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Study of circular transverse jet - A new method for high-efficiency mixing and combustion in crossflow

机译:圆形横向射流的研究 - 一种新方法在横流中的高效混合和燃烧方法

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摘要

For traditional combustion chambers, when the working condition deviates from the design point, the combustion efficiency will be greatly reduced, and harmful products such as NOx, CO and UHC will increase greatly. This brings huge waste of fuel and air pollution. In order to improve the combustion efficiency at off-design conditions, in this paper a new method using a circular transverse jet as a means of fuel injection, fuel/air mixing and flame stabilization is explored, and an innovative configuration of transverse jet device is developed. Accordingly, the circular transverse jet is studied numerically and experimentally. It is found that the unique aerodynamic structure and high turbulence intensity of the circular transverse jet give an efficient mixing of the fuel and the mainstream along the fuel jet trajectory. Although the deviation of the total excess air coefficient is far from 1, a uniform mixture is formed in the recirculation zone downstream of the jet with an excess air coefficient approaching to 1. Experimental results show that the average excess air coefficient in the recirculation zone is about 1.29, and the combustion efficiency reaches more than 99% at the end of the recirculation zone when the overall excess air coefficient is 10.5, even under the low pressure and temperature conditions. These results demonstrate an effective improvement of the combustion efficiency at off-design conditions by the method proposed in this paper. In addition, the flow field structure under the interaction of circular transverse jet with mainstream, the distribution characteristics of gas components and temperature in the combustion zone are studied, which laid the foundation for the further study and the engineering application of this method.
机译:对于传统的燃烧室,当工作条件偏离设计点时,燃烧效率将大大降低,并且诸如NOx,CO和UHC之类的有害产品将大大增加。这带来了巨大的燃料和空气污染。为了提高在非设计条件下的燃烧效率,在本文中,探索了使用圆形横向射流作为燃料喷射,燃料/空气混合和火焰稳定的新方法,以及横向喷射装置的创新配置发达。因此,圆形横向射流在数字上和实验上进行了研究。结果发现,圆形横向射流的独特空气动力结构和高湍流强度可有效地混合燃料和沿燃料射流轨迹的主流。虽然总过量空气系数的偏差远非1,但是在射流下游的再循环区域中形成均匀的混合物,其具有过量的空气系数接近1.实验结果表明,再循环区的平均过量空气系数是大约1.29,当整个过量的空气系数为10.5时,燃烧效率在再循环区域的末端达到99%以上,即使在低压和温度条件下也是如此。这些结果表明,通过本文提出的方法,有效提高了在非设计条件下的燃烧效率。另外,研究了在圆形横向射流与主流的相互作用下的流场结构,研究了气体成分的分布特性和燃烧区中的温度,为进一步研究和这种方法的工程应用奠定了基础。

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  • 来源
    《International Communications in Heat and Mass Transfer》 |2021年第4期|105207.1-105207.12|共12页
  • 作者单位

    College of Jet Engines and Power Plants Kazan National Research Technical University Kazan 420111 Russia;

    Institute of Engineering Thermophysics Chinese Academy of Sciences Beijing 100190 China University of the Chinese Academy of Sciences Beijing 100490 China;

    Institute of Engineering Thermophysics Chinese Academy of Sciences Beijing 100190 China;

    College of Jet Engines and Power Plants Kazan National Research Technical University Kazan 420111 Russia;

    Osney Laboratory University of Oxford Oxford England 0X1 3PJ United Kingdom;

    Institute of Engineering Thermophysics Chinese Academy of Sciences Beijing 100190 China University of the Chinese Academy of Sciences Beijing 100490 China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Circular transverse jet; Excess air coefficient; Combustion efficiency; Recirculation zone; Mixing coefficient;

    机译:圆形横机;超空气系数;燃烧效率;再循环区;混合系数;

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