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AN INVESTIGATION OF THE FATIGUE CRACK GROWTH RATE CHARACTERISTICS OF TITANIUM ALLOY IMI829

机译:钛合金 IMI829 疲劳裂纹扩展速率特性的研究

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摘要

The primary objective of the investigation was to analyze fatigue crack growth (FCG) rate characteristics of IMI829(Ti-5.5A1-3.5Sn- 3Zr-1Nb-0.25Mo-0.3Si) between 20-600 degrees Celsius using quantitative and qualitative methods. The validity of the mode I stress intensity range (DELTA)K as a correlating parameter was also considered. FCG rate data was summarized as (DELTA)K vs. FCG rate and the main findings were as follows. At 20 degrees Celsius, the FCG rate at constant (DELTA)K increased with increase in R(minimum/maximum) load ratio. Visual estimate of threshold stress intensity range ((DELTA)K(,th)) was 9.0 MPa SQRT.(m) for R = +0.1 and 4.1 MPa SQRT.(m) for R = +0.6. Increasing temperature generally resulted in increased FCG rate for a constant (DELTA)K. The estimated (DELTA)K(,th) value decreased from 9.0 MPa SQRT.(m) at 20 degrees Celsius to 5.7 MPa SQRT.(m) at 475 degrees Celsius. At 600 degrees Celsius, the (DELTA)K(,th) increased to 6.4 MPa SQRT.(m). Very little change in (DELTA)K(,th) occurred with increase in temperature between 20 to 600 degrees Celsius for the R = +0.6 test conditions. Increase in temperature also resulted in greater sensitivity of FCG to (DELTA)K in the (DELTA)K(,th) region. The acquisition of low FCG rate data at elevated temper- ature was very difficult due to crack growth retardation effects. The elevated temperature fracture surfaces were coated with scale assumed to be TiO(,2). The most prominent fracture feature was cleavage-like facet formation through aligned (alpha) colonies. Other fracture features were furrow formation, ripple and regular striations, and mixed mode fracture. Fracture morphology remained unchanged between 20-600 degrees Celsius. The use of a mode I (DELTA)K parameter as a correlating parameter appears to be invalid because of cracking due to loading modes II and III. The relevance of an elevated temperature (DELTA)K(,th) was also placed in doubt because of the problems associated with the presence of scaling on the fracture surfaces and the test technique used to determine (DELTA)K(,th).
机译:调查的主要目的是使用定量和定性方法分析 IMI829(Ti-5.5A1-3.5Sn- 3Zr-1Nb-0.25Mo-0.3Si) 在 20-600 摄氏度之间的疲劳裂纹扩展 (FCG) 速率特性。还考虑了模式 I 应力强度范围 (DELTA)K 作为相关参数的有效性。FCG 率数据总结为 (DELTA)K 与 FCG 率,主要发现如下。在 20 摄氏度时,常数 (DELTA)K 下的 FCG 速率随着 R(最小/最大)负载比的增加而增加。阈值应力强度范围 ((DELTA)K(,th)) 的目测估计值为 9.0 MPa SQRT。(m) 对于 R = +0.1 和 4.1 MPa SQRT。R = +0.6 时的 (m)。温度升高通常会导致常数 (DELTA)K 的 FCG 速率增加。估计的 (DELTA)K(,th) 值从 9.0 MPa SQRT 下降。(m) 在 20 摄氏度至 5.7 MPa SQRT 时。(m) 在 475 摄氏度时。在 600 摄氏度时,(DELTA)K(,th) 增加到 6.4 MPa SQRT。(m). 对于 R = +0.6 测试条件,当温度升高 20 至 600 摄氏度时,(DELTA)K(,th) 的变化非常小。温度升高还导致 FCG 对 (DELTA)K(,th) 区域中的 (DELTA)K 更敏感。由于裂纹生长延缓效应,在高温下获取低 FCG 速率数据非常困难。高温断裂表面涂有假定为 TiO (,2) 的氧化皮。最突出的断裂特征是通过对齐的 (alpha) 菌落形成的卵裂样小面。其他骨折特征包括沟形成、波纹和规则条纹以及混合型骨折。骨折形态在 20-600 摄氏度之间保持不变。使用模式 I (DELTA)K 参数作为相关参数似乎是无效的,因为加载模式 II 和 III 会导致开裂。高温 (DELTA)K(,th) 的相关性也受到质疑,因为与断裂面上存在结垢相关的问题以及用于确定 (DELTA)K(,th) 的测试技术。

著录项

  • 作者

    SOOLEY, PATRICK MICHAEL;

  • 作者单位

    University of Toronto (Canada);

    University of Toronto (Canada);

    University of Toronto (Canada);

  • 授予单位 University of Toronto (Canada);University of Toronto (Canada);University of Toronto (Canada);
  • 学科 Mechanical engineering
  • 学位
  • 年度 1985
  • 页码 1
  • 总页数 1
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Mechanical engineering;

    机译:机械工程;

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