Features of forming a coolant flow in the inlet section of the fuel cartridge for a RITM small nuclear power plant

IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Thermophysics and Aeromechanics Pub Date : 2025-03-12 DOI:10.1134/S0869864324040012
S. M. Dmitriev, T. D. Demkina, A. A. Dobrov, D. V. Doronkov, D. S. Doronkova, M. A. Legchanov, A. N. Pronin, A. V. Ryazanov, D. N. Solntsev
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Abstract

The paper presents the results of an experimental study on coolant flow patterns at the inlet section of a fuel assembly (FA) in the cartridge core of a reactor for a RITM small nuclear power plant. The objective was a study on influence of different inlet elements on the coolant axial velocity distribution. This task was performed by a series of experiments on a scale-up experimental model covering the inlet section components from the calibration washer up to the attachment unit between fuel rods and the diffuser. The model also covers the section of the fuel-element bundle between the absorbing grid and the spacer grid. This study is based on the pneumometric method for several critical cross sections over the model length. The allocation of measuring points covers the entire cross section of the model. The coolant flow features are visualized using digital maps for the working medium flow axial velocity in the fuel rod bundle cross section. The experimental modeling can be useful for optimizing the hydraulic profiling of the components at the inlet of the fuel rod assembly. The set of test data can be applied for validation of the LOGOS CFD software and for adjusting the technique of heat and fluid computations for the core zones under a cell approximation.

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RITM小型核电站燃料包入口段冷却液流形成的特点
本文介绍了RITM小型核电站堆芯燃料组件进口段冷却剂流动特性的实验研究结果。目的是研究不同进口元件对冷却剂轴向速度分布的影响。这项任务是通过在一个放大实验模型上进行的一系列实验来完成的,该模型涵盖了从校准垫圈到燃料棒和扩散器之间的连接单元的入口部分组件。该模型还涵盖了燃料元件束在吸收栅和间隔栅之间的部分。本研究是基于模型长度上几个临界截面的气动测量方法。测点的分配覆盖了模型的整个横截面。在燃料棒束截面上,使用工质流轴向速度的数字图来可视化冷却剂的流动特征。实验模型可用于优化燃料棒组件入口部件的水力剖面。该测试数据集可用于验证LOGOS CFD软件,并可用于调整单元近似下核心区的热流体计算技术。
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
Thermophysics and Aeromechanics
Thermophysics and Aeromechanics THERMODYNAMICS-MECHANICS
CiteScore
0.90
自引率
40.00%
发文量
29
审稿时长
>12 weeks
期刊介绍: The journal Thermophysics and Aeromechanics publishes original reports, reviews, and discussions on the following topics: hydrogasdynamics, heat and mass transfer, turbulence, means and methods of aero- and thermophysical experiment, physics of low-temperature plasma, and physical and technical problems of energetics. These topics are the prior fields of investigation at the Institute of Thermophysics and the Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences (SB RAS), which are the founders of the journal along with SB RAS. This publication promotes an exchange of information between the researchers of Russia and the international scientific community.
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