Evaporation and Ignition of Liquid Fuels at Critical Pressure Regime.
Evaporation and Ignition of Liquid Fuels at Critical Pressure Regime.
批准号:
06452180
负责人:
NIIOKA Takashi
金额:
$2.56万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
1994
资助国家:
日本
项目状态:
已结题
起止时间:
1994 至 1996
中文摘要
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英文摘要
Ignition times of a fuel droplet were measured in a high-pressure high-temperature ambient. Suspended n-heptane, n-octane, n-decane, and n-hexadecane droplets with diameters of 0.35 to 1.4mm were quickly immersed in an electric furnace at temperatures up to 950. Attachment of a droplet, movement of the furnace and measurement of ignition were carried out in an air vessel with pressures from atmospheric pressure to over the critical pressure.Relatively long ignition times of small droplets measured under atmospheric pressure could not be observed at high pressures and the diameter below which a droplet does not ignite became smaller with pressure for every fuel used in this research. Ignition time decreased monotonously with pressure, and even at supercritical pressures, the ignition time behavior did not change much. Being different from the case of combustion, it is suggested that drastic change of properties did not take place in ignition processes. This is basically because the surf … More ace temperature of the droplet is much lower for droplet ignition phenomena in comparison with the droplet burning.At the second stage of the research, flame spread phenomena in a suspended fuel droplet array were investigated for n-decane and n-hexadecane in a high-pressure ambience. Seven droplets of the same size were arranged horizontally at equal spacings. Flame spread rates were measured based on OH emission histories detected by a high-speed video camera with an image intensifier for droplet diameters of 0.50,0.75, and 1.0mm at ambient pressure from 0.1 to 2.0MPa.Results showed that, as droplet spacing became smaller, flame spread rate increased and had a maximum value at a certain spacing. A further decrease in droplet spacing caused the spread rate to decrease due to the large latent heat of vaporization. Flame spread rate decreased with pressure and no flame spread was observed at the pressure over the critical pressure. This is due to the rapid decrease in flame diameter with pressure. Less
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R.Nakanishi: "Ignition Experiment of a Fuel Droplet in High-Pressure High-Temperature Ambient" Twenty-fifth Symposium (International) Ignition on Combustion, The Combustion Institute. 447-453 (1994)
R.Nakanishi:“高压高温环境中燃料滴的点火实验”第二十五届(国际)燃烧点火研讨会,燃烧研究所。
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R.Nakanishiほか: "Ignition Experiment of a Fuel Droplet in High-Pressure High-Temperature Ambient" Twenty-fifth Symposium (Int.) on Combustion. 25. 447-454 (1995)
R. Nakanishi 等人:“高压高温环境中燃料液滴的点火实验”第二十五届燃烧研讨会(国际)25. 447-454 (1995)。
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Niioka Takashi: "Ignition Experiment on Droplet Array in Normal and Microgravity Environments" IUTAM Symposium on the Mechanics and Combustion of Droplets and Sprays. 367-377 (1994)
Niioka Takashi:“正常和微重力环境下液滴阵列的点火实验”IUTAM 液滴和喷雾的力学和燃烧研讨会。
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Kato Shinichiro: "Flame Spread Experiment of a Fuel Droplet Array in High Pressure Ambience" Third KSME-JSME Thermal Engineerirg Conference Kyongju,KSME-JSME. 263-268 (1996)
加藤真一郎:“高压环境下燃料液滴阵列的火焰传播实验”第三届 KSME-JSME 热工会议 庆州,KSME-JSME。
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加藤 伸一郎: "微小重力場における燃料液滴列の燃え拡がり実験" 日本マイクログラビティー応用学会誌. 第13巻4号. 263-268 (1996)
加藤信一郎:“微重力场中燃料液滴阵列的火焰传播实验”日本微重力应用学会杂志,第 13 卷,第 4 期,263-268(1996 年)。
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共 17 条
Study of the Effect of Shock Wave on Fuel Injection and Combustion
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批准号:14350505
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$9.15万
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财政年份:2002
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负责人:NIIOKA Takashi
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依托单位:
Research and Development of Two-staged Combustion Strut with Air Intake
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批准号:10555332
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$1.92万
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财政年份:1998
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负责人:NIIOKA Takashi
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依托单位:
CLALIFICATION OF FUNDAMENTAL PHENOMENA ON NON-EMISSION BURNING OF CO_2AND NOx
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批准号:10450078
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项目类别:Grant-in-Aid for Scientific Research (B).
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资助金额:$5.31万
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财政年份:1998
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负责人:NIIOKA Takashi
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依托单位:
Research and Development of Supersonic Combustion Strut with a Preburner
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批准号:07555678
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$2.11万
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财政年份:1995
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负责人:NIIOKA Takashi
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依托单位:
DEVELOPMENTAL SCIENTIFIC RESEARCH ON CERAMIC CONTROLLABLE-STRUT FOR SUPERSONIC COMBUSTION
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批准号:05555258
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项目类别:Grant-in-Aid for Developmental Scientific Research (B)
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资助金额:$4.16万
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财政年份:1993
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负责人:NIIOKA Takashi
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依托单位:
海外基金