A novel structure tube for supercritical CO2 turbulent flow with high non-uniform heat flux

被引:7
|
作者
Wang, Yan Juan [1 ]
Gao, Shuo [1 ]
Shi, Wei Jie [1 ]
Bin Liu, Qi [2 ,3 ]
Xu, Jin Liang [1 ]
机构
[1] North China Elect Power Univ, Beijing Key Lab Multiphase Flow & Heat Transfer, Beijing 102206, Peoples R China
[2] Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
[3] Univ Chinese Acad Sci, Beijing 100049, Peoples R China
基金
中国国家自然科学基金;
关键词
High non -uniform heat flux; Supercritical carbon dioxide; Thermal-fluid-mechanical coupling; Novel structure tube; CYCLE; IDENTIFICATION; COMBUSTION;
D O I
10.1016/j.ijheatmasstransfer.2023.124292
中图分类号
O414.1 [热力学];
学科分类号
摘要
Supercritical CO2 has been a promising alternative working medium in coal-fired power plants, high-temperature solar power systems, and fuel cells. In these cases, supercritical carbon dioxide is in a round tube under high temperature and pressure with high non-uniform heat flux. In this study, a novel struc-ture tube is proposed by optimizing the coupling between circumferential heat flux and tube thickness on the heat-absorbing side to improve its comprehensive performance. A thermal-fluid-mechanical cou-pling model was developed. The novel structure can reduce maximum temperature and temperature dif-ference effectively for the half-cycle uniform and non-uniform heat flux. The maximum thermal stress decreased by 23 and 29% and the maximum temperature decreased by 29.6 and 24.8 K for half-cycle uniform and non-uniform heat flux when the Eccentricity increased from 0 to 0.4. A comparison was made between the proposed structure, thin-walled tube, and traditional tube. Results showed that the performance of the proposed tube is the best. The maximum temperature decreases by approximately 55 K compared with the traditional and thin-walled tubes. The maximum equivalent stress of proposed tube is the smallest. Furthermore, the structure will improve the safety and economics of the tube. & COPY; 2023 Elsevier Ltd. All rights reserved.
引用
收藏
页数:11
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