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Crack Initiation, Propagation, and Arrest in 316L Model Pipe Components under Thermal Fatigue

机译:在热疲劳下316L模型管道部件中的裂纹启动,传播和停滞器

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There is a continuing need for reliable thermal fatigue analysis tools to ensure that high safety levels are maintained in the main coolant lines of light water reactors. As a contribution to this effort, a combined experimental and numerical investigation has been conducted on cylindrical components of 316L stainless steel subjected to cyclic thermal shocks of varying intensity. It exploits a dedicated rig in which the tubular test pieces are subjected to induction heating and water quenching. Under the applied loading, a network of cracks initiates at the inner surface; some of these propagate further through the wall thickness. The number of cycles to crack initiation is estimated from surface replicas taken during intermittent stops, whereas the crack depth of fatigue cracks is measured using an ultrasound time of flight diffraction technique (TOFD). The analysis is done by a sequentially coupled thermal-stress finite element analysis using a cyclic plasticity model. Predictions of the crack initiation life (based on crack initiation curves as well as crack propagation models for microstructurally short cracks) are in good agreement with the test results. Crack propagation for small fatigue cracks was estimated by plastic strain amplitude based propagation formulas, whereas long crack propagation is analyzed by Paris law type criteria using ΔK as well as ΔCTOD.
机译:有一个不断需要可靠的热疲劳分析工具,以确保较高的安全水平维持在轻水反应堆主冷却剂线。作为这种努力的一个贡献,组合的实验和数值调查已经对进行不同强度的环状热冲击316L不锈钢的圆柱形部件进行。它利用其中管状试验片经受感应加热和水淬专用钻机。下所施加的负载,在其内表面裂纹发起的网络;一些这些繁殖进一步通过壁的​​厚度。周期裂纹萌生的数目被从表面估计期间间歇停止副本所采取的,而疲劳裂纹的裂纹深度是使用飞行衍射技术(TOFD)的超声波的时间测量。该分析是通过使用循环塑性模型依次耦合热应力的有限元分析来完成。裂纹萌生寿命的预测(基于裂纹萌生曲线以及裂纹扩展模型微观结构短裂纹)与试验结果吻合良好。对于小疲劳裂纹裂纹扩展是由塑性应变振幅基于传播公式估计,而长裂纹扩展是通过使用ΔK以及ΔCTOD巴黎法类型标准进行分析。

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