首页|航天器用水热管冻结特性数值模拟研究

航天器用水热管冻结特性数值模拟研究

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热管在空间探测工程中具有重要应用,是航天器的重要导热元件.文章通过引入毛细力动量源项的数值模拟方法,对水热管在设计工况和低功率工况下工作及可能的冻结过程进行数值模拟研究.结果表明:水热管在设计工况下工作时,蒸汽与液膜表面存在剪切作用,热管的温度沿轴向降低,轴向最大温差不超过 3 K,具有良好的等温性.低功率工况下,热管冷凝段的温度降低至工质的熔点以下,工质冻结沉积,低温区逐渐扩散至冷凝段末端,冻结沉积最终将吸液芯完全堵塞,导致热管失效,不再具有良好的等温性能和传热性能.研究结果可为热管的长期稳定运行设计提供参考依据,为空间探测工程的成功保障提供科学参考.
Numerical Simulation Study on Freezing Characteristics of Water Heat Pipe Used for Spacecraft
Heat pipes have important applications in space exploration project and are important thermal conductive elements of spacecraft.In this paper,by introducing the capillary momentum source term,the working characteristics and possible freezing process of a water heat pipe at de-sign and low power working conditions are numerically investigated.The results show that when the water heat pipe works at the design working condition,there is a shear effect on the surface of the vapor and the liquid film,and the temperature of the heat pipe decreases along the axial direc-tion,and the maximum temperature difference in the axial direction does not exceed 3 K,which has good isothermality.At the low power working condition,the temperature of the condenser section of the heat pipe reduces below the melting point of the working fluid.The working fluid is frozen and deposited,and the low temperature zone gradually spreads to the end of the con-denser section,where the frozen deposition finally blocks the wick.Thus,the heat pipe no longer maintains the isothermality and the heat transfer ability,resulting in failure.This study result provides a reference for the long-term stable operation design of heat pipe,and provides a scien-tific reference for the successful guarantee of space exploration project.

water heat pipe used for spacecraftlow power conditioncapillary flowfrozen deposi-tion

牟玉鹏、刘剑术、李小斌、张红娜、李凤臣、韩冶、王泽鸣、柴宝华

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天津大学 先进内燃动力全国重点实验室,天津 300350

天津大学 机械工程学院,天津 300350

中国原子能科学研究院,北京 102413

航天器用水热管 低功率工况 毛细流动 冻结沉积

2024

航天器工程
中国空间技术研究院总体部(北京空间飞行器总体设计部)

航天器工程

CSTPCD北大核心
影响因子:0.552
ISSN:1673-8748
年,卷(期):2024.33(1)
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