| Citation: | MIAO Jianlei, HU Bin, SHI Qiang, et al. Research on the influences of structural parameters of small slot wide evaporative fuel supply/flame stabilization integrated flameholder on lean ignition and lean blowout performance[J]. Journal of Aerospace Power, 2026, 41(2):20230788 doi: 10.13224/j.cnki.jasp.20230788 |
With the advantages of good flame stability and high total pressure recovery coefficient, the small slot wide evaporative fuel supply/flame stabilization integrated flameholder has a good application prospect in the afterburner of wide-range aspirated engine in the future. To investigate the influences of structural parameters on the performances of the flameholder lean ignition and lean blowout, the lean ignition and lean blowout test and cold state numerical simulation of the flameholder with different slot width and hole ratio were carried out in rectangular test section under the condition of air velocity of 40—115 m/s and air temperature of 573 K. The results showed that: (1) with the increase of the hole ratio, the number of vortices in the local recirculation increased, the fuel atomization and evaporation were enhanced, and the ignition and lean blowout fuel/air ratio of the combustion chamber decreased; (2) with the increase of incoming flow speed, the ignition and lean blowout fuel/air ratio of large hole ratio flameholder decreased first and then increased, and the ignition and lean blowout fuel/air ratio of small hole ratio flameholder decreased continuously; (3) with the increase of slot width, the size of vortex system in the local recirculation zone increased, the fuel atomization and evaporation were enhanced, and the ignition and lean blowout fuel/air ratio of the combustion chamber decreased.
| [1] |
刘晓波, 郭楚微. 国外吸气式组合动力的发展现状与趋势[C]//中国航天第三专业信息网第三十九届技术交流会暨第三届空天动力联合会议. 河南 洛阳: 中国空气动力研究与发展中心, 2018: 190-201. LIU Xiaobo, GUO Chuwei. Status and trend study on airbreathing combined cycle propulsion overseas[C]//The 39th Technical Exchange Conference and the 3rd Joint Conference on Aerospace Power of China Aerospace Third Professional Information Network. Luoyang Henan: China Aerodynamics Research and Development Center, 2018: 190-201. (in Chinese
LIU Xiaobo, GUO Chuwei. Status and trend study on airbreathing combined cycle propulsion overseas[C]//The 39th Technical Exchange Conference and the 3rd Joint Conference on Aerospace Power of China Aerospace Third Professional Information Network. Luoyang Henan: China Aerodynamics Research and Development Center, 2018: 190-201. (in Chinese)
|
| [2] |
ICHIMARU O, ISHIZUKA M, MURASHIMA K. Overview of the Japanese national project for super/hypersonic transport propulsion system[R]. ASME 92-GT-252, 1992.
|
| [3] |
THOMAS S. Overview of the turbine based combined cycle discipline[R]. NASA, 2009 Annual Meeting.
|
| [4] |
金莉, 谭永华. 火焰稳定器综述[J]. 火箭推进, 2006, 32(1): 30-34. JIN Li, TAN Yonghua. Study on flameholders[J]. Journal of Rocket Propulsion, 2006, 32(1): 30-34. (in Chinese
JIN Li, TAN Yonghua. Study on flameholders[J]. Journal of Rocket Propulsion, 2006, 32(1): 30-34. (in Chinese)
|
| [5] |
安帅, 林宇震, 张弛, 等. 离心力场下V型火焰稳定器火焰稳定性的研究[J]. 航空动力学报, 2009, 24(5): 1011-1015. AN Shuai, LIN Yuzhen, ZHANG Chi, et al. Characterization of flame stabilization for V-gutter in centrifugal force field[J]. Journal of Aerospace Power, 2009, 24(5): 1011-1015. (in Chinese doi: 10.13224/j.cnki.jasp.2009.05.010
