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高油气比下燃气分析测温探针反应冻结性能研究 被引量:1

Quenching of Reaction in a Gas-Sampling Probe for Temperature Measurement in High Fuel-to-Air Ratio Combustor
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摘要 要使用燃气分析法实现燃烧室出口温度分布的高精度测量,需要确保取样探针内燃气样本的化学反应能够快速冻结.随着航空发动机燃烧室出口温度的不断提高,化学反应冻结的难度增加.本研究通过数值模拟与化学反应动力学计算,获得了气动探针内化学反应冻结随当量比和探针落压比的变化规律,分析了探针内部化学反应冻结过程的主要影响因素与机制.研究结果表明,随着当量比增加,探针内CO相对含量的变化量先上升后下降,在当量比为0.9~1.0时最大,达5.2%.随着落压比降低,激波内吞、静温升高,最终将会导致CO、CO_(2)的相对含量的变化量大幅上升. Effective chemical quenching is needed to ensure the test accuracy of the combustor exit temperature distribution by temperature by gas analysis(TBGA).However,as the exit temperature of the combustor rises,the difficulty in chemical quenching increases.In this research,numerical simulation and chemical reaction calculation were conducted to explore the trends of quench ratio by changing the equivalence ratio and pressure ratio,respectively.The main factors in the quenching process were then analyzed.As the equivalence ratio increases,the CO change ratio increases first and then decreases,with the greatest value of 5.2%at the equivalence ratio of 0.9—1.0.As the pressure ratio decreases,a shockwave pushes back,and the static temperature rises,resulting in a drastic increase in CO and CO_(2) concentrations.
作者 杨越 薛鑫 惠鑫 林宇震 Yang Yue;Xue Xin;Hui Xin;Lin Yuzhen(National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Energy and Power Engineering,Beihang University,Beijing 100191,China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,Research Institute of Aero-Engine,Beihang University,Beijing 100191,China)
出处 《燃烧科学与技术》 CAS CSCD 北大核心 2022年第2期214-219,共6页 Journal of Combustion Science and Technology
基金 国家科技重大专项资助项目(2017-Ⅲ-0005-0029).
关键词 燃气分析测温 探针取样 化学反应冻结 temperature by gas analysis(TBGA) probe sampling chemical quenching
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  • 1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. 被引量:14
  • 2李卫东.一种根据燃气成分计算燃气温度的方法[J].中国民航学院学报,2006,24(4):23-26. 被引量:8
  • 3郑必可,陈立红,林然,张新宇.高焓超声速气体取样分析[J].航空动力学报,2006,21(6):967-971. 被引量:5
  • 4范作民 吴忆峰 张洞泉.燃气分析计算技术报告[R].四川成都:中国燃气涡轮研究院,1978..
  • 5Irvin Glassman,Combustion[M].3rd Edition,ACADEMIC PRESS,California,1996.
  • 6张新宇,陈立红.高超声速推进技术的发展前景[R].厦门:全国流体力学青年研讨会,2001.
  • 7BLUST J W,GETZ M G,ZZBARNICK S.Probe Design Optimization for the Well Stirred Reactor[R].Reno,NV:AIAA Paper,1997.
  • 8COLKET M B,Ⅲ etc.Internal Aerodynamics of Gas Sampling Probes[J].Combustion and Flame,1982,44:3-14.
  • 9TOHRU MITANI.Quenching of Reaction in Gas-sampling Probes to Measure Scramjet Engine Performance[C].Italy:The Combustion Institute,1996.
  • 10MITANI,TOHRU TAKAHASHI,et al.Measurements of Scramjet Engine Performance by Gas Sampling[R].Astronautics:AIAA Paper,1998.

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