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基于FDS的微重力条件下密闭舱细水雾灭火过程仿真分析

李文新 孙鹏 杨慎林

航天器环境工程2016,Vol.33Issue(5):505-509,5.
航天器环境工程2016,Vol.33Issue(5):505-509,5.DOI:10.3969/j.issn.1673-1379.2016.05.008

基于FDS的微重力条件下密闭舱细水雾灭火过程仿真分析

Simulation of fire fighting in airtight cabin under microgravity conditions based on the FDS

李文新 1孙鹏 1杨慎林2

作者信息

  • 1. 中国航天员中心,北京 100094
  • 2. 中国科学技术大学,合肥 230026
  • 折叠

摘要

Abstract

In this paper, simulation of the water mist is carried out by the fire dynamics software (FDS) to study the fire extinguishing process in the airtight cabin of a manned spacecraft under microgravity conditions. It is found that the water mist at a certain angle would not only promote the proliferation of the smoke, but also make the fire fighting operation difficult, because the fresh air would promote the combustion process. The temperature and the concentration of the carbon monoxide in the process of putting out the cable fire are obtained. Analysis shows that the particle size of the water mist in the gravity environment should be controlled between 100 and 150µm, and the spray direction should be perpendicular to the plane where the fire happens.

关键词

火灾动力学软件/载人航天器/灭火/微重力/细水雾

Key words

FDS/manned spacecrafts/fire extinguishment/micro-gravity/water mist

分类

建筑与水利

引用本文复制引用

李文新,孙鹏,杨慎林..基于FDS的微重力条件下密闭舱细水雾灭火过程仿真分析[J].航天器环境工程,2016,33(5):505-509,5.

基金项目

国家青年科研试验基金项目 ()

航天器环境工程

OACSTPCD

1673-1379

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