AN Shuai, LIN Yuzhen, ZHANG Chi, et al. Characterization of flame stabilization for V-gutter in centrifugal force field[J]. Journal of Aerospace Power, 2009, 24(5): 1011-1015. (in Chinese) doi: 10.13224/j.cnki.jasp.2009.05.010
|
| [6] |
付藻群. 吸入式稳定器设计研究与试验[J]. 航空发动机, 1998, 24(3): 28-32. FU Zaoqun. Design, research and experiment of suction stabilizer[J]. Aeroengine, 1998, 24(3): 28-32. (in Chinese
FU Zaoqun. Design, research and experiment of suction stabilizer[J]. Aeroengine, 1998, 24(3): 28-32. (in Chinese)
|
| [7] |
杨阳, 马文杰, 樊未军, 等. 尾缘吹气稳定器缝宽对燃烧性能影响的试验[J]. 航空动力学报, 2008, 23(5): 858-864. YANG Yang, MA Wenjie, FAN Weijun, et al. Experimental on the effects of jet exit width on EBMC flameholders’ combustion performance[J]. Journal of Aerospace Power, 2008, 23(5): 858-864. (in Chinese doi: 10.13224/j.cnki.jasp.2008.05.012
YANG Yang, MA Wenjie, FAN Weijun, et al. Experimental on the effects of jet exit width on EBMC flameholders’ combustion performance[J]. Journal of Aerospace Power, 2008, 23(5): 858-864. (in Chinese) doi: 10.13224/j.cnki.jasp.2008.05.012
|
| [8] |
于文博, 范育新, 岳晨, 等. 一种蒸发式凹腔驻涡值班稳定器的流动与点火性能研究[J]. 推进技术, 2023, 44(5): 2206053. YU Wenbo, FAN Yuxin, YUE Chen, et al. Flow characteristics and ignition performance analysis of an evaporating cavity trapped vortex pilot flame-holder[J]. Journal of Propulsion Technology, 2023, 44(5): 2206053. (in Chinese doi: 10.13675/j.cnki.tjjs.2206053
YU Wenbo, FAN Yuxin, YUE Chen, et al. Flow characteristics and ignition performance analysis of an evaporating cavity trapped vortex pilot flame-holder[J]. Journal of Propulsion Technology, 2023, 44(5): 2206053. (in Chinese) doi: 10.13675/j.cnki.tjjs.2206053
|
| [9] |
杨开田. 航空发动机设计手册: 第11册 加力燃烧室[M]. 北京: 航空工业出版社, 2001.
|
| [10] |
金捷, 陈敏, 刘玉英, 等. 涡轮基组合循环发动机[M]. 北京: 国防工业出版社, 2019. JIN Jie, CHEN Min, LIU Yuying, et al. Turbine based combined cycle engine[M]. Beijing: National Defense Industry Press, 2019. (in Chinese
JIN Jie, CHEN Min, LIU Yuying, et al. Turbine based combined cycle engine[M]. Beijing: National Defense Industry Press, 2019. (in Chinese)
|
| [11] |
BELOVICH V, SAMIMY M. Mixing processes in a coaxial geometry with a central lobed mixer-nozzle[J]. AIAA Journal, 1997, 35(5): 838-841. doi: 10.2514/2.7455
|
| [12] |
王家骅. 蒸发式火焰稳定器的稳定机理研究[J]. 南京航空航天大学学报, 1980, 12(1): 69-84. WANG Jiahua. A mechanism of flame stabilization by means of vapour gutter in pre mixed flow[J]. Journal of Nanjing University of Aeronautics and Astronautics, 1980, 12(1): 69-84. (in Chinese
WANG Jiahua. A mechanism of flame stabilization by means of vapour gutter in pre mixed flow[J]. Journal of Nanjing University of Aeronautics and Astronautics, 1980, 12(1): 69-84. (in Chinese)
|
| [13] |
张斌. 航空发动机燃烧室点火模拟及特性研究[D]. 南京: 南京航空航天大学, 2014. ZHANG Bin. Ignition simulation and characteristics study of aero-engine combustion chamber[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014. (in Chinese
ZHANG Bin. Ignition simulation and characteristics study of aero-engine combustion chamber[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014. (in Chinese)
|
| [14] |
程晓军, 范育新, 王家骅. 薄膜蒸发稳定器在超级燃烧室内贫油点熄火特性[J]. 推进技术, 2015, 36(2): 246-252. CHENG Xiaojun, FAN Yuxin, WANG Jiahua. Performances of lean ignition and lean blowout with film evaporation flameholder in hyperburner[J]. Journal of Propulsion Technology, 2015, 36(2): 246-252. (in Chinese doi: 10.13675/j.cnki.tjjs.2015.02.012
