基于试验设计方法对氢燃料CIVB回火的多参数数值分析

推进技术 ›› 2016, Vol. 37 ›› Issue (6): 1098-1107.

基于试验设计方法对氢燃料CIVB回火的多参数数值分析

田晓晶^1,2,崔玉峰¹,邢双喜¹,房爱兵¹,聂超群¹

中国科学院先进能源动力重点试验室/工程热物理研究所，北京 100190; 中国科学院大学，北京 100049,中国科学院先进能源动力重点试验室/工程热物理研究所，北京 100190,中国科学院先进能源动力重点试验室/工程热物理研究所，北京 100190,中国科学院先进能源动力重点试验室/工程热物理研究所，北京 100190,中国科学院先进能源动力重点试验室/工程热物理研究所，北京 100190

发布日期:2021-08-15
作者简介:田晓晶，女，博士生，研究领域为富氢燃机燃烧室设计。E-mail: tianxiaojing@iet.cn 通讯作者:崔玉峰，男，博士，副研究员，研究领域为燃气轮机燃烧室设计和稳定性。
基金资助:
国家自然科学基金(51306180)。

Numerical Investigation of Effects of Multi-Factors

Key Laboratory of Advanced Energy and Power，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China; University of Chinese Academy of Sciences，Beijing 100049，China,Key Laboratory of Advanced Energy and Power，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China,Key Laboratory of Advanced Energy and Power，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China,Key Laboratory of Advanced Energy and Power，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China and Key Laboratory of Advanced Energy and Power，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China

Published:2021-08-15

摘要/Abstract

摘要： 为了能够全面考察多因素，包括质量流量、燃烧室结构(旋流器结构和预混段结构)、温度和燃料组分等对燃烧诱导涡破碎(CIVB)回火的影响，采用试验设计(DOE)方法进行多参数数值分析。对于CIVB回火的模拟采用二维轴对称模型，并补充用户自定义函数(UDF)来模拟旋流器的存在。结果表明:因素对CIVB回火影响的重要程度排序依次为:旋流器结构>预混段结构>温度>燃料组分>质量流量；其中，旋流器结构、预混段结构、温度和燃料组分对于CIVB回火具有高度显著的影响，而质量流量以及任意两因素间的交互作用可以忽略；各因素主要通过改变流场和火焰特性作用于CIVB回火。

关键词: 燃烧诱导涡破碎回火；试验设计方法；参数化分析；氢燃料火焰

Abstract: In order to investigate the effects of multi-factors，including mass flow rate，combustor geometry(swirler geometry and mixing zone geometry)，pre-heating temperature and fuel composition，on combustion induced vortex breakdown (CIVB) flashback，Design of Experiments (DOE) method was adopted for parametric analysis. For the simulation of CIVB flashback，two-dimensional axisymmetric model was used implementing user defined function (UDF) to represent the function of swirler. Through analyzing the results，the successive order of factors affecting CIVB flashback is swirler geometry，mixing zone geometry，preheating temperature，fuel composition and mass flow rate. Wherein，the first four factors have highly significant effects on CIVB flashback. By contrast，mass flow rate and the interaction between any two factors have insignificant and negligible effects. By further investigating，it is found that all the parameters take effect on CIVB flashback through changing flow distribution and flame properties.

Key words: Combustion induced vortex breakdown(CIVB)flashback；Design of experiments method；Parametric analysis；Hydrogen flame

田晓晶,崔玉峰,邢双喜,房爱兵,聂超群. 基于试验设计方法对氢燃料CIVB回火的多参数数值分析[J]. 推进技术, 2016, 37(6): 1098-1107.

TIAN Xiao-jing^1,2,CUI Yu-feng¹,XING Shuang-xi¹,FANG Ai-bing¹,NIE Chao-qun¹. Numerical Investigation of Effects of Multi-Factors[J]. Journal of Propulsion Technology, 2016, 37(6): 1098-1107.

