两点火源顺序点火起爆爆震波的数值研究 *

推进技术 ›› 2014, Vol. 35 ›› Issue (10): 1434-1440.

• 新型动力 • 上一篇

两点火源顺序点火起爆爆震波的数值研究 *

王治武¹,陈星谷²,郑龙席¹,卢　杰¹,彭畅新²

西北工业大学动力与能源学院，陕西西安 710072;中国航空动力机械研究所，湖南株洲 412002;西北工业大学动力与能源学院，陕西西安 710072;西北工业大学动力与能源学院，陕西西安 710072;中国航空动力机械研究所，湖南株洲 412002

发布日期:2021-08-15
作者简介:王治武(1981—)，男，博士，副教授，研究领域为燃烧学、流体力学等。
基金资助:
国家自然科学基金(51306153)；高等学校博士学科点专项科研基金新教师类资助课题(20116102120027)；陕西省自然科学基金(2014JM7258)；西北工业大学基础研究基金(NPU-FFR-JCY20130129)。

Numerical Investigation of Two Successive Ignitions Effect on Detonation Initiation

School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China;China Aviation Powerplant Research Institute，Zhuzhou 412002，China;School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China;School of Power and Energy，Northwestern Polytechnical University，Xi’an 710072，China;China Aviation Powerplant Research Institute，Zhuzhou 412002，China

Published:2021-08-15

摘要/Abstract

摘要： 为了研究两点火源顺序点火对爆震起爆的影响，对单点火源以及不同间距、不同点火间隔时间的两点火源点火起爆过程进行了数值模拟。采用恰当比的丙烷/空气为可爆混合物。计算结果表明，在单个点火源不能起爆爆震波时，在其下游一定距离的位置增加一个相同能量的点火源并在适当的点火间隔时间下顺序点火可以起爆爆震波；两个点火源的距离一定时，点火间隔时间需在一定范围内才能成功起爆爆震波；当点火源距离从50mm增加到150mm时，成功起爆爆震波的点火间隔时间的范围从10μs减小到0.5μs。

关键词: 起爆；顺序点火；点火间隔时间；点火距离；脉冲爆震发动机

Abstract: In order to investigate the effect of two successive ignitions on the characteristics of detonation initiation，the detonation initiation process was numerically simulated by CFD software. The processes of detonation initiation by one ignition and two successive ignitions with different distances and different ignition interval time were simulated and analyzed. Stoichiometric propane-air mixture was used as the fuel-oxidant. The simulation and analysis results indicate that the detonation wave in the detonation tube can not be initiated by one single ignition，but can be initiated when the successive second ignition with the same energy is added in the downstream and is ignited at the appropriate interval time. When the distance between the two ignitions is constant，the detonation wave can be initiated successfully by the two ignitions with a certain range of ignition interval time. When the distance between the two ignitions increases from 50 mm to 150 mm，the range of the ignition interval time decreases from 10μs to 0.5μs，with which detonation can be initiated.

Key words: Detonation initiation；Successive ignitions；Ignition interval time；Ignition distance；Pulse detonation engine

王治武,陈星谷,郑龙席,卢　杰,彭畅新. 两点火源顺序点火起爆爆震波的数值研究 *[J]. 推进技术, 2014, 35(10): 1434-1440.

WANG Zhi-wu¹,CHEN Xing-gu²,ZHENG Long-xi¹,LU Jie¹,PENG Chang-xin². Numerical Investigation of Two Successive Ignitions Effect on Detonation Initiation[J]. Journal of Propulsion Technology, 2014, 35(10): 1434-1440.

