基于多层氧化层结构的硼颗粒点火模型研究

doi:10.3969/j.issn.1000-1093.2016.12.009

兵工学报 ›› 2016, Vol. 37 ›› Issue (12): 2242-2250.doi: 10.3969/j.issn.1000-1093.2016.12.009

基于多层氧化层结构的硼颗粒点火模型研究

徐义华，胡旭，邹昊，李雨林，曾卓雄

（南昌航空大学飞行器工程学院, 江西南昌 330063）

收稿日期:2016-04-19 修回日期:2016-04-19 上线日期:2017-02-20
作者简介:徐义华（1971—)，男副教授，硕士生导师
基金资助:
国家自然科学基金项目（51266013、51066006）

Research on Model of Ignition of Boron Particle Based on Multiple Oxide Layer Structure

XU Yi-hua, HU Xu, ZOU Hao, LI Yu-lin, ZENG Zhuo-xiong

(School of Aircraft Engineering, Nanchang Hangkong University, Nanchang 330063, Jiangxi, China)

Received:2016-04-19 Revised:2016-04-19 Online:2017-02-20

摘要/Abstract

摘要： 为了研究相关因素对硼颗粒点火过程的影响规律，基于多层氧化层结构，改进了硼颗粒的点火模型。该模型考虑了颗粒氧化层表面物质成分的变化、表面火焰面形成的物理过程，模型计算结果与实验数据具有较高的吻合度。应用该模型研究了环境压强、颗粒直径、气相氧化剂浓度以及环境温度对硼颗粒点火过程的影响规律。结果表明，环境压力越大，颗粒点火时间越短；颗粒粒径越大，颗粒表面氧化层越厚，从而延长了颗粒的点火时间；在较大颗粒直径（>5 μm）下增加环境内氧气浓度有利于颗粒点火，对小颗粒直径（≤5 μm)则无明显影响；水蒸气浓度越大，颗粒点火时间越短；环境温度越高，越有利于颗粒点火。

关键词: 航空、航天推进系统, 固体火箭冲压发动机, 硼颗粒, 氧化层结构, 点火模型

Abstract: In order to study the influence of the related factors on the ignition process of boron particle by using numerical calculation method, an improved ignition model of boron particle is developed under the consideration of the multilayer oxide structure. The physical process of the change of species at the surface of the oxide layer and the formation of surface flame is considered in the model. The simulation results are in good agreement with published experimental data. The influences of ambient pressure, particle diameter, kinds of oxidant and their concentration, ambient temperature on the ignition process of boron particle are studied by using the improved ignition model. The simulation results show that the ignition time is shortened at higher ambient pressure. The larger the particle diameter is, the thicker the oxide layer is, thus delaying the ignition time. The higher oxygen concentration has a good effect on the ignition of boron particle on the larger particle diameter（>5 μm）, but has little significant influence on smaller particle diameter(≤5 μm). The ignition of boron particle is promoted with water vapor available. The higher concentration of water vapor makes the ignition time reduced. The higher ambient temperature is useful for the ignition of boron particle.

Key words: aerospace propulsion system, solid fuel ramjet, boron particle, oxide structure, ignition model

中图分类号:

V512

徐义华，胡旭，邹昊，李雨林，曾卓雄. 基于多层氧化层结构的硼颗粒点火模型研究[J]. 兵工学报, 2016, 37(12): 2242-2250.

XU Yi-hua, HU Xu, ZOU Hao, LI Yu-lin, ZENG Zhuo-xiong. Research on Model of Ignition of Boron Particle Based on Multiple Oxide Layer Structure[J]. Acta Armamentarii, 2016, 37(12): 2242-2250.

