Experimental study on temperature measurement of high pressure combustion based on filtered Rayleigh scattering technology
-
摘要: 为实现高压、受限空间条件下燃烧火焰二维温度场的测量,研究了基于碘分子超精细吸收凹陷的滤波瑞利散射技术。设计了一套滤波瑞利散射温度测量装置,主要由种子激光注入Nd:YAG激光器、碘分子滤波池、ICCD相机等组成。利用该测量装置,在高压火焰炉上开展了0.1~0.5MPa条件下的甲烷/空气预混火焰温度测量实验,结果表明:滤波瑞利散射测温技术能有效抑制米散射和背景杂散光的干扰,能在受限空间和带压条件下获得瞬态燃烧火焰温度场的分布,并且温度测量的相对不确定度优于15%;与热电偶温度测量实验的结果进行了对比,两者的偏差小于10%。因此,有望将滤波瑞利散射测温技术应用于发动机燃烧场温度诊断实验。Abstract: In order to explore the temperature measuring ability under the high-pressure condition and in a confined space, the filtered Rayleigh scattering technique is developed based on the iodine molecular ultrafine absorption. The filtered Rayleigh scattering temperature measuring apparatus, consisted of the seed laser, the Nd:YAG laser, the iodine molecule filter and the ICCD camera, is designed. And the iodine filter is used to remove the stray light interference from the soot and wall reflection. Moreover, this apparatus is applied on a high-pressure gas combustor (0.1~0.5MPa) to obtain the temperature distribution above the flat burner quantitatively. The results show that the relative uncertainty in the single-shot imaging is estimated to be about 15%. And a better than 10% agreement to the single point measurement is achieved by the thermocouple. Therefore, the filtered Rayleigh scattering technique is expected to be applied in the temperature measurement of the engine combustion.
-
图 8 (a) 经滤波瑞利散射技术得到的火焰温度分布图像;(b)不同腔压下,火焰炉上方1.5cm处的火焰温度分布图; (c)不同探测位置处,热电偶和FRS (50幅平均)温度测量结果
Figure 8. (a) Images of combustion temperature distribution by the FRS technique; (b) Distribution of combustion temperature at the height (1.5cm) above the burner; (c) Comparison of the temperature results between the FRS technique and the thermocouple
表 1 带压燃烧实验参数(压强p,甲烷和空气流量QCH4、QAir,当量比φ及其预混燃气总流速vpremixed)
Table 1. Parameters for combustion experiments (Chamber pressure p, flow rates for air through burner QAir and for fuel CH4 QCH4, equivalence ratios φ, premixed gas velocity vpremixed)
p/MPa QCH4/SLM QAir/SLM φ vpremixed/(cm·s-1) Case 1 0.11 0.6 4.8 1.19 16.67 Case 2 0.30 0.6 4.8 1.19 6.11 Case 3 0.50 0.6 4.8 1.19 3.67 -
[1] Liu J R, Hu Z Y, Zhang Z R. Laser spectroscopy applied to combustion diagnostics[J]. Optics and Precision Engineering, 2011, 19(2):284-296. doi: 10.3788/OPE.20111902.0284 [2] Fourguette D C, Zurni R M, Long M B. Two dimensional Rayleigh thermometry in a turbulent nonpremixed Methane-Hydrogen flame[J]. Combustion Science Technology, 1986, 44(30):307-317. doi: 10.1080-00102208608960310/ [3] 俞刚, 范学军.超声速燃烧与高超声速推进[J].力学进展, 2013, 43(5):449-454. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=lxjz201305001Yu G, Fan X J. Supersonic combustion and hypersonic propul-sion[J]. Progress in Mechanics, 2013, 43(5):449-454. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=lxjz201305001 [4] McMillin B K, Palmer J L, Seitzman J M, et al. Two line instantaneous temperature imaging of NO in a scramjet model flow-field[R]. AIAA-93-0044, 1993. [5] Seitzman J M, Palmer J L, Antonio A L. Instantaneous planar thermometry of shock-heated flows using PLIF of OH[R]. AIAA-93-0802, 1993. [6] Elliott G S, Glumac N. Molecular filtered Rayleigh scattering applied to combustion turbulence[R]. AIAA-99-0643, 1999. [7] Elliott G S, Glumac N, Carter C D. Molecular filtered Rayleigh scattering applied to combustion[J]. Measurement Science and Technology, 2001, 12(4):452-466. doi: 10.1088/0957-0233/12/4/309 [8] Miles R B, Lempert W R. Two-dimensional measurement of density, velocity, and temperature in turbulent high-speed air flows by UV Rayleigh scattering[J]. Applied Physics B, 1990, 51(4):1-7. doi: 10.1007/BF00332317 [9] Forkey J N, Lempert W R, Miles R B. Corrected and calibrated I2 absorption model at frequency-doubled Nd:YAG laser wavelengths[J]. Applied Optics, 1997, 36(27):6729-6738. doi: 10.1364/AO.36.006729 [10] Hoffman D, Munch K U, Leipertz A. Two-dimensional temperature determination in sooting flames by filtered Rayleigh scattering[J]. Opt Lett, 1996, 21(7):525-527. doi: 10.1364/OL.21.000525 [11] Doll U, Fischer M, Stockhausen G, et al. Frequency scanning filtered Rayleigh scattering in combustion experiments[C]//Proc of the 16th International Symposium on Applications of Laser Techniques to Fluid Mechanics. 2012. [12] Doll U, Stockhausen G, Willert C. Pressure, temperature, and three-component velocity fields by filtered Rayleigh scattering velocimetry[J]. Optical Letter, 2017, 42(19):3773-3776. doi: 10.1364/OL.42.003773 [13] Schroll M, Doll U, Stockhausen G, et al. Flow field characterization at the outlet of a lean burn single-sector combustor by laser-optical methods[J]. Journal of Engineering for Gas Turbines and Power, 2017, 139(6):011503. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=3563e908fdf24b72e33bde6ff0a76bc4 [14] 王晟, 刘晶儒, 胡志云, 等.用于燃烧场诊断的分子滤波瑞利散射技术[J].光学精密工程, 2011, 19(2):445-461. http://d.old.wanfangdata.com.cn/Periodical/gxjmgc201102032Wang S, Liu J R, Hu Z Y, et al. Development of filtered Rayleigh scattering for combustion diagnostic application[J]. Optics and Precision Engineering, 2011, 19(2):445-461. http://d.old.wanfangdata.com.cn/Periodical/gxjmgc201102032 [15] 郑尧邦, 陈力, 苏铁, 等.滤波瑞利散射测温技术研究[C]//中国空气动力学会测控技术专委会学术交流会论文集. 2013. http://www.wanfangdata.com.cn/details/detail.do?_type=conference&id=8056120Zheng Y B, Chen L, Su T, et al. Study on the temperature measurement by filtered ray-leigh scattering[C]//Proc of Academic Exchange Meeting of China Aerodynamic Society Measurement and Control Technical Committee. 2013. http://www.wanfangdata.com.cn/details/detail.do?_type=conference&id=8056120 [16] Tenti G, Boley C D, Desai R C. On the kinetic model description of Rayleigh-Brillouin scattering from molecular gases[J]. Canadian Journal of Physics, 1974, 52(2):285-290. [17] Pan X, Shneider M N, Miles R B. Coherent Rayleigh-Brillouin scattering in molecular gases[J]. Physical Review A, 2004, 69(3):33814-33822. doi: 10.1103/PhysRevA.69.033814