参考文献

[1] Fan W, Yan C J, Huang X Q, et al. Experimental Investigation on Two-Phase Pulse Detonation Engine [J]. Combustion and Flame, 2003, 133(4): 441-450.
[2] 王治武, 严传俊, 范玮, 等. 脉冲爆震发动机的点火-起爆性能[J]. 燃烧科学与技术, 2009, 15(5).
[3] 韩启祥, 王家骅, 王波. 预混气爆震管中爆燃到爆震转捩距离的研究[J].推进技术, 2003, 24(1) : 63-66.(HAN Qi-xiang, WANG Jia-hua, WANG Bo. Investigation of Deflagration to Detonation Transition Distance in a Tube with Mixture[J]. Journal of Propulsion Technology, 2003, 24(1): 63-66.)
[4] Chao J, Otsukab T , Lee J H S. An Experimental Investigation of the Onset of Detonation [J]. Proceedings of the Combustion Institute, 2005, 30: 1889-1897.
[5] Brophy C M, Sinibaldi J O, Damphousse P. Initiator Performance for Liquid Fueled Pulse Detonation Engines [R]. AIAA 2002-0472.
[6] 王治武, 严传俊, 郑龙席, 等. 预爆管起爆扇形爆震室试验研究[C]. 北京: 第二届爆轰与爆震发动机研讨会摘要集, 2011.
[7] Zel’dovich, Ya B, Kompaneets A S. The Theory of Detonation [M]. Moscow : Gostekhteorizdat, 1955.
[8] 曾昊, 何立明, 章雄伟, 等. 环形射流喷口位置对激波聚焦起爆的影响分析 [J]. 推进技术, 2011, 32(3): 437-442.(ZENG Hao, HE Li-ming, ZHANG Xiong-wei, et al. Investigation on the Influence of Jets Spout Location on Detonation Initiation Via Imploding Annular Shock Waves[J]. Journal of Propulsion Technology, 2011, 32(3):437-442.)
[9] 王治武, 陈星谷, 郑龙席, 等. 横向射流起爆爆震波数值研究[J]. 推进技术, 2013, 34(3): 422-427.(WANG Zhi-wu, CHEN Xing-gu, CHENG Long-xi, et al. Numerical Investigation of the Transverse Jet Effects on Detonation Initiation Characteristics[J]. Journal of Propulsion Technology, 2013, 34(3):422-427.)
[10] Frolov S M, Basevich V Ya, Aksenov V S, et al. Spray Detonation Initiation by Controlled Triggering of Electric Dischargers [J].Journal of Propulsion and Power, 2005, 21(1): 54-64.
[11] 徐胜利, 张红杰, 岳朋涛, 等. 管道内运动火焰生成压力波及其特性的研究[J]. 中国科学技术大学学报, 2000, 30(4): 387-392.
[12] Frolov S M, Basevich V Ya, Aksenov V S, et al. Optimization Study of Spray Detonation Initiation by Electric Discharges [J]. Shock Waves, 2005, 14(3): 175-186.
[13] Frolov S M. Initiation of Strong Reactive Shocks and Detonation by Traveling Ignition Pulses [J]. Journal of Loss Prevention in the Process Industries, 2006, 19: 238-244.
[14] Frolov S M. Liquid-Fueled, Air-Breathing Pulse Detonation Engine Demonstrator: Operation Principles and Performance [J].Journal of Propulsion and Power, 2006, 22(6).
[15] Frolov S M, Basevich V Y, Aksenov V S, et al. Detonation Initiation in Liquid Fuel Sprays by Successive Electric Discharges[J].Doklady Physical Chemistry, 2004, 394(4): 39-41.
[16] Sinibaldi Jose O, Rodriguez Joel, Channel Brent, et al. Investigation of Transient Plasma Ignition for Pulse Detonation Engines [R]. AIAA 2005-3774.
[17] 董刚, 范宝春, 蒋勇, 等. 连续点火诱导爆轰的数值研究[J].中国科学技术大学学报, 2007, 37(11): 1439-1444.(编辑:史亚红)　　　　　　　　　　　　　*　收稿日期:2013-11-06；修订日期:2013-12-23。基金项目:国家自然科学基金(51306153)；高等学校博士学科点专项科研基金新教师类资助课题(20116102120027)；陕西省自然科学基金(2014JM7258)；西北工业大学基础研究基金(NPU-FFR-JCY20130129)。　　　　　作者简介:王治武(1981—),男,博士,副教授,研究领域为燃烧学、流体力学等。E-mail:malsoo@mail.nwpu.edu.cn

两点火源顺序点火起爆爆震波的数值研究 *

Numerical Investigation of Two Successive Ignitions Effect on Detonation Initiation

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