合金的初加工(例如热加工)过程中的微观组织演变。

著录项

  • 作者

    Thomas Meurig;

  • 作者单位
  • 年度 2012
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  • 原文格式 PDF
  • 正文语种 English
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