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Local extinction and near-field structure in piloted turbulent CH4/air jet flames with inhomogeneous inlets

机译:具有不均匀入口的引燃湍流CH4 /空气射流火焰中的局部熄灭和近场结构

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摘要

Line-imaged measurements of temperature and major species, based on well-established Raman/Rayleigh/CO-LIF techniques, are used to better understand the scalar structure of piloted CH4/air jet flames with inhomogeneous inlets. Recent studies using a variant of the Sydney piloted burner have demonstrated that the blowoff velocity of a partially-premixed jet flame of CNG or CH4 and air can be increased significantly by tailoring the mixture fraction profile at the burner exit. This is done by adding a small, retractable central tube within the main tube of the burner and separately supplying fuel and air for partial premixing. Both tubes are located within the pilot annulus. When the central tube is retracted far upstream of the burner exit, the flame has the same stability as that of the original burner with homogeneous fuel-air composition at the jet exit. However, when the inner tube supplies fuel and is retracted an optimal distance (10-13 times the main tube diameter) the blowoff velocity is increased by nearly 40%. Previous results indicated that combustion very close to the burner exit occurs in a stratified-premixed mode, augmenting the stabilizing effect of the pilot. This is followed by transition to a diffusion-dominated mode of burning within the first ten main tube diameters.
机译:基于成熟的拉曼/瑞利/ CO-LIF技术对温度和主要种类进行线成像测量,可用于更好地理解带有不均匀入口的飞行员CH4 /空气喷射火焰的标量结构。最近使用悉尼引燃式燃烧器的变体进行的研究表明,通过调整燃烧器出口处的混合比分布,可以大大提高CNG或CH4和空气的部分预混喷射火焰的吹气速度。这是通过在燃烧器的主管内增加一根小的,可伸缩的中心管,并分别供应燃料和空气来进行部分预混合来完成的。两个管都位于先导环内。当中心管缩回到燃烧器出口的上游时,火焰的稳定性与原始燃烧器的稳定性相同,原始喷射器的射流出口处的燃料-空气成分均匀。但是,当内管供油并缩回最佳距离(主管直径的10-13倍)时,吹扫速度将增加近40%。先前的结果表明,非常接近燃烧器出口的燃烧以分层预混合模式发生,从而增强了引燃器的稳定作用。接下来是在前十个主管直径内过渡到以扩散为主的燃烧模式。

著录项

  • 来源
    《Combustion and Flame》 |2015年第10期|3516-3540|共25页
  • 作者单位

    Sandia Natl Labs, Combust Res Facil, Livermore, CA 94550 USA;

    Univ Sydney, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia;

    Sandia Natl Labs, Combust Res Facil, Livermore, CA 94550 USA;

    Univ Sydney, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia;

    Univ Sydney, Sch Aerosp Mech & Mechatron Engn, Sydney, NSW 2006, Australia;

  • 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

    Turbulent flames; Multimode combustion; Partially-premixed flames; Local extinction;

    机译:湍流火焰;多模燃烧;部分预混火焰;局部熄灭;
  • 入库时间 2022-08-18 00:11:09

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