基于引导气体和值班煤油的ATR发动机蒸发式火焰稳定器火焰动态特性研究

  • 孟祥韬 ,
  • 刘秋月 ,
  • 王中华 ,
  • 胡斌 ,
  • 曾文 ,
  • 赵庆军
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  • 1. 沈阳航空航天大学
    2. 南京理工大学
    3. 中国科学院工程热物理研究所

收稿日期: 2026-01-29

  修回日期: 2026-03-28

  网络出版日期: 2026-04-02

Study on flame dynamic characteristics of evaporative flameholder for ATR engine based on guided gas and pilot kerosene

  • MENG Xiang-Tao ,
  • LIU Qiu-Yue ,
  • WANG Zhong-Hua ,
  • HU Bin ,
  • ZENG Wen ,
  • ZHAO Qing-Jun
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Received date: 2026-01-29

  Revised date: 2026-03-28

  Online published: 2026-04-02

摘要

为探究空气涡轮火箭(Air Turbo Rocket,ATR )发动机燃烧室蒸发式火焰稳定器在引导乙烯和值班煤油共同作用下火焰的动态特性,以模型蒸发式火焰稳定器为研究对象,在常温、常压条件下,开展了不同引导乙烯量、值班煤油流量下的火焰动态特性燃烧实验。实验结果表明:1)高当量比状态下,引导乙烯的脉动区域主要集中在火焰稳定器的下游区域,且火焰的动态特性主要受冯卡门(Bénard-von Kármán,BVK)不稳定性影响;切断引导乙烯,值班煤油独立工作时,火焰的动态特性主要以体积振荡以及火焰的轴向脉动为主;当引导乙烯与值班煤油同时工作时,在V型槽内的火焰动态特性主要受燃烧热释放引发的体积振荡影响,在火焰稳定器尾缘剪切层附近的火焰动态特性主要受开尔文 - 亥姆霍兹(Kelvin–Helmholtz,KH)不稳定不稳定性影响。2)当引导乙烯当量比较小时,在火焰稳定器尾缘附近的火焰的动态特性主要受KH不稳定性影响,随着当量比的增大,燃烧区域逐渐向火焰稳定器下游移动,主导因素由KH不稳定性变为BVK不稳定性。3)引导乙烯流量为2g/s,值班煤油燃空比从0.0034增加到0.0085时对火焰稳定器火焰的动态特性影响较小,并且频率维持不变。稳定器后存在局部最佳燃空比,当超过局部最佳燃空比时继续增加值班煤油,会导致局部富油从而抑制火焰的放热脉动。

本文引用格式

孟祥韬 , 刘秋月 , 王中华 , 胡斌 , 曾文 , 赵庆军 . 基于引导气体和值班煤油的ATR发动机蒸发式火焰稳定器火焰动态特性研究[J]. 航空学报, 0 : 1 -0 . DOI: 10.7527/S1000-6893.2026.33433

Abstract

To investigate the flame dynamic characteristics of an evaporative flameholder in the combustion chamber of an Air Turbo Rocket (ATR) engine under the combined effects of guided ethylene and duty kerosene, a model evaporative flameholder was used as the experiment. Combustion experiments were conducted at room temperature and atmospheric pressure to examine the flame dynamics under different flow rates of guided ethylene and duty kerosene. The experimental results show that : 1) Under high equivalence ratio conditions, the pulsation zone guiding ethylene is primarily concentrated in the downstream region of the flameholder, and the dynamic characteristics of the flame are mainly influenced by Bénard-von Kármán (BVK) instability; When the ethylene supply is cut off and the kerosene burner operates independently, the flame dynamics are primarily characterized by volumetric oscillations and axial pulsations;When guided ethylene and duty kerosene are operated simultaneously, the flame dynamics within the V-shaped channel are primarily influenced by volume oscillations induced by heat release from combustion. Near the shear layer at the trailing edge of the flameholder, flame dynamics are predominantly affected by Kelvin–Helmholtz (KH) instability. 2) When the guided ethylene equivalence ratio is relatively low, the dynamic characteristics of the flame near the trailing edge of the flameholder are primarily influenced by KH instability. As the equivalence ratio increases, the combustion zone gradually shifts downstream along the flameholder, and the dominant factor transitions from KH instability to BVK instability. 3) When the guided ethylene flow rate is set to 2 g/s, increasing the duty kerosene fuel-air ratio from 0.0034 to 0.0085 has a negligible effect on the dynamic characteristics of the flameholder flame, and the frequency remains unchanged. A local optimum fuel-air ratio exists downstream of the flameholder. Continuing to add duty kerosene beyond this local optimum ratio will cause local fuel enrichment, thereby suppressing the flame's heat release pulsation.

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