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双偏振拉曼光谱测量航空发动机燃烧场浓度和温度

Measurement of Aero-Engine Combustion Field Concentration and Temperature by Dual Polarization Raman Spectroscopy

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【作者】 于长友; 程鹏; 李杰; 宋文艳; 王朝宗; 齐新华; 车庆丰; 陈爽; 许振宇;

【Author】 YU Chang-you;CHENG Peng;LI Jie;SONG Wen-yan;WANG Chao-zong;QI Xin-hua;CHE Qing-feng;CHEN Shuang;XU Zhen-yu;College of Automotive Engineering, Department of Energy and Power Engineering, Jilin University;School of Power and Energy, Aviation Propulsion System, Northwestern Polytechnical University;Equipment Design and Testing Technology Institute of China Aerodynamics Research and Development Center;Hefei Institutes of Physical Science, Anhui Institute of Optics and Precision Machinery, Chinese Academy of Sciences;

【通讯作者】 车庆丰;

【机构】 吉林大学汽车工程学院能源与动力工程系; 西北工业大学动力与能源学院航空推进系; 中国空气动力研究与发展中心设备设计与测试技术研究所; 中国科学院合肥物质科学研究院安徽光学精密机械研究所;

【摘要】 开发了一种基于体相位全息(VPH)透射光栅的双偏振自发拉曼光谱测量系统,实现在燃烧场中单脉冲激光下同步定量测量主要气态物种组分(二氧化碳CO2、氧O2、氮N2、水H2O、燃料及中间体CxHy)浓度和温度,同步测量的温度可修正其对物种拉曼散射截面的影响。系统中的两套光栅和ICCD相机可同步采集两个互相垂直方向的拉曼散射偏振信号,有效剔除荧光干扰。在可控压力及温度的气样池和McKenna标准火焰燃烧器进行了浓度和温度的标定,温度测量精度小于1.06%,组分浓度测量精度小于1.10%。在某航空发动机模型燃烧室燃烧场中,完成了单工况三维多测点组分浓度和温度的同步单脉冲(20 ns)定量测量。

【Abstract】 A dual-polarization spontaneous Raman spectroscopy measurement system based on volume phase holographic transmission grating(VPH) has been developed, which enables synchronous quantitative measurement of the concentration and temperature of major gaseous species components(carbon dioxide CO2, oxygen O2, nitrogen N2, water H2O, fuel, and intermediates) under a single laser pulse in a combustion field. The temperature obtained synchronously can correct the influence of temperature on the Raman scattering cross-section of species. Two sets of ICCD cameras synchronously collect Raman scattering signals in two mutually perpendicular directions, effectively eliminating fluorescence interference. This system can also achieve a joint testing technology of Rayleigh temperature measurement and Raman concentration measurement. The concentration and temperature were calibrated on the gas sample pool with controllable pressure and temperature and the McKenna standard burner; the temperature measurement accuracy is less than 1.06%, and the accuracy of component concentration measurement is less than 1.10%. In the combustion field of an aero-engine model combustion chamber, the simultaneous measurement for a single pulse(20 ns) of component concentration and temperature at three multi-measurement points in a single working condition was completed.

【基金】 国家重点研发计划项目(2020YFA0405700)资助
  • 【文献出处】 光谱学与光谱分析 ,Spectroscopy and Spectral Analysis , 编辑部邮箱 ,2025年03期
  • 【分类号】V231.2
  • 【下载频次】100
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