Please wait a minute...
 首页  期刊介绍 期刊订阅 联系我们 横山亮次奖 百年刊庆
 
最新录用  |  预出版  |  当期目录  |  过刊浏览  |  阅读排行  |  下载排行  |  引用排行  |  横山亮次奖  |  百年刊庆
清华大学学报(自然科学版)  2023, Vol. 63 Issue (4): 660-669    DOI: 10.16511/j.cnki.qhdxxb.2023.25.032
  论文 本期目录 | 过刊浏览 | 高级检索 |
天然气径向分级燃烧室低NOx排放的优化研究
田园, 耿俊杰, 孙逸凡, 祁海鹰
清华大学 能源与动力工程系, 北京 100084
Optimization investigation of low NOx emissions of natural gas radially staged combustor
TIAN Yuan, GENG Junjie, SUN Yifan, QI Haiying
Department of Energy and Power Engineering, Tsinghua University, Beijing 100084, China
全文: PDF(10932 KB)   HTML
输出: BibTeX | EndNote (RIS)      
摘要 为解决天然气径向分级燃烧室NOx排放超标问题,该文采用数值模拟和试验方法研究了天然气径向分级燃烧室结构改进策略和优化方案,多喷嘴参数匹配关系及部分负荷下NOx排放的预测关系式。结果表明:改变掺混孔径的达标方案合理可行,得到孔径值44.45 mm和其他性能参数的变化规律;中心喷嘴是决定NOx排放水平的主要因素;多喷嘴匹配关系的低排放设计准则是喷嘴燃料量相等;改进NOx排放预测公式准确反映了其部分负荷行为。该研究可为燃烧室后续试验调试和设计改进提供理论依据。
服务
把本文推荐给朋友
加入引用管理器
E-mail Alert
RSS
作者相关文章
田园
耿俊杰
孙逸凡
祁海鹰
关键词 天然气径向分级燃烧室结构改进策略掺混孔径变更多喷嘴匹配关系NOx排放预测公式    
Abstract:[Objective] To solve the problem of excessive NOx emissions of the existing natural gas radially staged combustor, the design principle of parameter matching between multiple nozzles at the head of the combustion chamber is explored, and an optimized prediction formula for NOx emission performance of the combustor is obtained. [Methods] This study adopts numerical simulation and experimental data analysis methods. The different loads and diameters of the dilution holes of the combustor are numerically simulated. Through the numerical analysis of the nonuniformity of the premix and the equivalent ratio of the original design, a structural improvement strategy and an optimization scheme to reduce the dilution holes' diameter were proposed. The influence of the improvement in the dilution holes' diameter on NOx emissions and that of the modification scheme on the total pressure loss and other performance parameters were investigated. The relationship between parameter matching of multiple nozzles and NOx emission under different combustion modes was investigated. Because of the deficiency of the current NOx emission prediction formula, based on the experimental and numerical data, the prediction formula of NOx emission under partial load is improved. [Results] Results showed that the original low-emission design of the combustor was unreasonable, and the NOx emission value was six times that of the limit value of 41 mg/Nm3 at 15% O2. The standard scheme of changing the dilution holes' diameter was reasonable and feasible, and the dilution holes' diameter Djet=44.45 mm can ensure that the standard of NOx was determined and verified by the experiment. The resulting changed in the total pressure loss and other performance parameters were within the acceptable range. In the proposed dilution holes' diameter modification scheme, the change in the dilution holes' area from large to small was 33.1%, 47.1%, and 59.5%, which exceeded 30% of the original design, and the head structure was not redesigned. A warning that the combustor may face the risk of wall overtemperature during long-term operation was proposed. The equivalence ratio and nonuniformity of the premix, two key parameters used to characterize lean premix, were sufficient and necessary conditions to effectively control the NOx emission. The central nozzle was the main factor in determining the emission level. Because the central area was in the high equivalent ratio area, the fuel amount of a single nozzle was high, premix uniformity was poor, and diffusion combustion of heavy-duty fuel occurred. Notably, the low-emission design criterion of the multi-nozzle matching relationship in the natural gas radially staged combustor investigated in this study was that the fuel amount of the single annular nozzle was equal to the fuel amount of the central area in combustion mode 2. [Conclusions] Based on the experimental and numerical data in this study, an improved NOx emission prediction formula that can accurately reflect the partial load behavior of this type of combustor is proposed. Compared with the test data of the two combustors, the prediction formula has sufficient accuracy, and the maximum relative error is 8.73%. This research provides a theoretical basis for the subsequent test debugging and design improvement of the combustor.
