首页> 外文会议>2002 ASME Pressure Vessels and Piping Conference, Aug 5-9, 2002, Vancouver, British Columbia, Canada >FATIGUE CRACK PROPAGATION ANALYSIS OF A NOZZLE CORNER USING THE INFLUENCE FUNCTION METHOD
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FATIGUE CRACK PROPAGATION ANALYSIS OF A NOZZLE CORNER USING THE INFLUENCE FUNCTION METHOD

机译:基于影响函数法的喷嘴角疲劳裂纹扩展分析

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A calculation system has been developed in order to evaluate the thermal fatigue crack propagation of a semi-elliptical crack on the corner of a nozzle. One fatigue crack was assumed on the inner surface of the nozzle corner of a representative PWR reactor vessel. The stress intensity factors K were calculated at the deepest and outermost surface points of the crack using the influence function method. A database was prepared for the cracks with a depth of 0.022 t - 0.5 t (t: pressure vessel thickness) and an aspect ratio of 0.1 a/c - 1.0 a/c (a: crack depth and c: half surface width). Eight-noded solid elements and the finite element analysis code MARC were used. The calculation system enables the propagation of fatigue cracks at nozzle corners to be carried out in a very short time.
机译:为了评估喷嘴拐角处的半椭圆形裂纹的热疲劳裂纹扩展,已经开发了一种计算系统。在一个典型的PWR反应堆容器的喷嘴角的内表面上假定了一个疲劳裂纹。使用影响函数法计算了裂纹最深和最外表面点的应力强度因子K。准备了深度为0.022 t-0.5 t(t:压力容器厚度)和纵横比为0.1 a / c-1.0 a / c(a:裂纹深度和c:半表面宽度)的裂缝数据库。使用了八节点实体元素和有限元分析代码MARC。该计算系统使疲劳裂纹在喷嘴角处的传播可以在很短的时间内完成。

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