三头部燃烧室点火过程中火焰传播特性研究
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作者单位:

1.南京航空航天大学能源与动力学院, 南京 210016;2.中国航空发动机集团有限公司湖南动力机械研究所, 株洲 412002

作者简介:

通讯作者:

李建中,男,教授,博士生导师, E-mail:ljzh0629@nuaa.edu.cn。

中图分类号:

V231.2

基金项目:


Study on Flame Propagation Characteristics of a Triple-dome Combustor During Ignition Process
Author:
Affiliation:

1.College of Energy and Power, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China;2.Hunan Aviation Powerplant Research Institute, Aero Engine Corporation of China, Zhuzhou 412002, China

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    摘要:

    为了探讨三头部燃烧室点火过程中的火焰传播特性,建立了矩形模型燃烧试验系统,开展了流动与点火过程中火焰传播特性、当量比对周向点火过程影响规律的研究。研究表明:初始火核主要在中心回流区边界形成,其传播过程具有阶段性,先顺流线方向进行传递,待燃烧强度增大到一定值后,火焰才开始向其他区域延伸;在相同压损下,当量比减小会使得燃烧室周向点火时间增加,主要为初始火焰发展阶段时间增加,当量比由0.89减小到0.6时,周向点火时间由33.5 ms增加到42 ms,流动加速系数由1.75增加到3.77,即随当量比减小,湍流褶皱等流动因素对火焰传播的加速效应增大;在初始火焰的发展阶段,气体热膨胀效应对火焰传播加速效应占主导作用。

    Abstract:

    A series of optical experiments were conducted to investigate the effect of flow filed on the flame ignition and propagation process between adjacent domes in triple-dome combustor. Results show that the initial fire core is formed mainly at the boundary of the recirculation zone, and the ignition process is staged. Initial flame core develops in the direction of local flow and it starts to propagate into other regions with the increase of combustion intensity. Under the same total pressure loss, the combustor’s circumference ignition time increases when the equivalence ratio decreases, especially in the time of the initial flame development. As the equivalence ratio decreases from 0.89 to 0.6, the circumference ignition time increases from 33.5 ms to 42 ms. During the circumferential ignition flame propagation, the coefficients of flow-induced acceleration increases with the decrease of equivalent ratio. When the equivalent ratio decreases from 0.89 to 0.6, the coefficients of flow-induced acceleration increases from 1.75 to 3.77, which means the turbulent wrinkle and other flow factors accelerate the flame propagation; in the initial flame development stage, the thermal expansion of gas dominates the flame propagation acceleration effect.

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冯剑寒,郎旭东,金武,任勇智,李建中.三头部燃烧室点火过程中火焰传播特性研究[J].南京航空航天大学学报,2021,53(1):150-157

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  • 收稿日期:2019-12-13
  • 最后修改日期:2020-01-26
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  • 在线发布日期: 2021-02-05
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