Enhanced combustion characteristics of combustor head based on gliding arc

Weida CHENG; Jinlu YU; Zhao CHEN; Lei ZHANG; Bingbing ZHAO

doi:10.13224/j.cnki.jasp.20210706

Chinese

您当前的位置：

首页 >

文章列表页 >

Enhanced combustion characteristics of combustor head based on gliding arc

Combustion,Heat and Mass Transfer | 更新时间：2025-04-07

- Enhanced combustion characteristics of combustor head based on gliding arc
- Journal of Aerospace Power Vol. 37, Issue 7, Pages: 1392-1402(2022)
- 作者机构：
  
  1.空军工程大学航空工程学院，西安 710038
  2.西北工业大学动力与能源学院，西安 710129
  3.中国航空发动机集团有限公司四川燃气涡轮研究院，成都 610500
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20210706
  CLC：
- 稿件说明：
移动端阅览
Weida CHENG, Jinlu YU, Zhao CHEN, et al. Enhanced combustion characteristics of combustor head based on gliding arc[J]. Journal of Aerospace Power, 2022, 37(7): 1392-1402.
DOI：

Weida CHENG, Jinlu YU, Zhao CHEN, et al. Enhanced combustion characteristics of combustor head based on gliding arc[J]. Journal of Aerospace Power, 2022, 37(7): 1392-1402. DOI： 10.13224/j.cnki.jasp.20210706.

摘要

为了研究基于滑动弧的燃烧室头部强化燃烧效果，探究了燃烧室头部的点火过程以及不同等离子体电源输入功率下的点/熄火边界，利用像增强系统获得了CH*基团的分布云图。实验结果表明：输入功率的增大使得燃烧室的点/熄火边界均得到拓展，与160 W工况相比，输入功率为320 W时，点火边界平均拓宽约17.6%，与未放电相比，输入功率为320 W时，熄火边界平均拓宽约45.3%，滑动弧放电对熄火边界拓宽效果明显；当滑动弧能够点燃来流新鲜混合气时，输入功率的增加使得CH*基团分布向上游移动，当输入功率为320 W时，燃烧火焰驻留在燃烧室头部，当滑动弧激励器仅具有助燃作用时，输入功率的增加使得局部CH*基团辐射强度增强，热释放速率增加。

Abstract

In order to study the combustion enhancement effect of combustor head based on gliding arc，the ignition process of combustor head and the ignition/flameout boundary under different plasma power inputs were explored，and the cloud images of CH* group were obtained by image enhancement system.The experimental results showed that with the increase of input power，the ignition/flameout boundary of combustor was expanded.Compared with 160 W，when the input power was 320 W，the ignition boundary was widened by about 17.6% on average.Compared with 0 W，when the input power was 320 W，the flameout boundary was widened by about 45.3% on average，and the gliding arc discharge had obvious effect on widening flameout boundary.When the gliding arc successfully ignited the fresh gas mixture flowing through it，the increase of input power made the CH* group distribution move upstream.When the input power was 320 W，the combustion flame was stuck around the head of the combustor.When the gliding arc exciter had only combustion⁃supporting function，the increase of input power made the local CH* group radiation intensity increase and the heat release rate increase.

关键词

Keywords

references

于锦禄 , 黄丹青 , 王思博 , 等 . 等离子体点火与助燃技术在航空发动机上的应用 [J]. 航空发动机 , 2018 , 44 （ 3 ）: 12 ⁃ 20 .

YU Jinlu , HUANG Danqing , WANG Sibo , et al . Application of plasma ignition and assisted combustion of aeroengine [J]. Aeroengine , 2018 , 44 （ 3 ）: 12 ⁃ 20 . （in Chinese）

何立明 , 刘兴建 , 赵兵兵 , 等 . 等离子体强化燃烧的目前研究进展 [J]. 航空动力学报 , 2016 , 31 （ 7 ）: 1537 ⁃ 1551 .

HE Liming , LIU Xingjian , ZHAO Bingbing , et al . Current investigation progress of plasma⁃assisted ignition and combustion [J]. Journal of Aerospace Power , 2016 , 31 （ 7 ）: 1537 ⁃ 1551 . （in Chinese）

李钢 , 李华 , 杨凌元 , 等 . 俄罗斯等离子体点火和辅助燃烧研究进展 [J]. 科技导报 , 2012 , 30 （ 17 ）: 66 ⁃ 72 .

LI Gang , LI Hua , YANG Lingyuan , et al . Review of the plasma ignition and assisted combustion in Russia [J]. Science & Technology Review , 2012 , 30 （ 17 ）: 66 ⁃ 72 . （in Chinese）

JU Y , SUN W . Plasma assisted combustion:dynamics and chemistry [J]. Progress in Energy and Combustion Science , 2015 , 48 : 21 ⁃ 83 .

