Investigation into the Effect of Structural Elements of the Entrance Section of a Fuel Assembly in the RITM Reactor on the Coolant Hydrodynamics in a Fuel-Rod Bundle

IF 1 Q4 ENERGY & FUELS
S. M. Dmitriev, T. D. Demkina, A. A. Dobrov, D. V. Doronkov, A. N. Pronin, A. V. Ryazanov, D. D. Kuritsin, D. S. Nikolaev
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Abstract

The results of experimental investigation into the coolant hydrodynamics within the entrance section of a fuel assembly in the core of the RITM reactor are presented. The investigation was aimed at capturing the effect of orifices and absorber grids of various designs on the development of the coolant flow in a fuel-rod bundle of a fuel assembly. To attain this goal, the experiments were performed in a scale model of the entrance section of the fuel assembly with all the structural elements of the standard assembly—from the throttle orifice to the second spacer grid. The spacing between model elements was increased by a scale factor equal to 5.8 relative to the standard spacing of their arrangement. The experiments were performed using two methods for investigating the coolant hydrodynamics: the pneumometric method and the tracer injection method. The studies were carried out at several cross-sections along the length of the model, and the studied region covered the entire cross-section of the model. The measurement sections were located considering the design features of the model. The hydraulic resistance coefficients (HRCs) of throttle orifices in fully open and maximally closed positions were experimentally determined. The features of the coolant flow at the inlet of the fuel assembly are visualized using maps of axial velocity distribution in the measurement sections as well as maps of injected tracer concentration distribution. A comparative analysis of the efficiency of application of two types of absorber grids was carried out. The experimental results were used to substantiate design solutions in modifying individual elements of the fuel assembly, as well as to confirm the reliability of new cores. In addition, the obtained experimental data can be used to validate the LOGOS CFD code developed in Russia.

Abstract Image

Abstract Image

RITM反应堆燃料组件入口段结构元件对燃料棒束内冷却剂流体动力学影响的研究
本文介绍了RITM反应堆堆芯燃料组件入口段冷却剂流体动力学的实验研究结果。调查的目的是捕捉不同设计的孔和吸收栅对燃料组件燃料棒束中冷却剂流动发展的影响。为了达到这一目标,实验在一个燃料组件入口部分的比例模型中进行,该模型包含了标准组件的所有结构元件——从节气口到第二间隔栅。模型元素之间的间距相对于其排列的标准间距增加了一个等于5.8的比例因子。实验采用气测法和示踪剂注入法两种研究冷却剂流体动力学的方法。研究在沿模型长度的多个横截面上进行,研究区域覆盖了模型的整个横截面。根据模型的设计特点对测量截面进行定位。实验确定了节流孔在全开和最大关闭位置的水力阻力系数。通过测量段的轴向速度分布图和注入示踪剂浓度分布图,可以直观地显示燃油组件入口冷却剂流动的特征。对比分析了两种吸收栅的应用效率。实验结果被用来证实修改燃料组件单个元件的设计方案,以及确认新堆芯的可靠性。此外,所获得的实验数据可用于验证俄罗斯开发的LOGOS CFD代码。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
1.30
自引率
20.00%
发文量
94
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