航天器环境工程
航天器環境工程
항천기배경공정
SPACECRAFT ENVIRONMENT ENGINEERING
2014年
3期
267-271
,共5页
赵建贺%张亚锋%石泳%俞进%王冉
趙建賀%張亞鋒%石泳%俞進%王冉
조건하%장아봉%석영%유진%왕염
载人航天器%密封舱%微重力%细水雾%灭火
載人航天器%密封艙%微重力%細水霧%滅火
재인항천기%밀봉창%미중력%세수무%멸화
manned spacecraft%sealed cabin%micro-gravity%water mist%fire extinguishment
为了研究微重力环境下细水雾灭火机理,利用FDS软件对细水雾雾化特征进行了仿真分析,结果表明:微重力环境有利于细水雾的形成和雾场的扩大,但由于没有重力场的作用而使得雾动量下降,导致雾滴穿透火焰的能力下降。通过对载人航天器密封舱内细水雾灭火的仿真计算,获得了火灾场特征位置处的温度及氧浓度(指体积分数)随时间变化规律,分析表明细水雾灭火不仅可以降低火焰的温度,而且还可通过稀释火灾场的氧浓度对火灾起到很好地抑制作用。
為瞭研究微重力環境下細水霧滅火機理,利用FDS軟件對細水霧霧化特徵進行瞭倣真分析,結果錶明:微重力環境有利于細水霧的形成和霧場的擴大,但由于沒有重力場的作用而使得霧動量下降,導緻霧滴穿透火燄的能力下降。通過對載人航天器密封艙內細水霧滅火的倣真計算,穫得瞭火災場特徵位置處的溫度及氧濃度(指體積分數)隨時間變化規律,分析錶明細水霧滅火不僅可以降低火燄的溫度,而且還可通過稀釋火災場的氧濃度對火災起到很好地抑製作用。
위료연구미중력배경하세수무멸화궤리,이용FDS연건대세수무무화특정진행료방진분석,결과표명:미중력배경유리우세수무적형성화무장적확대,단유우몰유중력장적작용이사득무동량하강,도치무적천투화염적능력하강。통과대재인항천기밀봉창내세수무멸화적방진계산,획득료화재장특정위치처적온도급양농도(지체적분수)수시간변화규률,분석표명세수무멸화불부가이강저화염적온도,이차환가통과희석화재장적양농도대화재기도흔호지억제작용。
A simulation model of water mist is established to study the fire extinguishment mechanism in case of a fire under the micro-gravity environment. Atomizing characteristics of the water mist are investigated under different gravity environments by the FDS. It is found that the spray momentum is reduced under the micro-gravity environment, but the scope of protection is increased. Numerical simulations of the fire being suppressed by the water mist in a typical manned spacecraft are carried out, and the temperature and the oxygen concentration against time are obtained. It turns out that the water mist can suppress the fire by flame cooling and oxygen dilution effectively.