张若兵 , 罗刚 , 黄昊晨 , 等 . 电极结构对滑动弧放电等离子体尺寸的影响规律 [J]. 高电压技术 , 2019 , 45 （ 10 ）: 3357 ⁃ 3364 .

ZHANG Ruobing , LUO Gang , HUANG Haocheng , et al . Influence of electrode structure on the dimension parameters of gliding arc discharge plasma [J]. High Voltage Engineering , 2019 , 45 （ 10 ）: 3357 ⁃ 3364 . （in Chinese）

汤洁 , 段忆翔 , 赵卫 , 等 . 介质阻挡放电等离子体增强引擎燃烧技术的初步研究 [J]. 高电压技术 , 2010 , 36 （ 3 ）: 733 ⁃ 738 .

TANG Jie , DUAN Yixiang , ZHAO Wei , et al . Study of dielectric barrier discharge nonequilibrium plasma⁃assisted combustion for more efficient engine [J]. High Voltage Engineering , 2010 , 36 （ 3 ）: 733 ⁃ 738 . （in Chinese）

赵兵兵 , 张鹏 , 何立明 , 等 . 等离子体助燃对燃烧产物影响的实验 [J]. 航空动力学报 , 2012 , 27 （ 9 ）: 1974 ⁃ 1978 .

ZHAO Bingbing , ZHANG Peng , HE Liming , et al . Experiments of plasma assisted combustion's effect on combustion products [J]. Journal of Aerospace Power , 2012 , 27 （ 9 ）: 1974 ⁃ 1978 . （in Chinese）

HWANG J , KIM W , BAE C , et al . Application of a novel microwave⁃assisted plasma ignition system in a direct injection gasoline engine [J]. Applied Energy , 2017 , 205 : 562 ⁃ 576 .

聂万胜 , 周思引 , 车学科 . 纳秒脉冲放电等离子体助燃技术研究进展 [J]. 高电压技术 , 2017 , 43 （ 6 ）: 1749 ⁃ 1758 .

NIE Wansheng , ZHOU Siyin , CHE Xueke . Review of plasma assisted combustion technology by nanosecond pulsed discharge [J]. High Voltage Engineering , 2017 , 43 （ 6 ）: 1749 ⁃ 1758 . （in Chinese）

ZHAO Bingbing , CHEN Gaocheng , HE Liming , et al . Experimental investigation of plasma jet ignition characteristics in kerosene⁃air mixtures [J]. Journal of Aerospace Engineering , 2020 , 33 （ 2 ）: 04019113.1 ⁃ 04019113.5 .

CZERNICHOWSKI A . Gliding arc:applications to engineering and environment control [J]. Pure and Applied Chemistry , 1994 , 66 （ 6 ）: 1301 ⁃ 1310 .

OMBRELLO T , WON S H , JU Y , et al . Flame propagation enhancement by plasma excitation of oxygen：Part Ⅱ effects of O 2 （a1Δg） [J]. Combustion and Flame , 2010 , 157 （ 10 ）: 1916 ⁃ 1928 .

张川宇 , 冯戎 , 朱家健 , 等 . 滑动弧等离子体辅助超声速燃烧实验研究 [J]. 固体火箭技术 , 2021 , 44 （ 2 ）: 160 ⁃ 165 .

ZHANG Chuanyu , FENG Rong , ZHU Jiajian , et al . Experimental investigation on gliding arc plasma⁃assisted combustion in the supersonic flow [J]. Journal of Solid Rocket Technology , 2021 , 44 （ 2 ）: 160 ⁃ 165 . （in Chinese）

FENG Rong , HUANG Yuhui , ZHU Jiajian , et al . Ignition and combustion enhancement in a cavity⁃based supersonic combustor by a multi⁃channel gliding arc plasma [J]. Experimental Thermal and Fluid Science , 2021 , 120 : 110248.1 ⁃ 110248.11 .

GAO J , KONG C , ZHU J , et al . Visualization of instantaneous structure and dynamics of large⁃scale turbulent flames stabilized by a gliding arc discharge [J]. Proceedings of the Combustion Institute , 2019 , 37 （ 4 ）: 5629 ⁃ 5636 .

OMBRELLO T , JU Y , FRIDMAN A . Kinetic ignition enhancement of diffusion flames by nonequilibrium magnetic gliding arc plasma [J]. AIAA Journal , 2008 , 46 （ 10 ）: 2424 ⁃ 2433 .

