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Spark ignition and stability limits of spray kerosene flames under subatmospheric pressure conditions

机译:SupAtmospheric压力条件下喷雾煤油火焰的火花点火和稳定性限制

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摘要

Flame stability limits and ignition delay time of the flameholder are experimentally studied in this work at the pressure of 0.03 - 0.06 MPa, Mach number of 0.1 - 0.3, and temperature of 320 K - 800 K. The results indicate that the reduction in equivalence ratios of lean ignition and blowout can be achieved by the increase in pressure or Mach number. Temperature rise will first increase and then decrease the lean ignition equivalence ratio. While increasing lean blowout equivalence ratio was observed with increasing temperature. The envelope of the stable combustion between the pressure and Mach number is measured, and the lowest temperature of successful ignition is 300 K, acquired at Mach 0.1 and 0.06 MPa. Besides, the correlation between the equivalence ratios of flame stability and inlet parameters, such as pressure, Mach number, temperature, is developed. The ignition process of the flameholder is imaged, and the ignition delay time decreases with increased pressure or temperature. The ignition delay time is shown first to decrease and then increase with the increase in Mach number. (C) 2021 Elsevier Masson SAS. All rights reserved.
机译:燃烧者的火焰稳定性限制和点火延迟时间在这项工作中在0.03-0.06MPa,马赫数0.1-0.3的压力下进行实验研究,以及320k - 800k的温度。结果表明等效比率降低通过增加压力或马赫数来实现瘦点火和井喷。温度升高将首先增加,然后降低贫点点火等效率。随着温度的增加,观察到增加瘦井喷等效比。测量压力和马赫数之间的稳定燃烧的包络,并且成功点火的最低温度为300 k,在Mach 0.1和0.06MPa时获得。此外,开发了发育火焰稳定性和入口参数等等效比之间的相关性,例如压力,马赫数,温度。成像燃料符的点火过程,并且点火延迟时间随着压力或温度的增加而降低。首先显示点火延迟时间以减小,然后随着Mach数的增加而增加。 (c)2021 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2021年第7期|106734.1-106734.12|共12页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Jiangsu Peoples R China|Natl Univ Singapore Dept Mech Engn Singapore 117576 Singapore;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Jiangsu Peoples R China;

    Natl Univ Singapore Dept Mech Engn Singapore 117576 Singapore;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Jiangsu Peoples R China|Tsinghua Univ Inst Aero Engine Beijing 100084 Peoples R China;

    Natl Univ Singapore Dept Mech Engn Singapore 117576 Singapore;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Flameholder; Flame stability; Low pressure; Ignition delay; Lean blowout;

    机译:扑脱者;火焰稳定;低压;点火延迟;瘦井喷;

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