学报(中文)

燃料分级比例对双燃料燃烧室燃烧性能的影响

展开
  • 沈阳航空航天大学 辽宁省航空推进系统先进测试技术重点实验室, 沈阳 110136

网络出版日期: 2020-07-31

基金资助

辽宁省自然科学基金(20180550358),航空科学基金(20170354001)资助项目

Influence of Fuel-Staging Ratio on Combustion Performance of Dual Fuel Combustor

Expand
  • Liaoning Key Laboratory of Advanced Testing Technology for Aeronautical Propulsion System, Shenyang Aerospace University, Shenyang 110136, China

Online published: 2020-07-31

摘要

通过数值与试验相结合的方法对一种双燃料低污染燃烧室的流场和燃烧特性进行了研究.利用Fluent软件对该低污染燃烧室进行了数值模拟,对燃烧室的点火、熄火特性进行了试验测试,在燃烧室进口参数一定的情况下,改变值班级和主燃级燃料能量的分配比例,对比分析主燃级能量比例对燃烧特性的影响.结果表明,所研究的低污染燃烧室头部存在中心回流区、角落回流区以及唇口回流区;燃烧室的点火、熄火特性满足要求;燃料分级比例对污染物排放具有较大的影响,在双燃料的设计点和单独使用气体燃料时,CO和NOx排放均达到了燃烧室的设计要求.

本文引用格式

刘爱虢, 陈炫任, 杨宇东, 陈雷, 王成军 . 燃料分级比例对双燃料燃烧室燃烧性能的影响[J]. 上海交通大学学报, 2020 , 54(7) : 756 -764 . DOI: 10.16183/j.cnki.jsjtu.2019.132

Abstract

The flow field and combustion characteristics of a dual fuel low pollution combustor were studied by using numerical and experimental methods. The low-pollution combustor was numerically simulated by using Fluent software. The ignition and extinguishing characteristics of the combustor were tested experimentally. The fuel energy distribution ratio of duty class and main combustion stage was changed when the inlet parameters of the combustor were fixed. The influence of the energy ratio of the main combustion stage on combustion characteristics was compared and analyzed. The results show that there is a central reflux zone, a corner reflux zone, and a lip reflux zone in the head of the low-pollution combustor studied. The ignition and extinguishing characteristics of the combustor meet the requirements and the fuel classification ratio has a great impact on pollutant emissions. When the dual fuel design point and the gas fuel are used alone, CO and NOx emissions meet the design requirements of the combustor.

