Experimental Investigation on combustion characteristics of DME lean side mixtures under micro-gravity
Experimental Investigation on combustion characteristics of DME lean side mixtures under micro-gravity
批准号:
16560196
负责人:
OKAJIMA Satoshi
金额:
$2.02万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2004
资助国家:
日本
项目状态:
已结题
起止时间:
2004 至 2007
中文摘要
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英文摘要
Experiments have been carried out to elucidate the fundamental combustion characteristics of DME fuel-air mixtures. The main results obtained for the study are as follows that, for the measurement of burning velocity on DME fuel-air mixtures using microgravity technique, □The micro-gravity technique is the most suitable method to extract the essential combustion characteristics of DME fuel-air mixtures, especially, near the very lean side of mixtures, The burning velocity of DME fuel-air mixtures monotonically decreases with decre4asing equivalence ratio and these values are nearly the same with those4 of methane-air mixtures at all the equivalence ratios studied, for instance the burning velocity is 44.2cm/s and 16.5cm/s, respectively, at equivalence of 1.1 and 0.65 under room temperature and atmospheric pressure and □The decrease of burning velocity of lean side of DME fuel-air mixtures is larger than that of rich side of mixtures, for the fundamental analysis an combustion behavior … More of DME laminar premixed burner flames, The burning velocity of DME premixed flames is approximately 34cm/s at 1.0 of equivalence ratio. As comparison of the burning velocity of DME with those of methane and propane-air mixture, the burning velocity of propane-air mixtures are larger than those of DME-air mixture and DME-air mixture are larger than methane-air mixtures. The blow off velocity and flashback velocity of DME are always larger than those of methane. □The stable region of the flame is easily to examine by the boundary velocity gradients(g). In case of circular tube laminar flow, the boundary velocity gradients can be expressed as g=4V/πR^3. Where V is the volume flow rate and R is the burner radius. Combustion of DME fuel-air mixtures is more stable than that of methane-air mixtures. In this study, we have tried to obtain the lower flammability limit using the burner method with the flame histories. The lower flammability limits of DME-air premixed flame obtained by this method are approximately Φ=0.34 and that of methane-air premixed flame are approximately Φ=0.55. From these data it may be predicted that the application to the engine combustion of DME is an effective alternative fuel for the future and, for measurement of quenching distance on combustion of DME fuel-air mixtures by flat flame propagation method, (1) Both of the quenching distance of DME fuel-air mixtures measuring by parallel plate and circular tube increase with decreasing equivalence ratio and these values are almost identical with the corresponding value for methane-air and propane-air mixtures. □The relationship between the quenching distance of parallel plate L_q, and circular tube d_q may be expressed by L_q=0.65・d_q. (3) The effect of buoyancy makes flame propagation speed increase and quenching distance decrease in upward flame propagation. (4) The quenching distance also depends on the ratio of surface area S to internal volume V of cylindrical long tube and the quenching distance becomes smaller as the S/V decreases.From these experimental data it may be predicted that the application to the engine combustion of DME fuel is not impossible. Less
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同軸流拡散火炎を用いてのDME燃料の燃焼特性の解明に関する研究
同轴扩散火焰阐明二甲醚燃料燃烧特性的研究
DOI:
--
发表时间:
2005
期刊:
日本機械学会東北支部第41期講演会・講演論文集
影响因子:
--
作者:
[岡島 敏, 細矢豊]
通讯作者:
細矢豊
微小重力下における高圧雰囲気中でのDME-空気混合気の燃焼特性の解明に関する研究
微重力高压气氛下二甲醚-空气混合物燃烧特性解析研究
DOI:
--
发表时间:
2006
期刊:
第44回燃焼シンポジウム・日本燃焼学会
影响因子:
--
作者:
[岡島敏, 山本和信]
通讯作者:
山本和信
DME燃料の同軸流拡散火炎における燃焼観察と燃焼特性の解明に関する研究
DME燃料同轴扩散火焰燃烧观察及燃烧特性研究
DOI:
--
发表时间:
2005
期刊:
影响因子:
--
作者:
[岡島 敏, 細矢 豊]
通讯作者:
細矢 豊
DME拡散火炎間燃え移り現象の観察
DME扩散火焰间燃尽现象的观察
DOI:
--
发表时间:
2007
期刊:
日本機会学会2006年度関東支部第13期総会講演会・日本機械学会
影响因子:
--
作者:
[岡島敏, 河合良樹]
通讯作者:
河合良樹
Combustion Characteristics at Lean Side of DME-Propane-Air Mixtures Using Microgravity Technique
利用微重力技术研究二甲醚-丙烷-空气混合物稀侧的燃烧特性
DOI:
--
发表时间:
2006
期刊:
Thirty-First International Symposium on Combustion, The Combustion Institute
影响因子:
--
作者:
[S.Okajima, A.Nakamura]
通讯作者:
A.Nakamura
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