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On fatigue damage and smal-crack growth behavior of silicon nitride under cyclic thermal-shock loading

机译:循环热冲击载荷作用下氮化硅的疲劳损伤和小裂纹生长行为

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The relationship between the cyclic crack grwoth rate and the maximum stress intensity factor was determined for polycrystalline silicon nitride under repeated thermal-shock loading conditions. For comparison purposes, the rate of fatigue-crack growth was also determined under load cycling conditions. It was observed that at the same nominal K_(max) value the crack growth rete under thermal-shock conditions was several orders of magnitude faster than under mechanical-fatigue loading. During quenching, a thermal gradient developed and macroscopic thermal stresses were produced in the singular stress field ahead of the crack. Also during the quench, microscopic tensile stresses developed within the grain boundary glassy phase as the result of a difference in the coefficient of thermal expansion between the silicon nitride and the glassy phase. The resulting combination of stresses resulted in the much greater rate of crack growth under cyclic thermal-shock conditions as compared to mechanical-fatigue conditions.
机译:在反复的热冲击载荷条件下,确定了多晶硅氮化硅的循环裂纹增长速率与最大应力强度因子之间的关系。为了进行比较,还确定了在负载循环条件下的疲劳裂纹增长率。可以看出,在相同的名义K_(max)值下,热冲击条件下的裂纹扩展速度要比机械疲劳载荷下快几个数量级。在淬火过程中,在裂纹前的奇异应力场中产生了一个热梯度,并产生了宏观的热应力。同样在淬火期间,由于氮化硅和玻璃相之间的热膨胀系数不同,在晶界玻璃相内产生了微观拉伸应力。与机械疲劳条件相比,在循环热冲击条件下,所产生的应力组合导致裂纹扩展的速率高得多。

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