Key wordsnatural gas radially staged combustor    structural improvement strategy    change in the dilution holes' diameter    multi-nozzle matching relationship    NOx emission predicting formula
收稿日期: 2023-02-20      出版日期: 2023-04-22
基金资助:国家科技重大专项资助项目(Y2019-I-0022-0021)
通讯作者: 祁海鹰,教授,E-mail:hyqi@tsinghua.edu.cn     E-mail: hyqi@tsinghua.edu.cn
作者简介: 田园(1997-),男,硕士研究生。
引用本文:   
田园, 耿俊杰, 孙逸凡, 祁海鹰. 天然气径向分级燃烧室低NOx排放的优化研究[J]. 清华大学学报(自然科学版), 2023, 63(4): 660-669.
TIAN Yuan, GENG Junjie, SUN Yifan, QI Haiying. Optimization investigation of low NOx emissions of natural gas radially staged combustor. Journal of Tsinghua University(Science and Technology), 2023, 63(4): 660-669.
链接本文:  
http://jst.tsinghuajournals.com/CN/10.16511/j.cnki.qhdxxb.2023.25.032  或          http://jst.tsinghuajournals.com/CN/Y2023/V63/I4/660
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
[1] 蒋洪德,任静,李雪英,等.重型燃气轮机现状与发展趋势[J].中国电机工程学报, 2014, 34(29):5096-5102. JIANG H D, REN J, LI X Y, et al. Status and development trend of the heavy duty gas turbine[J]. Proceedings of the CSEE, 2014, 34(29):5096-5102.(in Chinese)
[2] 中华人民共和国国家质量监督检验检疫总局,中国国家标准化管理委员会.火电厂大气污染物排放标准:GB 13223-2011[S].北京:中国环境科学出版社, 2012. General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China. Emission standard of air pollutants for thermal power plants:GB 13223-2011[S]. Beijing:China Environmental Science Press, 2012.(in Chinese)
[3] 祝俊宗,胡羽,夏单城,等.改善低NOx燃烧室预混均匀性的结构优化策略[J].中国电机工程学报, 2017, 37(21):6353-6362. ZHU J Z, HU Y, XIA D C, et al. Structural optimization strategy of improving the premixing uniformity in a low NOx combustor[J]. Proceedings of the CSEE, 2017, 37(21):6353-6362.(in Chinese)
[4] ALKABIE H. Design methods of the ABB Alstom power gas turbine dry low emission combustion system[J]. Proceedings of the Institution of Mechanical Engineers, Part A:Journal of Power and Energy, 2000, 214(4):293-315.
[5] TSUKAGOSHI K, ARIMURA H, TANAKA K, et al. Development of air cooled combustor for Mitsubishi G class gas turbine[C]//Proceedings of the ASME Turbo Expo 2010:Power for Land, Sea, and Air. Glasgow, UK:ASME, 2010:719-723.
[6] KHOSRAVY M. Review of the new combustion technologies in modern gas turbines[M]//BENINI E. Progress in Gas Turbine Performance. Riieka:IntechOpen, 2013.
