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Frequency-dependent environmental fatigue crack propagation in the 7XXX alloy/aqueous chloride system.

机译:频率依赖性环境疲劳裂纹在7XXX合金/氯化水体系中的传播。

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摘要

The need to predict the fatigue performance of aging aerospace structures has focused interest on environmentally assisted cracking in thick-section damage-tolerant aluminum alloys (AA). The objective of this research is to characterize and understand the time-dependent processes that govern environmental fatigue crack propagation (EFCP) in 7XXX series aluminum alloys exposed to an aggressive environment. Results are utilized to identify the rate-controlling step in growth enhancement in order to develop a mechanistic model describing the time dependency of EFCP. Aluminum alloy 7075, tested in the sensitive (SL) orientation and exposed to aqueous chloride solution, is studied.; Da/dNcrit for different D K levels depends on 1/√fcrit, as predicted by process zone hydrogen-diffusion-limited crack growth modeling. A model based on hydrogen diffusion controlled growth is modified to include a stress-dependent critical hydrogen concentration normalized with the crack tip hydrogen concentration (Ccrit/CS).; It is proposed that da/dNcrit for a given D K and R corresponds to the distance ahead of the crack tip where the local tensile stress associated with Kmax is maximum. The reversed plasticity estimate of this location equals da/dNcrit for two aging conditions of 7075 (SL)/NaCl at R = 0.1. The EFCP dependencies on alloy microstructure (T6 vs. T7), crack orientation (SL vs. LT), and stress ratio are measured and interpreted based on their effect on da/dN crit and fcrit as well as environmental closure.; Chromate addition to the chloride solution eliminates the environmental acceleration of crack growth and reduces corrosion-product induced closure. In chromate-inhibited solution, the frequency dependence of EFCP in 7075 (SL) is unique. Da/dN is reduced at moderate and low frequencies to a value similar to crack growth rate in moist air, probably due to formation of a passive film which inhibits hydrogen uptake. Inhibition is mitigated by increasing frequency or increasing D K, which increase the crack tip strain rate, likely destabilizing the chromate protective film and promoting hydrogen uptake. (Abstract shortened by UMI.)
机译:预测老化的航空航天结构的疲劳性能的需求已引起人们的关注,重点是厚截面耐损铝合金(AA)的环境辅助开裂。这项研究的目的是表征和理解随时间变化的过程,这些过程控制着暴露于侵蚀性环境的7XXX系列铝合金的环境疲劳裂纹扩展(EFCP)。结果被用于识别生长增强中的速率控制步骤,以建立描述EFCP时间依赖性的机械模型。研究了在敏感(SL)方向上测试并暴露于氯化物水溶液的铝合金7075。如过程区氢扩散限制的裂纹扩展模型所预测,不同D K水平的Da / dNcrit取决于1 /√fcrit。修改了基于氢扩散控制生长的模型,使其包括由裂纹尖端氢浓度(Ccrit / CS)归一化的应力相关临界氢浓度。建议给定的D K和R的da / dNcrit对应于裂纹尖端之前的距离,在该距离处与Kmax相关的局部拉伸应力最大。对于两个老化条件为7075(SL)/ NaCl的R = 0.1,此位置的可逆塑性估计值等于da / dNcrit。 EFCP对合金微观结构(T6与T7),裂纹取向(SL与LT)以及应力比的依赖性是根据其对da / dN临界和临界和环境封闭的影响进行测量和解释的。向氯化物溶液中添加铬酸盐消除了裂纹扩展的环境加速作用,并减少了腐蚀产物引起的闭合。在铬酸盐抑制溶液中,EFCP在7075(SL)中的频率依赖性是独特的。 Da / dN在中等频率和低频下会降低到类似于潮湿空气中裂纹扩展速率的值,这可能是由于形成了抑制氢吸收的钝化膜。抑制作用可通过增加频率或增加D K来减轻,这会增加裂纹尖端的应变速率,从而可能会使铬酸盐保护膜失去稳定性并促进氢的吸收。 (摘要由UMI缩短。)

著录项

  • 作者

    Gasem, Zuhair Mattoug.;

  • 作者单位

    University of Virginia.;

  • 授予单位 University of Virginia.;
  • 学科 Engineering Materials Science.; Applied Mechanics.; Engineering Metallurgy.
  • 学位 Ph.D.
  • 年度 1999
  • 页码 214 p.
  • 总页数 214
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;应用力学;冶金工业;
  • 关键词

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