论文:2020,Vol:38,Issue(1):104-113
引用本文:
李乐, 索建秦, 于涵, 郑龙席. 燃气分析系统优化设计及应用研究[J]. 西北工业大学学报
LI Le, SUO Jianqin, YU Han, ZHANG Longxi. Optimal Design and Application of Gas Analysis System[J]. Northwestern polytechnical university

燃气分析系统优化设计及应用研究
李乐, 索建秦, 于涵, 郑龙席
西北工业大学 动力与能源学院, 陕西 西安 710072
摘要:
为了实现高温、高压环境下航空发动机燃烧室出口温度、燃烧效率、污染排放等性能参数的准确测量,对现有的燃气取样及分析系统进行了优化设计,对数据后处理方法进行了修正,并建立了适用于燃烧室出口温度计算的全成分焓值守恒法。基于贫油直接喷射低污染燃烧室对燃气分析系统和数据后处理方法进行了性能评估和应用研究。研究结果表明:优化后的燃气分析系统符合国际民航组织的污染排放测量要求,并且该系统响应时间快、数据有效性高;通过对比燃气分析法和传统测量方法,燃气分析法精度更高、工作范围更宽、稳定性更好,能够准确评估燃烧室出口温度、燃烧效率和污染排放等性能。
关键词:    燃气分析    取样耙    低污染    燃烧室    焓值守恒法   
Optimal Design and Application of Gas Analysis System
LI Le, SUO Jianqin, YU Han, ZHANG Longxi
School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:
To accurately measure the performance parameters of an aero-engine combustor under high-temperature and high-pressure environment, such as outlet temperature, combustion efficiency and pollutant emission, the optimal design of the existing gas sampling and analysis system was carried out, the data post-processing method was corrected, and the full-component enthalpy conservation method suitable for calculating combustor outlet temperature was established. A lean direct injection and low-pollution combustor was used to evaluate the performance and application of its gas analysis system and its data post-processing method. The investigation results indicate that the optimized gas analysis system meets the International Civil Aviation Organization's pollutant emission measurement requirements and that it has a fast response and a high data quality. The comparison of the measurement results of the gas analysis system with those of the traditional measurement methods shows that the gas analysis system has a more accurate measurement, a wider condition range and a better stability, thus accurately evaluating the outlet temperature, combustion efficiency and emission characteristics of a gas turbine combustor.
Key words:    gas analysis    sampling rake    low emission    combustor    enthalpy conservation method   
收稿日期: 2019-01-16     修回日期:
DOI: 10.1051/jnwpu/20203810104
基金项目: 国家科技重大专项(2017-Ⅲ-0002-0026)资助
通讯作者:     Email:
作者简介: 李乐(1991-),西北工业大学博士研究生,主要从事航空发动机燃烧技术研究。
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参考文献:
[1] 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(in Chinese)
[2] 张弛, 林宇震, 徐华胜, 等. 民用航空发动机低排放燃烧室技术发展现状及水平[J]. 航空学报, 2014, 35(2):332-350 ZHANG Chi, LIN Yuzhen, XU Huasheng, et al. Development Status and Level of Low Emissions Combustor Technologies for Civil Aero-Engine[J]. Chinese Journal of Aeronautics, 2014, 35(2):332-350(in Chinese)
[3] 王明瑞, 王振华, 韩冰, 等. 航空发动机主燃烧室高温测量技术[J]. 航空发动机, 2016, 42(5):87-93 WANG Mingrui, WANG Zhenhua, HAN Bing, et al. High Temperature Measurement Technology for Main Combustor Chamber of Aeroengine[J]. Aeroengine, 2016, 42(5):87-93(in Chinese)
[4] WILLIAMSON R C, STANFORTH C M. Measurement of Jet Engine Combustion Temperature by the Use of Thermocouples and Gas Analysis[J]. SAE-Tech-690433
[5] Sanford Gordon, Bonnie J McBride. Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouguet Detonations[R]. NASA SP-273
