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首页> 外文期刊>Combustion and Flame >Multi-channel nanosecond discharge plasma ignition of premixed propane/air under normal and sub-atmospheric pressures
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Multi-channel nanosecond discharge plasma ignition of premixed propane/air under normal and sub-atmospheric pressures

机译:常压和负压下丙烷/空气预混合的多通道纳秒放电等离子体点火

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摘要

Relight of jet engines at high altitude is very difficult due to the relatively low pressure and temperature of inlet air. Currently, advanced ignition technology for high-altitude relight in jet engines is urgently needed. Successful ignition is achieved only when the ignition kernel can propagate outwardly beyond the so-called critical flame initiation radius. At high altitude with low pressure, the critical flame initiation radius becomes large and it cannot be easily reached by the ignition kernel. Therefore, in order to achieve successful ignition at low pressure conditions, large ignition kernel should be generated. In this study, plasma assisted ignition using multi-channel nanosecond discharge (MND) is proposed to induce a large ignition kernel and to achieve successful ignition at low pressures. Ignition experiments for propane/air mixtures at different equivalence ratios (Phi=0.8 similar to 1.6) and under normal and sub-atmospheric pressures (P=03 similar to 1.0 bar) were conducted in a constant volume combustion chamber. The performance of three ignition methods, spark discharge, single-channel nanosecond discharge (SND) and MND, were assessed; and the advantages of MND for ignition at sub-atmospheric pressures were demonstrated. The ignition kernel development, ignition probability, minimum ignition energy, and flame development for these three ignition methods (spark, SND and MND) were measured and compared. It was found that compared to spark and SND, MND can generate a much larger ignition kernel with stronger flame wrinkling and has much higher ignition probability, especially at low pressures. Therefore, MND has the advantage in achieving successful ignition at low pressure. Besides, it was shown that though the ignition kernel evolution and ignition probability strongly depend on ignition methods, the subsequent flame propagation is not greatly affected by ignition and there is little change in the flame rise time for different ignition methods. (C) 2017 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:由于进气的压力和温度相对较低,因此在高空重新喷射喷气发动机非常困难。当前,迫切需要用于喷气发动机的高空重燃的先进点火技术。只有当点火核能向外传播超过所谓的临界火焰起爆半径时,才能成功点火。在低压高空,临界火焰起爆半径变大,点火内核不易达到。因此,为了在低压条件下成功点火,应产生大的点火核。在这项研究中,提出了使用多通道纳秒放电(MND)的等离子辅助点火以诱导大点火核并在低压下成功点火。在恒定容积的燃烧室中进行了丙烷/空气混合物在不同当量比(Phi = 0.8,类似于1.6)以及常压和低于大气压(P = 03,类似于1.0 bar)下的点火实验。评估了三种点火方法的性能:火花放电,单通道纳秒放电(SND)和MND。并证明了MND在低于大气压下点火的优势。测量并比较了这三种点火方法(火花,SND和MND)的点火核发展,点火概率,最小点火能量和火焰发展。结果发现,与火花和SND相比,MND可以产生更大的点火核,具有更强的起皱纹,并且具有更高的点火概率,尤其是在低压下。因此,MND具有在低压下成功点火的优点。此外,结果表明,尽管点火核的演变和点火概率很大程度上取决于点火方法,但随后的火焰传播不受点火的影响很大,并且不同点火方法的火焰上升时间几乎没有变化。 (C)2017燃烧研究所。由Elsevier Inc.出版。保留所有权利。

著录项

  • 来源
    《Combustion and Flame》 |2017年第8期|102-113|共12页
  • 作者单位

    Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China|Xi An Jiao Tong Univ, Sci & Technol Plasma Dynam Lab, Xian 710049, Peoples R China;

    Xi An Jiao Tong Univ, Sci & Technol Plasma Dynam Lab, Xian 710049, Peoples R China;

    Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Peoples R China;

    Peking Univ, Coll Engn, Dept Mech & Engn Sci, SKLTCS, Beijing 100871, Peoples R China;

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

    Ignition; Multi-channel nanosecond discharge; Ignition kernel; Propane/air; Low pressure;

    机译:点火;多通道纳秒放电;点火核;丙烷/空气;低压;

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