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effect of hydrogen addition and burner diameter on the stability and structure of lean, premixed flames.

机译:加氢和燃烧器直径对稀薄预混火焰的稳定性和结构的影响。

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摘要

Low swirl burners (LSBs) have gained popularity in heating and gas power generation industries, in part due to their proven capacity for reducing the production of NOx, which in addition to reacting to form smog and acid rain, plays a central role in the formation of the tropospheric ozone layer. With lean operating conditions, LSBs are susceptible to combustion instability, which can result in flame extinction or equipment failure. Extensive work has been performed to understand the nature of LSB combustion, but scaling trends between laboratory- and industrial-sized burners have not been established. Using hydrogen addition as the primary method of flame stabilization, the current work presents results for a 2.54 cm LSB to investigate potential effects of burner outlet diameter on the nature of flame stability, with focus on flashback and lean blowout conditions. In the lean regime, the onset of instability and flame extinction have been shown to occur at similar equivalence ratios for both the 2.54 cm and a 3.81 cm LSB and depend on the resolution of equivalence ratios incremented. Investigations into flame structures are also performed. Discussion begins with a derivation for properties in a multicomponent gas mixture used to determine the Reynolds number (Re) to develop a condition for turbulent intensity similarity in differently-sized LSBs. Based on this requirement, operating conditions are chosen such that the global Reynolds number for the 2.54 cm LSB is within 2% of the Re for the 3.81 cm burner. With similarity obtained, flame structure investigations focus on flame front curvature and flame surface density (FSD). As flame structure results of the current 2.54 cm LSB work are compared to results for the 3.81 cm LSB, no apparent relationship is shown to exist between burner diameter and the distribution of flame surface density. However, burner diameter is shown to have a definite effect on the flame front curvature. In corresponding flow conditions, a decrease in burner diameter results a broader distribution of curvature and an increased average curvature, signifying that compared to the larger 3.81 cm LSB, the flame front of the smaller burner contains tighter, smaller scale wrinkling.
机译:低涡流燃烧器(LSB)在供热和天然气发电行业中广受欢迎,部分原因是它们具有降低NOx产生的可靠能力,除了反应形成烟雾和酸雨外,NOx还在形成过程中发挥重要作用对流层臭氧层。在稀薄的工作条件下,LSB易受燃烧不稳定的影响,这可能导致火焰熄灭或设备故障。为了了解LSB燃烧的性质,已经进行了广泛的工作,但是尚未确定实验室和工业尺寸燃烧器之间的结垢趋势。使用加氢作为火焰稳定的主要方法,当前工作给出了一个2.54 cm LSB的结果,以研究燃烧器出口直径对火焰稳定性的潜在影响,重点是回火和稀薄吹气条件。在稀薄状态下,对于2.54 cm和3.81 cm LSB的当量比,不稳定和火焰熄灭的发生已显示出来,并且取决于当量比的分辨率提高。还对火焰结构进行了研究。讨论始于推导用于确定雷诺数(Re)的多组分气体混合物的性能,从而为不同尺寸LSB中的湍流强度相似性创造条件。根据此要求,选择工作条件,以使2.54厘米LSB的总雷诺数在3.81厘米燃烧器的Re的2%之内。在获得相似性的情况下,火焰结构研究集中于火焰前曲率和火焰表面密度(FSD)。将当前2.54厘米LSB工作的火焰结构结果与3.81厘米LSB的结果进行比较,表明燃烧器直径与火焰表面密度分布之间没有明显的关系。但是,燃烧器直径显示出对火焰前曲率有确定的影响。在相应的流动条件下,燃烧器直径的减小导致曲率分布更广,平均曲率增加,这表明与较大的3.81 cm LSB相比,较小的燃烧器的火焰前部包含更紧密,更小比例的起皱。

著录项

  • 作者

    Kaufman, Kelsey Leigh.;

  • 作者单位

    The University of Iowa.;

  • 授予单位 The University of Iowa.;
  • 学科 Mechanical engineering.;Aerospace engineering.
  • 学位 M.S.
  • 年度 2014
  • 页码 155 p.
  • 总页数 155
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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