[6] ZHUOHUI J H, CHANGLIE W, CLARENCE T C, et al. Emissions Characteristics of a P&W's Axially Staged Sector Combustors[C]//AIAA Sci Tech Forum, San Diego, California, 2016
[7] KATHLEEN M T, DEREK P P, ZHUOHUI J H, et al. A Comparison of Three Second-Generation Swirl-Venturi Lean Direct Injection Combustor Concepts[C]//AIAA Propulsion and Energy Forum, Salt Lake City, 2016
[8] CIEZKI H, SCHEEL F, KWAN W. Investigation of the Combustion Process in a Scramjet Model Combustor with a Sampling Probe System[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, 2004
[9] 李亚娟, 王明瑞, 葛新, 等. 基于燃气分析法的航空发动机燃烧室性能研究[J]. 航空发动机, 2016, 42(1):37-41 LI Yajuan, WANG Mingrui, GE Xin, et al. Research on Aeroengine Combustor Performance Based on Gas Analysis Method[J]. Aeroengine, 2016, 42(1):37-41(in Chinese)
[10] 李亚娟, 王明瑞, 韩冰, 等. 燃气分析法测试燃气轮机主燃烧室燃烧效率、气态污染物误差分析[J]. 航空动力学报, 2017, 32(5):1051-1057 LI Yajuan, WANG Mingrui, HAN Bin, et al. Gas Turbine Primary Combustor Error Analysis of Combustion Efficiency and Exhaust Emission Using Gas Analysis Method[J]. Journal of Aerospace Power, 2017, 32(5):1051-1057(in Chinese)
[11] Society of Automotive Engineers. Aircraft Gas Turbine Engine Exhaust Smoke Measurement[R]. SAE ARP 1179, 2011
[12] Society of Automotive Engineers. Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines[R]. SAE ARP 1256D, 2011
[13] 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 Inject(LDI) Combustor[J]. Journal of Northwestern Polytechnical University, 2018, 36(5):816-823(in Chinese)
[14] 尉署名. 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 Jiaotong University Press, 2014(in Chinese)
[15] 李乐. 飞机发动机燃气分析系统设计与实现[D]. 西安:西北工业大学, 2018 LI Le. Design and Implementation of Aircraft Engine Gas Analysis System[D]. Xi'an:Northwestern Polytechnical University, 2018(in Chinese)
[16] 刘高恩, 王华芳, 吕品, 等. 飞机发动机排气污染物的测量[J]. 航空动力学报, 2003, 18(3):348-352 LIU Gaoen, WANG Huafang, LYU Pin, et al. Gas Turbine Engine Emission Measurement[J]. Journal of Aerospace Power, 2003, 18(3):348-352(in Chinese)
[17] 王明瑞, 肖阳, 韩冰, 等. 航空燃气涡轮发动机燃气分析测试及计算方法[J]. 航空动力学报, 2015, 30(11):2568-2574 WANG Mingrui, XIAO Yang, HAN Bing, et al. Temperature Field Test for Aeroengine Combustor with Five Nozzles Based on Gas Analysis[J]. Journal of Aerospace Power, 2015,30(11):2568-2574(in Chinese)
[18] 杜声同, 严传俊. 航空燃气轮机燃烧与燃烧室[M]. 西安:西北工业大学出版社, 1994 DU Shengtong, YAN Chuanjun. Combustion and Combustor of Aeroengine[M]. Xi'an:Northwestern Polytechnical University Press, 1994(in Chinese)
[19] PHILIP P W, PAUL F. Gas Turbine Performance[M]. 2nd Ed. Blackwell Science, 2014
[20] 钟华贵, 吉洪湖, 李继保. 燃气分析测量高温燃气温度的方法[J]. 航空动力学报, 2005,20(3):460-466 ZHONG Huagui, JI Honghu, LI Jibao. Methods for Gas Temperature Measurement by Gas Analysis[J]. Journal of Aerospace Power, 2005,20(3):460-466(in Chinese)
[21] National Institute of Standards and Technology. NIST-JANAF Thermochemical Tables[EB/OL]. (2016-01-29)[2018-12-15]. https://janaf.nist.gov/
[22] Society of Automotive Engineers. Procedure for the Analysis and Evaluation of Gaseous Emissions from Aircraft Engines[R]. SAE ARP 1533, 2013