平板热管性能优化及其在航天热控中的应用进展  

Application and development of flat heat pipe in spacecraft thermal control

作　　者：冷亚坤 张旭[2] 甄华龙 刘迎春[2] 王仲琦 蒲亮[1] LENG Yakun;ZHANG Xu;ZHEN Hualong;LIU Yingchun;WANG Zhongqi;PU Liang(School of Energy and Power Engineering,Xi'an Jiaotong University,Xi'an 710049,China;Innovation Academy for Microsatellites of Chinese Academy of Sciences,Shanghai 201304,China)

机构地区：[1]西安交通大学能源与动力工程学院,西安710049 [2]中国科学院上海微小卫星工程中心,上海201304

出　　处：《科技导报》2024年第24期46-57,共12页Science & Technology Review

基　　金：中国科学院上海微小卫星工程中心项目(202109158)。

摘　　要：平板热管具有传热效率高、均温性好、安全可靠等优点,已成为航天器热控的重要途径之一。吸液芯结构优化是提高平板热管流动传热性能的主要方式。在吸液芯结构设计方面,综述了高性能吸液芯结构设计方法,并分析了宏观-介观-微观多尺度数值模型的选择和应用。在吸液芯表面改性方面,探讨了提高纳米结构机械稳定性、调整传热机制和开展数值模拟研究的重要性。针对太空环境下高辐射和散热困难难题,展望了平板热管在航天器热控中的发展方向。Flat heat pipe,due to its advantages of high heat transfer efficiency,great temperature uniformity,and safety and reliability,has become one of the important options for spacecraft thermal control.Optimization of wick structure is an important method to improve the flow and heat transfer performance of flat heat pipe.For the design of wick structures,the method of designing high performance wick structures was revealed,and guidance was provided for the selection and application of macromeso-micro multiscale numerical model.For wick surface modification,the importance to improve nanostructure mechanical stability,adjust heat transfer mechanism and carry out numerical simulation research was emphasized.To solve the problems of heat dissipation and high radiation in space environment,the development directions of flat heat pipe in spacecraft thermal control were figured out,and the shortcomings of current research were analyzed.

关 键 词：平板热管 吸液芯 结构优化 多尺度 数值模型 

分 类 号：V444.36[航空宇航科学与技术—飞行器设计]