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载人航天器密封舱内火灾流场特性数值研究

赵建贺 王冉 俞进 石泳 赵新攀

航天器环境工程Issue(6):610-615,6.
航天器环境工程Issue(6):610-615,6.DOI:10.3969/j.issn.1673-1379.2013.06.009

载人航天器密封舱内火灾流场特性数值研究

Numerical simulation on fire in sealed cabin of manned spacecraft

赵建贺 1王冉 1俞进 1石泳 1赵新攀1

作者信息

  • 1. 中国空间技术研究院 载人航天总体部,北京 100094
  • 折叠

摘要

Abstract

A sealed cabin model was established to obtain flow-field distribution laws in case of a fire in manned spacecraft under micro-gravity environment. FDS software was used to simulate fires under different location and ventilation. The distribution of smoke temperature and soot density were gained. The results can be a reference for installation of fire detectors in sealed cabins.

关键词

载人航天器/密封舱/微重力/火灾/流场/仿真研究

Key words

manned spacecraft/sealed cabin/micro-gravity/fire/flow-field/simulation study

分类

资源环境

引用本文复制引用

赵建贺,王冉,俞进,石泳,赵新攀..载人航天器密封舱内火灾流场特性数值研究[J].航天器环境工程,2013,(6):610-615,6.

基金项目

国家重大科技专项工程 ()

航天器环境工程

OACSTPCD

1673-1379

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