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A study of anomalous hardening and deformation by superdislocations in single crystal titanium-56aluminum alloy.

机译:单晶钛-56铝合金超位错异常硬化和变形的研究。

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摘要

Uniaxial compression deformation has been conducted with single crystal gamma-Ti-56Al from 200K to 1073K in three orientations, [1¯ 6 12], [1¯ 2 6] and [2¯ 4 7]. The yield stress and critical resolved shear stress depend on temperature as well as deformation orientation under single slip of 101] superdislocations. A moderate dependence of the stresses on temperature and orientation was observed in the temperature range of RT to 673K while a strong dependence was found to occur in the temperature of 673K to 1073K. The results show that critical resolved shear stress of the single crystal deformed in these orientations is correlated with the Schmid factor for the 101] {lcub}111{rcub} slip systems at intermediate temperatures, and for cube-cross-slip at high temperatures. The Cottrell-Stokes type compression tests performed at 573K/873K show that the flow stress ratio, tau873/tau573, was found to be 1.5 for ascending sequence and 1.0 for descending sequence deformation, respectively. The difference between the two sequences is because the cubecross-slip structure of superdislocations resulted from deformation at high temperatures remains operating at intermediate temperatures. It suggested that the Cottrell-Stokes type compression in single crystal Ti-56Al was not fully reversible. High-resolution electron microscopy and weak beam imaging technique have been applied to the deformed single crystals for investigating of the self-dissociated superdislocation cores. The results revealed that the cores of dissociated superdislocations were partially cross-slipped onto a non-primary octahedral plane at intermediate temperatures forming a "rooftop configuration". The anomalous hardening behavior at intermediate temperatures can be explained by the proposed Interaction Energy Model. The cross-slip mode of the cores is characterized by the cube plane cross-slip at high temperatures. It is believed that Kear-Wilsdorf lock can be utilized to interpret the anomalous hardening at this temperature regime in Ti-56Al single crystal. The energy calculations suggest that "rooftop configuration" and Kear-Wilsdorf lock yield a minimum value of interaction energy between two coupling superpartials in an anisotropic medium. A sudden disappearance of anomalous hardening above their respective peak temperatures in three corresponding orientations was accompanied by the superseding of superdislocations with ordinary dislocations. It may be explained by the fact that the yield stress of ordinary dislocation is low enough to offset the Schmid factor advantage of superdislocation slip in {lcub}111{rcub} or {lcub}010) planes.
机译:单晶γ-Ti-56Al单晶压缩变形从200K到1073K在三个方向[1 6 12],[1 2 6]和[2 4 4]进行。屈服应力和临界解析剪切应力取决于温度以及<101]超位错的单滑移下的变形方向。在RT至673K的温度范围内观察到应力对温度和取向的适度依赖性,而在673K至1073K的温度下发现强烈的依赖性​​。结果表明,在中等温度下,在<101] {lcub} 111 {rcub}滑移系统中,在这些方向上变形的单晶的临界分辨剪切应力与施密特因子相关,而在高温下,对于立方相交滑动,它的施密德因子与。在573K / 873K进行的Cottrell-Stokes型压缩试验表明,流变应力比tau873 / tau573对于升序变形分别为1.5,对于降序变形为1.0。这两个序列之间的差异是因为由高温变形引起的超位错的立方交叉滑动结构仍在中间温度下运行。这表明单晶Ti-56Al中的Cottrell-Stokes型压缩不是完全可逆的。高分辨率电子显微镜和弱束成像技术已经应用于变形的单晶,以研究自解离的超位错核。结果显示,在中间温度下,解离的超位错核心部分交叉滑动到非主八面体平面上,形成“屋顶构型”。中间温度下的异常硬化行为可以通过提出的相互作用能模型来解释。铁芯的交叉滑动模式的特征在于在高温下的立方平面交叉滑动。据信,在该温度范围内,Ti-56Al单晶中可利用Kear-Wilsdorf锁来解释异常硬化。能量计算表明,“屋顶结构”和Kear-Wilsdorf锁在各向异性介质中产生了两个耦合超子之间的相互作用能的最小值。异常硬化在其各自的峰值温度之上在三个相应的方向上突然消失,伴随着超位错与普通位错的取代。可以通过以下事实来解释:普通位错的屈服应力足够低,以抵消{lcub} 111 {rcub}或{lcub} 010)平面中超位错滑移的Schmid因子优势。

著录项

  • 作者

    Wang, Zhongmin.;

  • 作者单位

    Polytechnic University.;

  • 授予单位 Polytechnic University.;
  • 学科 Engineering Materials Science.; Engineering Metallurgy.; Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1998
  • 页码 131 p.
  • 总页数 131
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;冶金工业;机械、仪表工业;
  • 关键词

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