EXPERIMENTAL RESEARCH ON VERY HIGH-INTENSITY COMBUSTION IN HIGH-SPEED PREMIXED GAS FLOW

高速预混气流中极高强度燃烧的实验研究

基本信息

  • 批准号:
    63550054
  • 负责人:
  • 金额:
    $ 1.15万
  • 依托单位:
  • 依托单位国家:
    日本
  • 项目类别:
    Grant-in-Aid for General Scientific Research (C)
  • 财政年份:
    1988
  • 资助国家:
    日本
  • 起止时间:
    1988 至 1989
  • 项目状态:
    已结题

项目摘要

Very high-speed combustion or very high-intensity combustion would be possible in two types, which are the very intense turbulent flames and the detonations. Both types in premixed gases are generated from propagating flames. In the presence of obstacles in the combustible gas, the turbulence is produced by the induced flow. The turbulence will increase the transport of mass and energy and the area of flame front, leading to the increase in the rate of combustion reactions and, hence, to the enhancement of the pressure waves. All these effects to increase the burning rate depend on the induced flow velocity, which in turn depends on the burning rate itself. This relation is able to form a positive feedback system. Based on this idea, we found that the propagating flame can easily be accelerated even in fully unconfined gas mixtures when comb-shaped grids are placed repeatedly in the flame path.In the present research, we investigate the structures of the very high-speed deflagration an … More d the mechanisms of the transition to detonation. They are observed by schlieren framing or streak photographs, using a high-speed camera. The brightness of the flames is also observed at a point where the light emissions are measured by photocell system. The transient pressure waves are measured by piezoelectric pressure transducers. The combustible gases we used are the stoichiometric mixtures of methane, ethane or hydrogen with oxygen slightly diluted by nitrogen, argon or helium. Deflagration of any mixtures can be accelerated to any velocity by repeated obstacles. The noticeable accelerations of the flames are observed just after disappearing of the large eddies formed behind obstacles, or grid wires. The accelerating flames seen by schlieren framing photographs, look as fine grain which are much smaller than the scales of turbulence in the other burning regions. The fine and intense turbulent flames generate blast waves, as observed by pressure measurements. The mechanisms of the flame acceleration do not depend on the kind of mixtures we used. For any mixture the transition of deflagration to detonation does occur, but the onset of detonation of methane mixtures delays up to over 1000 m/s of flame speed. The very fast deflagration forms "shock + flame" structure. Less
非常高速的燃烧或非常高强度的燃烧可能有两种类型,即非常强烈的湍流火焰和爆炸。预混气体中的这两种类型都是由传播火焰产生的。在可燃气体中存在障碍物的情况下,诱导流产生湍流。湍流将增加质量和能量的传输以及火焰前缘的面积,从而导致燃烧反应速率的增加,并且因此导致压力波的增强。所有这些提高燃速的效果都取决于诱导流速,而诱导流速又取决于燃速本身。这种关系能够形成一个正反馈系统。基于这一思想,我们发现,即使在完全开放的混合气体中,当在火焰路径上重复放置梳状网格时,传播的火焰也很容易被加速。 ...更多信息 d的过渡到爆炸的机制。他们观察到的纹影框架或条纹照片,使用高速相机。火焰的亮度也被观察到在一个点,其中的光发射是由光电池系统测量。瞬态压力波由压电压力传感器测量。我们使用的可燃气体是甲烷、乙烷或氢气与氧气的化学计量混合物,氧气被氮气、氩气或氦气稍微稀释。任何混合物的爆燃都可以被重复的障碍物加速到任何速度。在障碍物或网格线后面形成的大涡流消失后,可以观察到火焰的明显加速。纹影分幅照片中看到的加速火焰看起来像是细颗粒,比其他燃烧区域的湍流尺度要小得多。精细而强烈的湍流火焰产生冲击波,正如压力测量所观察到的那样。火焰加速的机制不依赖于我们使用的混合物的种类。对于任何混合物的爆燃到爆震的过渡确实发生,但爆震的甲烷混合物的开始延迟超过1000米/秒的火焰速度。快速爆燃形成“激波+火焰”结构。少

项目成果

期刊论文数量(5)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
小川勇治・滝史郎: "メタン酸素混合気の開放空間中での火炎爆ごう遷移" 日本機械学会論文集(B編). 55. 1454-1457 (1989)
Yuji Okawa 和 Shiro Taki:“开放空间中甲烷-氧气混合物的火焰爆炸转变”日本机械工程师学会会刊(B 版)55。1454-1457(1989 年)。
  • DOI:
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    0
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  • 通讯作者:
Y. Ogawa and S. Taki: "Deflagration to Detonation in Methane/Oxygen Mixtures in Open Space" Transactions of The Japan Society of Mechanical Engineers. vol. B-55. 1454-1457 (1989)
Y. Okawa 和 S. Taki:“开放空间中甲烷/氧气混合物的爆燃到爆炸”日本机械工程师学会会刊。
  • DOI:
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    0
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Shiro,Taki: Progress in Astronautics Aeronautics. 114. 140-154 (1988)
Shiro,Taki:航天航空学的进展。
  • DOI:
  • 发表时间:
  • 期刊:
  • 影响因子:
    0
  • 作者:
  • 通讯作者:
滝史郎: 日本機械学会論文集. (1989)
Shiro Taki:日本机械工程师学会会议记录(1989)。
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TAKI Shiro其他文献

TAKI Shiro的其他文献

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{{ truncateString('TAKI Shiro', 18)}}的其他基金

Development of the Propulsion System Using Detonations
利用爆炸的推进系统的开发
  • 批准号:
    16360421
  • 财政年份:
    2004
  • 资助金额:
    $ 1.15万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
Study on Stabilization of Supersonic Combustion Using Ram Accelerator
冲压式加速器超音速燃烧稳定性研究
  • 批准号:
    12450394
  • 财政年份:
    2000
  • 资助金额:
    $ 1.15万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
STUDY ON THE COMBUSTION IN RAM ACCELERATOR
RAM加速器燃烧研究
  • 批准号:
    06452346
  • 财政年份:
    1994
  • 资助金额:
    $ 1.15万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
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