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Crack growth behavior under creep-fatigue conditions using compact and double edge notch tension-compression specimens.

机译:使用紧凑和双缺口缺口拉伸压缩试样在蠕变疲劳条件下的裂纹扩展行为。

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摘要

The American Society for Testing and Materials (ASTM) has recently developed a new standard for creep-fatigue crack growth testing, E 2760-10, that supports testing compact specimens, C(T), under load controlled conditions. C(T) specimens are commonly used for fatigue and creep-fatigue crack growth testing under constant-load-amplitude conditions. The use of these specimens is limited to positive load ratios. They are also limited in the amount of crack growth data that can be developed at high stress intensity values due to accumulation of plastic and/or creep strains leading to ratcheting in the specimen. Testing under displacement control can potentially address these shortcomings of the load-controlled tests for which the C(T) geometry is unsuitable. A double edge notch tension-compression, DEN(T-C), specimen to perform displacement controlled creep-fatigue crack growth testing is developed and optimized with the help of finite element and boundary element analyses. Accurate expressions for estimating the fracture mechanics crack tip parameters such as the stress intensity parameter, K, the crack mouth opening displacement (CMOD), and the load-line displacement (LLD) are developed over a wide range of crack sizes for the DEN(T-C) specimen. A new compliance relationship for use in experimental testing has been developed by using the compliance form available in ASTM E-647 standard. Experimentally determined compliance value compared well with the new relation for C15 steel (AISI 1015) and P91 steel tested at room and elevated temperature conditions respectively. Fatigue crack growth rate data generated using the DEN(T-C) specimens on the two metallic materials are in good agreement with the data generated using standard compact specimens; thus validating the stress-intensity factor and the compliance equation for the double edge notch tension-compression specimen. The testing has shown that the DEN(T-C) specimen is prone to crack asymmetry issues. Through inspection of fatigue surfaces, it has been found that that better alignment control procedures are needed to ensure symmetric crack fronts for the DEN(T-C) specimen. Creep-fatigue crack growth tests were conducted on 9Cr-1Mo (P91) steels at 625°C with various hold times. These tests were conducted using C(T) specimens under constant load amplitude conditions (tension-tension) and DEN(T-C) specimens under displacement like conditions (tension-compression). Crack growth data generated under creep-fatigue conditions using standard C(T) specimens correlated well with crack growth data generated using DEN(T-C) specimens. The crack growth rates per cycle increased significantly with increase in hold time when crack growth data were plotted with the cyclic stress intensity parameter, Delta-K. A transient behavior in the initial portion of da/dN versus Delta-K plots were observed for the hold time tests, as reported previously by several other researchers. It is shown for the C(T) specimens that the creep-fatigue interactions during crack growth for various hold times are represented better by the (Ct)avg parameter implying that the P91 steel behaves in a creep-ductile manner. Significant differences (factors of 2 to 5) were observed between the calculated values of (Ct)avg and those based on measured values of force-line deflection. It is also shown that there is a high risk of obtaining invalid data in longer hold time tests under force-control conditions. The usefulness of DEN(T-C) specimens for crack growth studies under displacement controlled conditions to combat ratcheting problems in tests conducted under load conditions is established. The tests conditions for the round-robin program on creep-fatigue crack growth testing in support of ASTM E-2760 are finalized. Further developments needed in creep-fatigue crack growth testing are also presented.
机译:美国材料试验学会(ASTM)最近开发了蠕变疲劳裂纹扩展测试的新标准E 2760-10,该标准支持在载荷控制的条件下测试紧凑的试样C(T)。 C(T)标本通常用于在恒定载荷-振幅条件下的疲劳和蠕变疲劳裂纹扩展测试。这些样品的使用仅限于正载荷比。由于塑性和/或蠕变应变的积累导致试样中出现棘轮现象,因此在高应力强度值下可能产生的裂纹扩展数据量也受到限制。在位移控制下的测试可以潜在地解决C(T)几何形状不适合的负载控制测试的这些缺点。在有限元和边界元分析的帮助下,开发并优化了可进行位移控制蠕变疲劳裂纹扩展测试的双缺口缺口拉伸压缩(DEN(T-C))试样。在广泛的DEN裂纹尺寸范围内,开发出用于估算断裂力学裂纹尖端参数(如应力强度参数,K,裂纹口张开位移(CMOD)和载荷线位移(LLD))的精确表达式。 TC)标本。通过使用ASTM E-647标准中提供的符合性表格,开发了一种用于实验测试的新符合性关系。实验确定的顺应性值与分别在室温和高温条件下测试的C15钢(AISI 1015)和P91钢的新关系进行了很好的比较。使用两种金属材料上的DEN(T-C)试样生成的疲劳裂纹扩展速率数据与使用标准紧凑型试样生成的数据非常吻合。从而验证了双切口缺口拉压试样的应力强度因子和柔度方程。测试表明DEN(T-C)样品容易出现裂纹不对称问题。通过检查疲劳表面,发现需要更好的对准控制程序来确保DEN(T-C)试样的对称裂纹前缘。在9Cr-1Mo(P91)钢上于625°C下以不同的保持时间进行了蠕变疲劳裂纹扩展测试。这些测试是使用C(T)试样在恒定载荷振幅条件下(拉伸-拉伸)和DEN(T-C)试样在类似位移的条件下(拉伸-压缩)进行的。使用标准C(T)标本在蠕变疲劳条件下生成的裂纹扩展数据与使用DEN(T-C)标本生成的裂纹扩展数据密切相关。当使用循环应力强度参数Delta-K绘制裂纹扩展数据时,每个周期的裂纹扩展速率随保持时间的增加而显着增加。如其他几位研究人员先前报道的,在保持时间测试中,观察到了da / dN与Delta-K图的初始部分的瞬态行为。对于C(T)试样表明,通过(Ct)avg参数可以更好地表示裂纹在不同保持时间内的蠕变疲劳相互作用,这表明P91钢表现出蠕变延性。在(Ct)avg的计算值与基于力线挠度的测量值之间存在显着差异(2到5倍)。还表明,在力控制条件下进行更长的保持时间测试时,获得无效数据的风险很高。建立了DEN(T-C)标本在位移控制条件下对抗裂纹在载荷条件下进行的棘轮问题方面的研究的有用性。确定了支持ASTM E-2760的蠕变疲劳裂纹扩展测试循环程序的测试条件。还介绍了蠕变疲劳裂纹扩展测试所需的进一步发展。

著录项

  • 作者单位

    University of Arkansas.;

  • 授予单位 University of Arkansas.;
  • 学科 Engineering Mechanical.;Applied Mechanics.;Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2013
  • 页码 188 p.
  • 总页数 188
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:42:13

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