首页 | 本学科首页   官方微博 | 高级检索  
     检索      

含相变材料热防护结构一体化设计与试验
引用本文:曹晨宇,王睿星,邢晓冬,宋宏伟,黄晨光.含相变材料热防护结构一体化设计与试验[J].宇航学报,2019,40(3):352-361.
作者姓名:曹晨宇  王睿星  邢晓冬  宋宏伟  黄晨光
作者单位:1. 哈尔滨工程大学机电工程学院,哈尔滨 150001; 2. 中国科学院力学研究所流固耦合系统力学重点试验室,北京 100190
基金项目:国防基础科研重点项目(JCKY2016130B009); 国家自然科学基金(91016025, 11472276, 11332011)
摘    要:利用相变材料储热密度大、比热容高等优势,设计了一种含相变材料的新型一体化热防护结构(PCM-ITPS),并通过数值计算分析了其隔热特性。结果表明,在一体化热防护结构底板处铺设相变材料可吸收热短路效应导入的过量热载,改善结构的隔热性能。然后设计并制备PCM-ITPS试验件,通过隔热性能测试试验对结构隔热特性进行验证。在此基础上进行热应力分析验证其承载性能,并以结构参数为设计变量,隔热和承载性能要求为约束条件,实现了PCM-ITPS结构的轻量化设计,优化后PCM-ITPS方案相对传统ITPS方案减重23.35%。以上工作为促进热防护系统的设计-制造一体化进程提供必要的理论储备与技术支持。

关 键 词:一体化热防护结构  隔热性能  热应力  定形相变材料  轻量化设计  
收稿时间:2018-07-30

Design and Experimental Investigation of Integrated Thermal Protection Structure Containing Phase Change Material Layer
CAO Chen yu,WANG Rui xing,XING Xiao dong,SONG Hong wei,HUANG Chen guang.Design and Experimental Investigation of Integrated Thermal Protection Structure Containing Phase Change Material Layer[J].Journal of Astronautics,2019,40(3):352-361.
Authors:CAO Chen yu  WANG Rui xing  XING Xiao dong  SONG Hong wei  HUANG Chen guang
Institution:1. School of Mechanical and Electrical Engineering, Harbin Engineering University, Harbin 150001, China; 2. Key Laboratory for Mechanics in Fluid Solid Coupling Systems, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
Abstract: This paper designs a new type of ITPS containing phase change material layer (PCM-ITPS). The numerical simulation is conducted to discuss the impact of the PCM on the thermal protection performance, and the PCM-ITPS unit cell test samples are manufactured to test the thermal protection performance. Both numerical simulation and test results prove the excellent thermal protection performance of the PCM-ITPS. On this basis, the thermal stress finite element simulation of the model is completed to verify its mechanical performance. Furthermore, the platform for the automatic design and optimization is built for the PCM-ITPS. With the structural dimensional parameters as the design parameters and the performance requirements as the constraints, the lightweight design of the integrated thermal structure is accomplished. As a result, the mass of the optimized PCM-ITPS is reduced by 23.35% compared with the optimized traditional ITPS. In conclusion, this work is able to provide the theoretical and technical support for the integrated design and manufacturing processes of a thermal protection system.
Keywords:Integrated thermal protection system  Thermal protection performance  Thermal stress analysis  Form-stable phase change material  Lightweight optimization design  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号