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Infrared Thermography for Non-destructive Evaluation of 2D C/SiC Composites Under Fatigue Loading

机译:用于疲劳负载下的2D C / SIC复合材料的非破坏性评估的红外热成像

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Fatigue tests of 2D C/SiC composites were performed on an Instron material testing machine.Constant-amplitude cyclic loading,with stress ratio (σmin/σmax) of 0.1 and sinusoidal frequency of 10Hz,were applied on plain and centre-holed plate specimens.Utilizing an infrared (IR) thermography system,the evolution of the surface temperature fields were monitored during the fatigue process.Damage evolution was discussed based on the variations of the modulus and the maximum temperature increment (△T) derived from IR image.At lower stress levels,△T rose quickly in the early cyclic stage and went steady as cycles processed.When the applied stress exceeded the fatigue endurance limit,△T rose rapidly until specimen failure.By analyzing △T during fatigue loading,it was possible to evaluate the damage evolution.△T had fairly well agreement with the damage evolution derived from modulus,and it could be used to predict the damage evolution of 2D C/SiC composites.
机译:在Instron材料试验机上进行了2D C / SiC复合材料的疲劳试验。在普通和中心孔板标本上施加了0.1的应力比(Σmin/σmax)的应力比(Σmin/σmax)。利用红外线(IR)热成像系统,在疲劳过程中监测表面温度场的演化。基于模量的变化和源自IR图像的最大温度增量(△T)讨论了阳光的变化。在早期的循环阶段,△T迅速升高的压力水平,随着循环处理的稳定而稳定。当施加的应力超过疲劳耐久性极限时,△T迅速升至样品衰竭。在疲劳负荷期间分析△T,可以评估损伤的演化。△T与模量衍生的损伤进化相当好,可用于预测2D C / SiC复合材料的损伤演化。

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