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Crack opening displacements during fatigue crack growth in Ti-SiC fibre metal matrix composites by X-ray tomography

机译:X射线层析成像技术在Ti-SiC纤维金属基复合材料疲劳裂纹扩展过程中的开裂位移

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摘要

High spatial resolution X-ray microtomography has been used to map the variation of crack opening displacement (COD) across matrix cracks in unidirectional Ti-6AI-4V/SCS-6 SiC fibre composites. These show the crack front to bow out between fibres as the crack emerges from a ply and to advance preferentially towards the fibres when located between plies. Quantitative image analysis of 3D volume reconstructions has enabled the COD to be measured at K_(min), K_(mid) and K_(max). Hysteresis in crack opening was observed during the fatigue cycle (loads applied statically). Very little variation in COD has been observed parallel to the crack front irrespective of proximity to the bridging fibres. The changes in COD relative to the initial residual opening at K_(min) are not inconsistent with being proportional to the square root of the distance from the crack tip. Considerable crack blunting was observed during an overload leading to a significant residual crack opening upon unloading.
机译:高空间分辨率X射线显微照相术已被用来绘制单向Ti-6AI-4V / SCS-6 SiC纤维复合材料中基体裂纹的开裂位移(COD)变化图。这些结果表明,当裂纹从层中出现时,裂纹前沿在纤维之间弯曲,并且当位于层之间时优先向纤维前进。对3D体积重建的定量图像分析使COD的测量值为K_(min),K_(mid)和K_(max)。在疲劳周期(静态施加的载荷)下观察到裂纹开口的滞后现象。平行于裂纹前沿观察到的COD变化很小,而与桥接纤维的接近程度无关。 COD相对于K_(min)处的初始残余开口的变化与与裂纹尖端距离的平方根成正比并不一致。在过载期间观察到相当大的裂纹钝化,导致在卸载时明显残留裂纹。

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