CHENG Xiaojun, FAN Yuxin, WANG Jiahua. Performances of lean ignition and lean blowout with film evaporation flameholder in hyperburner[J]. Journal of Propulsion Technology, 2015, 36(2): 246-252. (in Chinese) doi: 10.13675/j.cnki.tjjs.2015.02.012
|
| [15] |
刘冉, 刘玉英, 高昭. 结构参数对蒸发式火焰稳定器贫油熄火性能的影响及其预测方法研究[J]. 推进技术, 2017, 38(12): 2753-2760. LIU Ran, LIU Yuying, GAO Zhao. Structural parameters effects on lean blowout performance and prediction method for piloted vaporization flameholder[J]. Journal of Propulsion Technology, 2017, 38(12): 2753-2760. (in Chinese doi: 10.13675/j.cnki.tjjs.2017.12.014
LIU Ran, LIU Yuying, GAO Zhao. Structural parameters effects on lean blowout performance and prediction method for piloted vaporization flameholder[J]. Journal of Propulsion Technology, 2017, 38(12): 2753-2760. (in Chinese) doi: 10.13675/j.cnki.tjjs.2017.12.014
|
| [16] |
冯玉桦, 刘玉英, 邓远灏, 等. 含湿量对蒸发式火焰稳定器贫油熄火性能的影响[J]. 航空动力学报, 2020, 35(9): 1866-1874. FENG Yuhua, LIU Yuying, DENG Yuanhao, et al. Effects of humidity ratio on lean blowout performance of piloted vaporization flameholder[J]. Journal of Aerospace Power, 2020, 35(9): 1866-1874. (in Chinese doi: 10.13224/j.cnki.jasp.2020.09.008
FENG Yuhua, LIU Yuying, DENG Yuanhao, et al. Effects of humidity ratio on lean blowout performance of piloted vaporization flameholder[J]. Journal of Aerospace Power, 2020, 35(9): 1866-1874. (in Chinese) doi: 10.13224/j.cnki.jasp.2020.09.008
|
| [17] |
金莉, 谭永华. 蒸发式火焰稳定器冷态流场计算[J]. 火箭推进, 2007, 33(1): 23-27. JIN Li, TAN Yonghua. Numerical prediction of cold flow field behind a vapor flameholder[J]. Journal of Rocket Propulsion, 2007, 33(1): 23-27. (in Chinese
JIN Li, TAN Yonghua. Numerical prediction of cold flow field behind a vapor flameholder[J]. Journal of Rocket Propulsion, 2007, 33(1): 23-27. (in Chinese)
|
| [18] |
陈亮任, 凌文辉. 低压下蒸发式稳定器结构对燃烧效率的影响[J]. 战术导弹技术, 2013(6): 66-73. CHEN Liangren, LING Wenhui. Influence of vaporizing flame holder structure on combustion efficiency at low pressure[J]. Tactical Missile Technology, 2013(6): 66-73. (in Chinese
CHEN Liangren, LING Wenhui. Influence of vaporizing flame holder structure on combustion efficiency at low pressure[J]. Tactical Missile Technology, 2013(6): 66-73. (in Chinese)
|
| [19] |
CHENG Xiaojun, FAN Yuxin. Experimental study of lean ignition and lean blowout performance improvement using an evaporation flameholder[J]. International Journal of Heat and Mass Transfer, 2016, 103: 319-326. doi: 10.1016/j.ijheatmasstransfer.2016.07.003
|
| [20] |
马文杰. 吸气式一体化喷油稳定器流动和燃烧性能研究[D]. 北京: 北京航空航天大学, 2008. MA Wenjie. Research on the flow and combustion performance of aspirated inside fuelling integrated flame holder[D]. Beijing: Beijing University of Aeronautics and Astronautics, 2008. (in Chinese
MA Wenjie. Research on the flow and combustion performance of aspirated inside fuelling integrated flame holder[D]. Beijing: Beijing University of Aeronautics and Astronautics, 2008. (in Chinese)
|
| [21] |
吴伟秋, 范育新, 缪俊杰, 等. 壁式与径向组合稳定器的流动与点火特性研究[J]. 推进技术, 2022, 43(7): 200969. WU Weiqiu, FAN Yuxin, MIAO Junjie, et al. Flow and ignition characteristics of wall combined with radial flame-holder[J]. Journal of Propulsion Technology, 2022, 43(7): 200969. (in Chinese doi: 10.13675/j.cnki.tjjs.200969
WU Weiqiu, FAN Yuxin, MIAO Junjie, et al. Flow and ignition characteristics of wall combined with radial flame-holder[J]. Journal of Propulsion Technology, 2022, 43(7): 200969. (in Chinese) doi: 10.13675/j.cnki.tjjs.200969
|
| [22] |
黄勇, 林宇震, 樊未军, 等. 燃烧与燃烧室[M]. 北京: 北京航空航天大学出版社, 2009.
|