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The role of microstructural variability on the very high cycle fatigue lifetime variability of the alpha + beta titanium alloy, Ti-6246 .

机译:微观结构变化对α+β钛合金Ti-6246的极高循环疲劳寿命变化的作用。

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摘要

The fatigue behavior of structural components in the regime of very high cycle fatigue (VHCF) (106-109 cycles) has been attracting increased commercial interest as components are increasingly being called upon to perform in this regime of lifetimes. In VHCF, the applied stresses relative to the yield stress are very low. Therefore, it is presumed that a substantial portion of fatigue lifetime is consumed by the fatigue crack initiation process, and that cyclic plasticity only accumulates in microstructural neighborhoods that are susceptible to fatigue damage accumulation. Thus, microstructural heterogeneity is believed to significantly effect the fatigue lifetime variability.;The very high cycle fatigue behavior of Ti-6246 has been investigated using ultrasonic fatigue techniques, and lifetimes ranging from 10 6-109 cycles have been observed. Fatigue cracks initiate by facet formation within αp grains. It has been found that the facets form in grains that are slightly larger than average and that the facets appear to form by a process of slip since the facet plane normals are oriented approximately 35-55° with respect to the tensile axis. Three characteristic fatigue crack initiation sites have been identified. These initiation sites, ranked in order of increasing fatigue resistance are: surface, subsurface with isolated facets, and subsurface with contiguous transgranular faceting. The texture of the material in these initiation regions is favorable for basal and prism slip. This texture is derived from the prior β texture, and a mechanism of fatigue crack initiation resulting from strain incompatibility has been proposed.;Fatigue crack growth experiments have been completed to measure the influence of local texture on the ease of fatigue crack initiation and the resulting fatigue crack growth rates. These experiments have found that the controlling microstructural dimension is on the order of 20-25 μm. The texture appears to affect initiation of fatigue cracks from notches as well. For notches placed within neighborhoods favorably oriented for basal slip, fatigue crack initiation will be encouraged. However, for notches placed within microstructural regions unfavorably oriented for basal slip, fatigue crack initiation will be inhibited.
机译:随着零件越来越多,在极高循环疲劳(VHCF)(10 6 -10 9 循环)状态下结构构件的疲劳行为已引起越来越多的商业兴趣。要求在这种终身制度下执行。在VHCF中,相对于屈服应力的施加应力非常低。因此,可以认为疲劳寿命的主要部分是由疲劳裂纹萌生过程所消耗的,并且循环可塑性仅累积在容易发生疲劳损伤累积的微结构附近。因此,微观结构的异质性被认为会显着影响疲劳寿命的变异性。;采用超声疲劳技术研究了Ti-6246的极高循环疲劳行为,其寿命范围为10 6 -10 9 个周期。疲劳裂纹是由α p 晶粒内的刻面形成引起的。已经发现,小面形成为比平均略大的晶粒,并且由于小面平面法线相对于拉伸轴取向为大约35-55°,因此小面似乎是通过滑动过程形成的。已经确定了三个特征性的疲劳裂纹萌生点。这些起始位置按耐疲劳性增加的顺序排列为:表面,具有孤立面的地下和具有连续的跨晶面的地下。在这些起始区域中,材料的质地对于基底和棱柱滑动是有利的。该纹理是从先前的β纹理衍生而来的,并提出了由应变不相容引起的疲劳裂纹萌生的机理。;已经完成了疲劳裂纹扩展实验,以测量局部纹理对疲劳裂纹萌生的容易程度及其结果的影响。疲劳裂纹的增长率。这些实验已经发现控制的微结构尺寸为20-25μm的量级。质地似乎也影响从缺口开始的疲劳裂纹。对于位于基部滑动方向有利的区域内的凹口,将鼓励疲劳裂纹的产生。但是,对于在基部滑动方向不利的微结构区域内放置的缺口,疲劳裂纹的产生将受到抑制。

著录项

  • 作者

    Szczepanski, Christopher J.;

  • 作者单位

    University of Michigan.;

  • 授予单位 University of Michigan.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2008
  • 页码 180 p.
  • 总页数 180
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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