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

单一压力容器镍氢电池组几何参数对其温度场的影响
引用本文:陈晓玲,张武高,陈飞,杨立.单一压力容器镍氢电池组几何参数对其温度场的影响[J].航空学报,2008,29(1):187-191.
作者姓名:陈晓玲  张武高  陈飞  杨立
作者单位:1. 上海交通大学,动力机械与工程教育部重点实验室,上海,200030
2. 上海交通大学,化学化工学院,上海,200030
摘    要: 针对实际空间用单一压力容器(IPV)镍氢电池组的传热特点,建立其瞬态热分析的数学物理仿真模型。通过设计改变电池组几何参数,包括电池组底板厚度、套筒高度和厚度,采用有限差分法,对比模拟研究电池组在飞船实际运行条件下几何参数对其温度场的影响。结果表明:套筒厚度对电池组温度场的影响最为敏感,增大套筒厚度可明显缩短电池组热系统达到平衡态的响应时间;其次是套筒高度;改变底板厚度对电池组温度场变化影响不明显。该研究为镍氢电池组的结构优化和热控制研究提供理论基础。

关 键 词:单一压力容器  镍氢电池组  数学物理模型  温度场  几何参数  
文章编号:1000-6893(2008)01-0187-05
修稿时间:2007年2月19日

Influence of Geometric Parameters of an Individual Pressure Vessel Ni-H2 Battery Group on the Temperature Field
Chen Xiaoling,Zhang Wugao,Chen Fei,Yang Li.Influence of Geometric Parameters of an Individual Pressure Vessel Ni-H2 Battery Group on the Temperature Field[J].Acta Aeronautica et Astronautica Sinica,2008,29(1):187-191.
Authors:Chen Xiaoling  Zhang Wugao  Chen Fei  Yang Li
Institution:1Key Laboratory for Power Machiner and Engineering of Ministry of Education, Shanghai Jiao Tong University 2School of Chemistry and Chemical Technology, Shanghai Jiao Tong University
Abstract:According to the heat transfer characteristics in the individual pressure vessel (IPV) Ni-H2 battery group, the mathematical and the physical model for the battery group was established and the finite differential method was adopted. By designing different geometric parameters for a practical individual pressure vessel Ni-H2 battery group, the temperature fields were compared under the working condition of spacecraft. The results show that the sleeve thickness is the most sensitive to the change of temperature. By increasing the thickness of sleeve, the response time is shortened when the battery group arrives the thermal equilibrium. The sleeve height is more sensitive to the temperature change. The influence of base thickness is not obvious. It is proposed to decrease the base thickness and increase the sleeve height and sleeve thickness as possible at the permit of structure and weight of the spacecraft.
Keywords:individual pressure vessel  Ni-H2 battery group  mathematical and physical models  temperature field  geometric parameter
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》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