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Improved test method and analytical modelling for fatigue crack growth in coarse-grain titanium alloy with rough fatigue surfaces

机译:具有粗糙疲劳表面的粗晶粒钛合金疲劳裂纹扩展的改进测试方法和分析模型

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Fatigue crack growth rate properties are typically determined by experimental methods in accordance with ASTM Standard E647. These traditional methods use standard notched specimens that are precracked under cyclic tensile loads before the main test The data that are produced using this approach have been demonstrated elsewhere to be potentially adversely affected by the test method, particularly in the threshold region where load reduction (LR) methods are also required. Coarse-grained materials that exhibit rough and tortuous fatigue surfaces have been observed to be strongly affected by the tensile precracking and LR, in part because the anomalies caused by crack closure and roughness-induced closure become more important The focus of the work reported in this paper was to further develop methods to determine more accurate fatigue crack growth rate properties from threshold through to fracture for coarse-grained, β-annealed, titanium alloy Ti-6Al-4V extra low interstitial thick plate material. A particular emphasis was put upon the threshold and near threshold region, which is of strong importance in the overall fatigue life of components. New approaches that differ from the ASTM Standard included compression precracking, LR starting from a lower load level and continuing the test beyond rates where crack growth would otherwise be considered below threshold. For the threshold regime, two LR methods were also investigated: the ASTM method and a method where the load is reduced with crack growth such that the crack mouth opening displacement is held constant, in an attempt to avoid remote closure. Constant amplitude fatigue crack growth rate data were produced from threshold to fracture for the titanium alloy at a variety of stress ratios. Spike overload tests were also conducted These data were then used to develop an improved analytical model to predict crack growth under spectrum loading and the predictions were found to correlate well with test results.
机译:疲劳裂纹扩展速率特性通常根据ASTM标准E647通过实验方法确定。这些传统方法使用标准的缺口试样,该试样在主要测试之前已在周期性拉伸载荷下预先开裂。使用这种方法产生的数据已在其他地方得到证明,可能会受到测试方法的不利影响,特别是在降低载荷的阈值区域(LR )方法也是必需的。观察到粗晶粒材料显示出粗糙且曲折的疲劳表面,受到拉伸预裂纹和LR的强烈影响,部分原因是由裂纹闭合和粗糙度引起的闭合引起的异常变得更加重要。论文将进一步开发方法,以确定更粗的,β退火的钛合金Ti-6Al-4V超低间隙厚板材料从阈值到断裂的更精确的疲劳裂纹扩展速率特性。特别强调了阈值区域和阈值附近区域,这对于组件的整体疲劳寿命非常重要。与ASTM标准不同的新方法包括压缩预裂化,从较低的载荷水平开始LR并继续进行测试,超出了否则裂纹扩展将被视为低于阈值的速率。对于阈值状态,还研究了两种LR方法:ASTM方法和一种方法,该方法随着裂纹的增长而减小载荷,以使裂纹口张开位移保持恒定,从而避免远程闭合。钛合金在各种应力​​比下,从阈值到断裂都产生了恒定振幅的疲劳裂纹扩展速率数据。还进行了尖峰过载测试,然后将这些数据用于开发改进的分析模型,以预测在频谱载荷下的裂纹扩展,并且发现这些预测与测试结果非常相关。

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