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Numerical study on heat transfer and thermal stress of the upper cone membrane wall in radiant syngas cooler

机译:辐射合成气冷却器上锥膜壁的热传递和热应力的数值研究

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The high temperature syngas induced from the entrained-flow gasifier contains a large amount of sensible heat, which can be efficiently recovered by radiant syngas cooler (RSC). In this work, the membrane wall models of the upper cone section in the RSC are established. The heat transfer characteristics between membrane wall and syngas are explored by numerical simulation under different operating conditions, and the thermal stress distribution on the membrane wall surface is calculated by the fluid-structure coupling method. The results show that the inner surface of the fin is partially overheated and the maximum stress exceeds the allowable stress of the material when there is no protection for the membrane wall. The increase of inlet syngas temperature and flow rate will enhance heat transfer of the upper cone membrane wall, and the effect of the inlet syngas temperature is more obvious. After the application of the silicon carbide refractory, the surface temperature of the membrane wall, especially the temperature of the wide fin parts, is greatly reduced. Moreover, the membrane wall is slightly deformed and warped due to the temperature difference between the two sides of the membrane wall.
机译:从夹带流动气化器诱导的高温合成气含有大量的显热量,其可以通过辐射合成气冷却器(RSC)有效地回收。在这项工作中,建立了RSC中的上锥形部分的膜壁模型。在不同的操作条件下的数值模拟探索膜壁和合成气之间的传热特性,并且通过流体 - 结构耦合方法计算膜壁表面上的热应力分布。结果表明,当没有保护膜壁的保护时,翅片的内表面被部分过热,并且最大应力超过材料的允许应力。入口合成气温度和流速的增加将增强上锥形膜壁的传热,并且入口合成气温度的效果更明显。在碳化硅耐火材料的施加之后,膜壁的表面温度,尤其是宽翅片部件的温度大大降低。此外,由于膜壁的两侧之间的温差,膜壁略微变形并翘曲。

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