[7] ROKKE P E, HUSTAD J E, ROKKE N A, et al. Technology update on gas turbine dual fuel, dry low emission combustion systems[C]//Proceedings of the ASME Turbo Expo 2003, Collocated with the 2003 International Joint Power Generation Conference. Atlanta, USA:ASME, 2003:97-107.
[8] DAVIS L B. Dry low NOx combustion systems for GE heavy-duty gas turbines[C]//Proceedings of the ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. Birmingham, UK:ASME, 1996:57-68.
[9] ZENG W, PANG L Y, ZHENG W L, et al. Study on combustion and emission characteristics of a heavy-duty gas turbine combustor fueled with natural gas[J]. Fuel, 2020, 275:117988.
[10] RIZK N K, MONGIA H C. Lean low NOx combustion concept evaluation[J]. Symposium (International) on Combustion, 1991, 23(1):1063-1070.
[11] MOHAMMAD B S, JENG S M. Design procedures and a developed computer code for single annular combustor preliminary design[C]//Proceedings of the 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit. Denver, USA:AIAA, 2009:5208.
[12] 叶文,刘传亮,范雪飞,等. 9E燃机LEC-III燃烧室预混模式的数值计算[J].动力工程学报, 2016, 36(8):608-614, 628. YE W, LIU C L, FAN X F, et al. Numerical study on flow characteristics in LEC-III combustor liner of a 9E gas turbine under premix mode[J]. Journal of Chinese Society of Power Engineering, 2016, 36(8):608-614, 628.(in Chinese)
[13] MOORE M J. NOx emission control in gas turbines for combined cycle gas turbine plant[J]. Proceedings of the Institution of Mechanical Engineers, Part A:Journal of Power and Energy, 1997, 211(1):43-52.
[14] SHAKARIYANTS S A, VAN BUIJTENEN J P, VISSER W P J. Generic geometry definition of the aircraft engine combustion chamber[C]//Proceedings of the ASME Turbo Expo 2004:Power for Land, Sea, and Air. Vienna, Austria:ASME, 2004:173-180.
[15] LEFEBVRE A H, NORSTER E R. The design of tubular gas turbine combustion chambers for optimum mixing performance[J]. Proceedings of the Institution of Mechanical Engineers, Conference Proceedings, 1968, 183(14):150-155.
[16] SHEHATA M. Emissions and wall temperatures for lean prevaporized premixed gas turbine combustor[J]. Fuel, 2009, 88(3):446-455.
[17] KLEIN A. Characteristics of combustor diffusers[J]. Progress in Aerospace Sciences, 1995, 31(3):171-271.
[18] LEFEBVRE A H. Fuel effects on gas turbine combustion-liner temperature, pattern factor, and pollutant emissions[J]. Journal of Aircraft, 1984, 21(11):887-898.
[19] RIZK N K, MONGIA H C. Emissions predictions of different gas turbine combustors[C]//Proceedings of the 32nd Aerospace Sciences Meeting and Exhibit. Reno, USA:AIAA, 1994:118.
[20] RIZK N K, MONGIA H C. Semianalytical correlations for NOx, CO, and UHC emissions[J]. Journal of Engineering for Gas Turbines and Power, 1993, 115(3):612-619.
[21] 谢刚. R0110重型燃气轮机DLN燃烧室的性能试验与分析[D].北京:清华大学, 2010. XIE G. Performance test and analysis on the DLN combustor of R0110 heavy duty gas turbine[D]. Beijing:Tsinghua University, 2010.(in Chinese)
[22] 焦树建.燃气轮机燃烧室[M]. 2版.北京:机械工业出版社, 1990. JIAO S J. Gas turbine combustor[M]. 2nd ed. Beijing:China Machine Press, 1990.(in Chinese)
No related articles found!
Viewed
Full text


Abstract

Cited

  Shared   
  Discussed   
版权所有 © 《清华大学学报(自然科学版)》编辑部
本系统由北京玛格泰克科技发展有限公司设计开发 技术支持:support@magtech.com.cn