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Thermal Shock Damage Evaluation of Porous Refractory by Finite Element Method

机译:多孔耐火材料热冲击损伤的有限元评价。

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摘要

This work addresses damage evaluation of porous mullite refractory subjected to thermal shock. Incommunicating circular pores were distributed randomly at a volume percentage up to 40% in a cylinder of 20 cm diameter. The analysis was performed by means of the software ANSYS~® combined with a pre-program that generates randomly distributed pores of given size. The analysis procedure was divided into two stages. In the first, transient thermal analysis considering temperature-dependent material property was dealt with different thermal shock temperatures under natural cooling condition. The following structure analysis ran based on the obtained temperature distribution. The material damage was defined by that the local tensile stress reached to or was over the strength of the refractory. The extent of damage was determined as the ratio of the area of the damaged regions to the section area of the cylinder. The results show that the porosity, thermal shock temperature and cooling time have a high effect on the material damage. The lower the porosity is, the larger the extent of damage. The thermal damage increases with the raise of thermal shock temperature and the cooling time. The damage develops rapidly within 10 minutes but slows down after one hour cooling. The damage difference at high shock temperature stage (≥ 1000℃) is less than at low shock temperature stage. The pore size effect gets into practice only at high shock temperature stage: the damage increases with the raise of the pore size. The present research confirms that high porosity and small pore size could decrease greatly thermal shock damage and should be considered in the micro structural design of refractory.
机译:这项工作解决了遭受热冲击的多孔莫来石耐火材料的损伤评估。在直径为20 cm的圆柱体中,不连通的圆形孔以高达40%的体积百分比随机分布。分析是通过软件ANSYS®结合预程序生成的,该程序生成给定大小的随机分布的孔。分析过程分为两个阶段。首先,在自然冷却条件下,采用不同的热冲击温度来处理考虑温度依赖性材料特性的瞬态热分析。根据获得的温度分布进行以下结构分析。材料损坏的定义是达到或超过耐火材料强度的局部拉伸应力。损坏的程度确定为损坏区域的面积与圆柱体的截面积之比。结果表明,孔隙率,热冲击温度和冷却时间对材料的破坏影响很大。孔隙率越低,破坏程度越大。热损伤随着热冲击温度和冷却时间的升高而增加。损伤会在10分钟内迅速发展,但冷却一小时后会减慢。高冲击温度阶段(≥1000℃)的损伤差异小于低冲击温度阶段的损伤差异。孔径效应只有在较高的冲击温度阶段才能实现:损伤随着孔径的增加而增加。本研究证实,高孔隙率和小孔径可大大降低热冲击破坏,应在耐火材料的微观结构设计中予以考虑。

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