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Stress intensity factors for mixed-mode crack growth in imitation models under biaxial loading

机译:双轴载荷下仿制模型混合模式裂纹增长的应力强度因子

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In this study a procedure to stress intensity factors calculation for imitation models made of titanium alloy is described. In service fatigue cracks are detected in a disk and blade “dovetail type” attachment. On the base of this attachment dimensions and with taking into account the biaxial loading conditions of rotating compressor disk the two geometries of imitation model of gas turbine engine compressor disk are developed. To accurate verification of biaxial loading conditions, the first imitation model of constant thickness is used. In order to fully reproduce the geometry of the compressor disk and conditions of mixed mode crack growth, the second imitation model with reduced cross section is proposed. The fatigue crack growth experiments of imitation models were carried out at room temperature on a biaxial testing machine. Two different stress ratio values are applied several times to each imitation model in order to fix the experimental crack front positions. The elastic and plastic stress intensity factors used for the representation of the experimental results are computed by using full-size 3D Finite Element analysis of the imitation models with surface quarter elliptical and through-thickness cracks.
机译:在本研究中,描述了一种对由钛合金制成的仿制模型计算的应力强度因子计算的过程。在使用的疲劳裂缝中,在盘和叶片“燕尾榫型”附件中检测到。在该附接尺寸的基础上,并且考虑到旋转压缩机盘的双轴装载条件,开发了燃气涡轮发动机压缩机盘的仿制模型的两个几何形状。为了精确验证双轴负载条件,使用恒定厚度的第一模拟模型。为了完全再现压缩机盘的几何形状和混合模式裂纹生长的条件,提出了具有减少横截面的第二模拟模型。在双轴试验机上在室温下进行仿制模型的疲劳裂纹生长实验。将两个不同的应力比值用于每个模拟模型的多次应用,以固定实验裂缝前位置。用于表示实验结果的弹性和塑性应力强度因子通过使用具有表面椭圆形和厚度裂缝的仿制模型的全尺寸3D有限元分析来计算。

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