|国家科技期刊平台
首页|期刊导航|航天器工程|航天器用钾热管传热性能的敏感性分析和优化

航天器用钾热管传热性能的敏感性分析和优化OA北大核心CSTPCD

Optimization and Sensitivity Analysis of Heat Transfer Performance of Potassium Heat Pipe Used for Spacecraft

中文摘要英文摘要

碱金属热管在空间核电源系统中具有重要应用,是航天器辐射散热器的重要组件.文章研究钾热管对充液率、吸液芯层数、吸液芯丝网目数及热负载功率的敏感性,并对上述多参数耦合下钾热管传热性能进行优化.分析结果表明:钾热管温差随充液率和吸液芯丝网目数的增加而降低,随吸液芯层数和热负载功率的增加而升高,且钾热管的整体温度和蒸气流速随热负载功率的增加分别升高和降低.钾热管性能对吸液芯层数和热负载功率敏感,优化得到最优参数组合为充液率 1.0 时 7 层 350 目吸液芯和 712.475 W的热负载功率.文章采用的分析和优化方法对热管式辐射散热器的工程应用设计具有工程参考价值.

Alkali metal heat pipes have important applications in space nuclear power systems and are important components of the spacecraft radiant radiator.In this paper,the sensitivity of the potassium heat pipe to the liquid filling ratio,the count of layers and mesh of the wick and the thermal load power are investigated,and the heat transfer performance of the heat pipe with multi-parameter coupling is optimized.The analysis results show that the temperature difference of the heat pipe decreases with the increase of the liquid filling ratio and the mesh count,and in-creases with the increase of the count of wick layers and thermal load power.Moreover the overall temperature increases and the vapor velocity decreases with the increase of thermal load power.For potassium heat pipe,the count of wick layers and the thermal load power are sensitive to the heat transfer performance.The optimal combination of parameters obtained is 1.0 of liquid filling ratio,7 layers of 350 mesh wick and 712.475 W of thermal load power.The analysis and optimi-zation method adopted in this paper have engineering reference value for the design and optimiza-tion of heat pipe radiators.

韩冶;张亚坤;柴宝华;王泽鸣;牟玉鹏;刘剑术;姚良;李小斌;李凤臣

中国原子能科学研究院,北京 102413天津大学 机械工程学院,天津 300350||天津大学 先进内燃动力全国重点实验室,天津 300350

能源与动力

航天器用钾热管敏感性分析传热性能性能优化

potassium heat pipe used for spacecraftsensitivity analysisheat transfer perfor-manceperformance optimization

《航天器工程》 2024 (002)

48-54 / 7

10.3969/j.issn.1673-8748.2024.02.008

评论