参考文献

[1] Lieuwen T, McDonell V G, Santavicca D, et al. Burner Development and Operability Issues Associated with Steady Flowing Syngas Fired Combustors[J]. Combustion Science and Technology, 2008, 180(6): 1169-1192.
[2] Dam B, Corona G, Hayder M, et al. Effects of Syngas Composition on Combustion Induced Vortex Breakdown (CIVB) Flashback in a Swirl Stabilized Combustor[J]. Fuel, 2011, 90(11): 3274-3284.
[3] Fritz J, Kroner M, Sattelmayer T. Flashback in a Swirl Burner with Cylindrical Premixing Zone[J]. Journal of Engineering for Gas Turbine and Power, 2004, 126(2): 276-283.
[4] Kr?ner M, Sattelmayer T, Fritz J, et al. Flame Propagation in Swirling Flows Effect of Local Extinction on the Combustion Induced Vortex Breakdown[J]. Combustion Science and Technology, 2007, 179(7): 1385-1416.
[5] Konle M, Kiesewetter F, Sattelmayer T. Simultaneous High Repetition Rate PIV-LIF-Measurements of CIVB Driven Flashback[J]. Experiments in Fluids, 2008, 44(4): 529-538.
[6] Kr?ner M, Fritz J, Sattelmayer T. Flashback Limits for Combustor Induced Vortex Breakdown in a Swirl Burner[R]. ASME 2002-GT-30075.
[7] Burmberger S, Hirsch C, Sattelmayer T. Design a Radial Swirler Vortex Breakdown Burner[R]. ASME 2006-GT-90497
[8] Barmina I, Desnickis A, Meijere A, et al. Active Electric Control of Emissions from Swirling Combustion[M]. Germany: Advanced Combustion and Aerothermal Technologies, NATO Science for Peace and Security Series C: Environmental Security, Springer, 2007.
[9] Shelil N, Griffiths A, Bagdanavicius A, et al. Flashback Limits of Premixed H2/CH4 Flames in a Swirl-Premixed Combustor[R]. ASME 2010-GT-23623.
[10] Noble D R, Zhang Q, Shareef A, et al. Syngas Mixture Composition Effects upon Flashback and Blowoff[R]. ASME 2006-GT-90470.
[11] Escudier M. Vortex Breakdown: Observations and Explanations[J]. Progress in Aerospace Sciences, 1988, 25(2): 189-229.
[12] Tangermann E, Pfitzner M. Numerical Investigation of Flame Flashback into Swirling Flow[R]. ASME 2008-GT-51081.
[13] Kiesewetter F, Hirsch C, Fritz J, et al. Two-Dimensional Flashback Simulation in Strongly Swirling Flows[R]. ASME 2003-GT-38395.
[14] 田晓晶, 崔玉峰, 房爱兵, 等. 预混段结构对氢燃料旋流预混燃烧诱导涡破碎回火极限影响的数值研究[J]. 中国电机工程学报, 2014, 34(8): 1276-1284.
[15] 赵选民. 试验设计方法[M]. 北京:科学出版社, 2006.
[16] 田晓晶, 崔玉峰, 邢双喜, 等. 预混段结构对旋流预混氢火焰回火形式影响的数值研究[J]. 推进技术, 2015, 36(3): 345-351. (TIAN Xiao-jing, CUI Yu-feng, XING Shuang-xi, et al. Numerical Investigation on Effect of Mixing Zone Structure on Flashback Type for Swirl-Premixed Hydrogen Flame[J]. Journal of Propulsion Technology, 2015, 36(3): 345-351.)
[17] 王维, 楚武利, 张皓光. 基于试验设计的高负荷轴流压气机叶顶喷气参数化研究[J]. 推进技术, 2014, 35(2):178-186. (WANG Wei, CHU Wu-li, ZHANG Hao-guang. Parametric Study of Tip Injection in a High-Loaded Axial Compressor Based on Design of Experiment[J]. Journal of Propulsion Technology, 2014, 35(2): 178-186.)
[18] 刘文卿. 试验设计[M]. 北京:清华大学出版社, 2004.
[19] David B, Vincent M, Peter T, et al. Flashback and Turbulent Flame Speed Measurements in Hydrogen/ Methane Flames Stabilized by a Low-Swirl Injector at Elevated Pressures and Temperatures[J]. Journal of Engineering for Gas Turbines and Power, 2014, 136(3): 031502.
[20] Syred N, Beer J. Combustion in Swirling Flows: a Review[J]. Combustion and Flame, 1974, 23(2): 143-201.
[21] Squire H B. Analysis of the Vortex Breakdown Phenomenon [M]. UK: Imperial College of Science and Technology, Aeronautics Department, 1960.
[22] Ashoke D, Sumanta A. Dynamics of Upstream Flame Propagation in a Hydrogen-Enriched Premixed Flame[J]. International Journal of Hydrogen Energy, 2012, (37): 17294-17309.(编辑:朱立影)　　　　　　　　　　　　　*　收稿日期:2014-12-16；修订日期:2015-03-16。基金项目:国家自然科学基金(51306180)。作者简介:田晓晶,女,博士生,研究领域为富氢燃机燃烧室设计。E-mail: tianxiaojing@iet.cn通讯作者:崔玉峰,男,博士,副研究员,研究领域为燃气轮机燃烧室设计和稳定性。E-mail: cuiyf@iet.cn