参考文献

［1］敖文, 杨卫娟, 韩志江, 等. 硼颗粒点火燃烧模型进展研究［J］. 固体火箭技术, 2012, 35(3): 361-366, 371.
AO Wen, YANG Wei-juan, HAN Zhi-jiang, et al. Research on boron particles ignition and combustion model ［J］. Journal of Solid Rocket Technology, 2012, 35(3): 361-366, 371. (in Chinese)
［2］ Hussmann B, Pfitzner M. Extended combustion model for single boron particles-part I: theory［J］. Combustion and Flame, 2010, 157(4): 803-821．
［3］ Hussmann B, Pfitzner M. Extended combustion model for single boron particles-part II: validation［J］. Combustion and Flame, 2010, 157(4): 822-833．
［4］胡建新, 夏智勋, 罗振兵, 等. 固体火箭冲压发动机补燃室内硼颗粒点火计算研究［J］. 含能材料, 2004, 12(6): 342-345.
HU Jian-xin, XIA Zhi-xun, LOU Zhen-bing, et al. Calculation on ignition of boron particle of ducted rocket secondary chamber ［J］. Energetic Materials, 2004, 12(6): 342-345. (in Chinese)
［5］方传波, 夏智勋, 肖云雷, 等. 考虑Stefan影响的单颗粒硼着火过程研究［J］. 物理学报, 2013, 62(16): 164702-1-164702-8.
FANG Chuan-bo, XIA Zhi-xun, XIAO Yun-lei, et al. Study of ignition process of boron particle with considering Stefan flow effects ［J］. Acta Physica Sinica, 2013, 62(16): 164702-1-164702-8. (in Chinese)
［6］ Macek A, Semple J M. Combustion of boron particles at atmospheric pressure［J］. Combustion Science and Technology, 1969, 1(3): 181-191.
［7］王洪远, 徐义华, 胡旭, 等. 空气旋转进气对含硼固体冲压发动机二次燃烧性能影响的研究［J］. 兵工学报，2015, 36(4): 619-625.
WANG Hong-yuan, XU Yi-hua, HU Xu, et al. Research on the characteristics of secondary combustion of boron-based ducted rocket with swirling air injection ［J］. Acta Armamentarii, 2015, 36(4): 619-625. (in Chinese)
［8］ King M K. Boron particle ignition in hot gas streams［J］. Combustion Science and Technology, 1973, 8 (5/6): 255-273.
［9］ King M K. Ignition and combustion of boron particles and clouds［J］. Journal of Spacecraft and Rocket, 1982, 19(4): 294-306.
［10］ Li S C, Williams F A. Ignition and combustion of boron in wet and dry atmospheres［J］. Symposium (International) on Combustion, 1991, 23(1): 1147-1154.
［11］ Li S C, Williams F A. Ignition and combustion of boron particles combustion of boron-based solid propellants and solid fuels［M］. Boca Raton, FL: CRC Press Inc, 1993: 248-271．
［12］ Yeh C L, Kuo K K. Ignition and combustion of boron particles［J］. Progress in Energy and Combustion Science, 1996, 22(6): 511-541．
［13］ Ao W, Yang W J, Wang Y, et al. Ignition and combustion of boron particles at one to ten standard atmosphere［J］. Journal of Propulsion and Power, 2014, 30 (3): 760-764.
［14］ Ao W, Zhou J H, Liu J Z, et al. Kinetic model of single boron particle ignition based upon both oxygen and (BO)n diffusion mechanism［J］. Combustion, Explosion, and Shock Waves, 2014, 50(3): 262-271.
［15］ Wilke C R. Diffusion properties of multicomponent gases［J］. Chemical Engineering Process, 1950, 46(2): 95-104.
［16］ Povitsky A, Goldman Y. Boron particle ignition in high-speed flow［C］∥AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit. Monterey, CA: AIAA, 1993.
［17］ Glassman I, Williams F A, Antaki P. A physical and chemical interpretation of boron particle combustion［C］∥Twentieth Symposium( International) on Combustion. Ann Arbor, MI: The Combustion Institute, 1984.
［18］ Ulas A, Kuo K K, Gotzmer C. Ignition and combustion of boron particles in fluorine-containing environments［J］. Combustion and Flame, 2001, 127 (1/2): 1935-1957.
［19］胡建新. 含硼推进剂固体火箭冲压发动机补燃室工作过程研究［D］. 长沙:国防科学技术大学, 2006.
HU Jian-xin. Research on the secondary combustion chamber operation process of boron-based propellant ducted roeket ［D］. Changsha: National Defense Science and Technology University, 2006. (in Chinese)
［20］ Zhou W. Numerical study of multi-phase combustion: ignition and combustion of an isolated boron particle in fluorinated environments［D］. Princton: Princeton University, 1998.

[1]	王虹富，白帆，刘彦，段卓平，黄风雷. 爆炸冲击波作用下黑索今基含铝炸药的冲击点火反应速率模型[J]. 兵工学报, 2021, 42(2): 327-339.
[2]	傅鑫，曹永华，张一彬，朱超. 基于一种泄漏流边界模型的封严篦齿分析方法研究[J]. 兵工学报, 2017, 38(4): 824-832.
[3]	王洪远，徐义华，胡旭，曾卓雄. 空气旋转进气对含硼固体冲压发动机二次燃烧性能影响的研究[J]. 兵工学报, 2015, 36(4): 619-625.
[4]	朱大林，唐胜景，郭杰，高峰. 基于单学科可行法的固体火箭发动机参数优化设计[J]. 兵工学报, 2012, 33(8): 897-901.
[5]	常武军，鞠玉涛，王蓬勃. HTPB推进剂脱湿与力学性能的相关性研究[J]. 兵工学报, 2012, 33(3): 261-266.
[6]	韩波，鞠玉涛，周长省. HTPB推进剂粘聚区本构模型反演识别研究[J]. 兵工学报, 2012, 33(11): 1335-1341.

基于多层氧化层结构的硼颗粒点火模型研究

Research on Model of Ignition of Boron Particle Based on Multiple Oxide Layer Structure

PDF

可视化

被引次数

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 6

编辑推荐

Metrics

本文评价