OMBRELLO T , JU Y . Kinetic Ignition enhancement of H 2 versus fuel⁃blended air diffusion flames using nonequilibrium plasma [J]. IEEE Transactions on Plasma Science , 2008 , 36 （ 6 ）: 2924 ⁃ 2932 .

TANG Yong , SUN Jinguo , SHI Baolu , et al . Extension of flammability and stability limits of swirling premixed flames by AC powered gliding arc discharges [J]. Combustion and Flame , 2021 , 231 : 111483.1 ⁃ 111483.13 .

于锦禄 . 等离子体点火与助燃在航空发动机中的应用研究 [R]. 西安：第三届全国青年燃烧学术会议 , 2017 .

张磊 , 于锦禄 , 陈一 , 等 . 基于滑动弧的航空发动机燃烧室头部喷雾特性 [J]. 航空学报 , 2021 , 42 （ 3 ）: 275 ⁃ 289 .

ZHANG Lei , YU Jinlu , CHEN Yi , et al . Spray characteristics of gliding arc discharge combustion dome of areo⁃engine combustors [J]. Acta Aeronautica et Astronautica Sinica , 2021 , 42 （ 3 ）: 275 ⁃ 289 . （in Chinese）

胡长淮 , 何立明 , 陈一 , 等 . 燃烧室头部激励的等离子体强化燃烧特性实验研究 [J]. 推进技术 , 2021 , 42 （ 12 ）: 2762 ⁃ 2771 .

HU Changhuai , HE Liming , CHEN Yi , et al . Experimental research on the characteristics of plasma⁃enhanced combustion excited by the combustor dome [J]. Journal of Propulsion Technology , 2021 , 42 （ 12 ）: 2762 ⁃ 2771 . （in Chinese）

张凯 , 金迪 , 宋飞龙 , 等 . 纳秒脉冲滑动弧放电等离子体裂解煤油实验研究 [EB/OL]. 推进技术 .[ 2021⁃12⁃14 ]. https:∥doi.org/10.13675/j.cnki.tjjs.200993 https://doi.org/10.13675/j.cnki.tjjs.200993 .

ZHANG Kai , JIN Di , SONG Feilong , et al . Experimental research on nanosecond pulsed gliding arc discharge plasma cracking kerosene [EB/OL]. Journal of Propulsion Technology .[ 2021⁃12⁃14 ]. （in Chinese）

王宽亮 , 李飞 , 刘德峰 , 等 . 基于CH自由基发光的旋流火焰放热率时空特性研究 [J]. 航空动力学报 , 2019 , 34 （ 4 ）: 920 ⁃ 928 .

WANG Kuanliang , LI Fei , LIU Defeng , et al . Study of the temporal and spatial characteristics for swirling flame heat release rate based on CH chemiluminescence [J]. Journal of Aerospace Power , 2019 , 34 （ 4 ）: 920 ⁃ 928 . （in Chinese）

肖为 , 江立军 , 陈盛 . 燃烧室电火花点火模型 [J]. 航空动力学报 , 2021 , 36 （ 1 ）: 25 ⁃ 33 .

XIAO Wei , JIANG Lijun , CHEN Sheng . Spark ignition model for combustor [J]. Journal of Aerospace Power , 2021 , 36 （ 1 ）: 25 ⁃ 33 . （in Chinese）

HABER L C ， VANDSBURGER U ， SAUNDERS W R ， et al . An experimental examination of the relationship between chemiluminescent light emissions and heat⁃release rate under non⁃adiabatic conditions ［R］. ASME Paper 2000⁃GT⁃0121 , 2000 .

黄勇 , 林宇震 , 樊志军 , 等 . 燃烧与燃烧室 [M]. 北京：北京航空航天出版社， 2009 .

何立明 . 飞机推进系统原理 [M]. 北京：国防工业出版社， 2009 .

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Experimental on the thermal effects of pulsed dielectric barrier discharge plasma

Numerical investigation on leading-edge vortex control fornon-slender delta wing by nanosecond pulsedielectric barrier discharge actuation

Plasma body force phenomenological model for different altitudes

Plasma assisted methane ignition based on shock tube

基于自适应MOMEDA滚动轴承故障特征提取方法

Related Author

YANG Leilei

CAI Jinsheng

TIAN Yongqiang

王学德

牛中国

梁华

赵光银

肖良华

Related Institution

中国航空工业集团有限公司空气动力研究院

空军工程大学航空工程学院航空等离子体动力学实验室

西北工业大学航天学院燃烧、热结构与内流场重点实验室

空军工程大学航空工程学院等离子体动力学重点实验室

航天工程大学研究生院

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