参考文献

[1]翁一武, 闻雪友, 翁史烈. 燃气轮机技术及发展[J].自然杂志, 2017, 39(1): 43-47. WENG Yiwu, WEN Xueyou, WENG Shilie. Gas turbine technology and development[J]. Chinese Journal of Nature, 2017, 39(1): 43-47. [2]杨强. 中小型双燃料燃气轮机发展现状及应用前景分析[J].舰船科学技术, 2019, 41(2): 1-8. YANG Qiang. Development and application of small and medium-sized dual-fuel gas turbine[J]. Ship Science And Technology, 2019, 41(2): 1-8. [3]MOLL D, LRSTAD D, BAI X S. Numerical investigation of methane/hydrogen/air partially premixed flames in the SGT-800 burner fitted to a combustion rig[J]. Flow, Turbulence and Combustion, 2016, 96(4): 987-1003. [4]李孝堂.航机改型燃气轮机设计及试验技术[M].北京: 航空工业出版社, 2017. LI Xiaotang. Design and test technology of aircraft modified gas turbine [M]. Beijing: Aviation Industry Press, 2017. [5]刘爱虢, 朱悦, 陈保东, 等. 某重型燃气轮机NOx排放性能反应动力学数值计算[J]. 上海交通大学学报, 2017, 51(11): 1383-1390. LIU Aiguo, ZHU Yue, CHEN Baodong, et al. Reaction kinetic simulation of NOx emission performance for a heavy-duty gas turbine[J]. Journal of Shanghai Jiao Tong University, 2017, 51(11): 1383-1390. [6]王增国,冉军辉,李国勇.双燃料燃气轮机燃料快速切换技术分析与试验研究[J]. 热能动力工程, 2019, 34(8): 31-34. WANG Zengguo, RAN Junhui, LI Guoyong. Analysis of fast fuel switching technology for dual fuel gas turbine and its experimental study [J]. Journal of Engineering for Thermal Energy and Power, 2019, 34(8): 31-34. [7]李雅军, 师蓓蓓, 张晨曦, 等. 双燃料燃气轮机喷嘴结构及性能研究[J].舰船科学技术, 2015, 37(5): 47-53. LI Yajun, SHI Beibei, ZHANG Chenxi, et al. Research on structure and performance of dual fuel nozzle[J]. Ship Science And Technology, 2015, 37(5): 47-53. [8]尉曙明, 索建秦. 航空衍生工业燃气轮机双燃料贫燃预混低污染燃烧技术[J]. 航空动力学报, 2015, 30(9): 2049-2057. WEI Shuming, SUO Jianqin. Aero-derivative industrial gas turbine dual fuel lean premixed low emission technology[J]. Journal of Aerospace Power, 2015, 30(9): 2049-2057. [9]严欢. 燃油喷射参数对双燃料发动机燃烧过程影响研究[D]. 哈尔滨: 哈尔滨工程大学, 2015. YAN Huan. Research on fuel injection parameters influencing on dual fuel engine combustion process [D]. Harbin: Harbin Engineering University, 2015. [10]张龙, 张珊珊, 查筱晨, 等. 一种燃气轮机燃烧室中心体供油双燃料喷嘴: CN104654360 A[P]. 2015-07-29. ZHANG Long, ZHANG Shanshan, ZHA Xiaochen, et al. A dual fuel nozzle for gas turbine combustor: CN104654360 A[P]. 2015-07-29. [11]杨强, 冉军辉, 孔庆毅, 等.典型双燃料燃气轮机产品对比及技术难点分析[J].舰船科学技术, 2019, 41(1): 102-106. YANG Qiang, RAN Junhui, KONG Qingyi, et al. Dual fuel gas turbine product comparison and analysis of technical difficulties[J]. Ship Science and Technology, 2019, 41(1): 102-106. [12]博伊斯.燃气轮机工程手册[M]. 北京: 石油工业出版社, 2012. BOIS. Gas turbine engineering manual[M]. Beijing: Petroleum Industry Press, 2012. [13]刘爱虢, 朱悦, 陈保东, 等.航改型双环燃烧室燃烧反应特性试验[J]. 航空动力学报, 2017, 32(8): 1793-1800. LIU Aiguo, ZHU Yue, CHEN Baodong, et al. Experiment on combustion characteristics of aeroderivate gas turbine twins annular combustor[J]. Journal of Aerospace Power, 2017, 32(8): 1793-1800. [14]邓远灏, 颜应文, 朱嘉伟, 等. LPP低污染燃烧室两相喷雾燃烧数值研究[J]. 航空动力学报, 2014, 34(4): 792-800. DENG Yuanhao, YAN Yingwen, ZHU Jiawei, et al. Numberical investigation of two-phase spray combustion performance for LPP low-emission combustor[J]. Journal of Aerospace Power, 2014, 34(4): 792-800. [15]于涵, 索建秦, 朱鹏飞, 等. 中心分级贫油直喷(LDI)燃烧室流动及污染排放特性研究[J]. 西北工业大学学报, 2018, 36(5): 816-823. YU Han, SUO Jianqin, ZHU Pengfei, et al. The characteristic of flow field and emissions of a concentric staged lean direct injection(LDI) combustor[J]. Journal of Northwestern Polytechnical University, 2018, 36(5): 816-823. [16]刘爱虢, 朱悦, 陈保东, 等. 三级旋流器旋流角匹配影响双环预混旋流燃烧室燃烧性能试验[J]. 推进技术, 2017, 38(7): 1539-1547. LIU Aiguo, ZHU Yue, CHEN Baodong, et al. Experiment on effects of triple swirler swirl angle mat-ching on combustion performance of twins annular premixing swirler combustor[J]. Journal of Propulsion Technology, 2017, 38(7): 1539-1547. [17]林宇震, 许全宏, 刘高恩. 燃气轮机燃烧室[M]. 北京: 国防工业出版社, 2008. LIN Yuzhen, XU Quanhong, LIU Gaoen. Gas turbine combustor[M].Beijing: National Defense Industry Press, 2008. [18]勒菲沃A H, 鲍拉尔D R. 燃气涡轮发动机燃烧[M]. 刘永泉,等,第3版.北京: 航空工业出版社, 2016. LEFEBVRE Arthur H, BALLAL Dillip R. Gas turbine combustion[M]. LIU Yongquan, et al, 3rd ed. Beijing: Aviation Industry Press, 2016. [19]尉曙明.先进燃气轮机燃烧室设计研发[M]. 上海: 上海交通大学出版社, 2014. WEI Shuming. Advanced gas turbine combustor design and development[M]. Shanghai: Shanghai Jiao Tong University Press, 2014. [20]金如山, 索建秦.先进燃气轮机燃烧室[M].北京: 航空工业出版社, 2016. JIN Rushan, SUO Jianqin. Advanced gas turbine combustor[M]. Beijing: Aviation Industry Press, 2016. [21]DHANUKA S K, TEMME J E. Unsteady aspects of lean premixed-prevaporized (LPP) gas turbine combustors: Flame-flame interactions[J]. Journal of Propulsion and Power, 2011, 27(3): 631-641. [22]李孝堂, 侯凌云, 尚守堂, 等.现代燃气轮机技术[M]. 北京: 航空工业出版社, 2006. LI Xiaotang, HOU Lingyun, SHANG Shoutang, et al. Modern gas turbine technology[M]. Beijing: Aviation Industry Press, 2006.
文章导航

/