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

空间站燃烧科学实验系统设计
引用本文:张振忠,孔文俊,张华良.空间站燃烧科学实验系统设计[J].空间科学学报,2020,40(1):72-78.
作者姓名:张振忠  孔文俊  张华良
作者单位:1. 中国科学院工程热物理研究所 北京 100190;
基金项目:中国载人航天工程计划燃烧科学实验系统项目;国家自然科学基金项目(U1738113)共同资助
摘    要:建立空间站燃烧实验系统,可满足未来空间微重力燃烧实验系统需求.通过空间站微重力燃烧实验研究,可拓展空间燃烧学研究.根据所要实现的功能及燃烧实验需求,对中国空间站燃烧柜的燃烧科学实验系统进行了设计和分析.燃烧科学实验系统由8个子系统组成,是一个适合开展气、液、固多种燃料燃烧实验的综合性实验系统.考虑到强度设计要求,在完成方案设计后,对系统进行了有限元分析,并在研制的结构件上进行了力学环境实验.实验与分析结果表明,本文设计的实验系统能够满足环模实验的要求,结构合理可行. 

关 键 词:微重力    燃烧科学实验系统    方案设计    力学环境实验
收稿时间:2019-10-26

Design of Combustion Science Experimental System for China Space Station
ZHANG Zhenzhong,KONG Wenjun,ZHANG Hualiang.Design of Combustion Science Experimental System for China Space Station[J].Chinese Journal of Space Science,2020,40(1):72-78.
Authors:ZHANG Zhenzhong  KONG Wenjun  ZHANG Hualiang
Institution:1 Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190;2 School of Engineering Sciences, University of Chinese Academy of Sciences, Beijing 100049;3 School of Astronautics, Beihang University, Beijing 100191
Abstract:In order to conduct the microgravity combustion experiments in China Manned Space Station,it is necessary to establish an onboard combustion science experiment system.With the experimental study of microgravity combustion,it is beneficial to expand the depth and breadth of combustion research and promote the development of combustion science.According to the functions to be realized and the requirements of combustion experiments,the design and analysis of the experimental system for combustion science rack are carried out.The combustion experiment system consists of eight subsystems,which is a comprehensive experiment system that is suitable for combustion experiments with gas,liquid and solid fuels,respectively.In consideration of the strength design requirements,after the completion of the scheme design,the finite element analysis of the system is carried out,and the mechanical environment experiment is completed with the developed structural setup.The experimental and analytical results show that the design can meet the requirements of the environment simulation experimental outline,and is reasonable and feasible for space experiments.
Keywords:Microgravity  Combustion science experimental system  Scheme design  Mechanical environment test
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《空间科学学报》浏览原始摘要信息
点击此处可从《空间科学学报》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