快速压缩机第一级点火拉曼散射测温技术的发展及NO-LIF检出限的确定

IF 5 Q2 ENERGY & FUELS
Raphael Dewor , Christian Schulz , Rene Daniel Büttgen , Thorsten Brands , Karl-Alexander Heufer , Hans-Jürgen Koß
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引用次数: 0

摘要

再循环NOX与两级燃料在早期燃烧过程中的相互作用尚不完全清楚,特别是在较低温度下。最近发展的动态燃烧模型试图重现这些相互作用。为了验证和改进这些新模型,需要对燃烧过程中的温度进行精确的定量测量。以前的工作使用瑞利或LIF技术,并没有达到适合动力学模型的精度。本文首次证明了利用拉曼散射在快速压缩机上进行一维空间分辨温度测量的可行性。对正戊烷作为二级燃料在一级点火过程中的温度数据进行了高精度测量。此外,需要温度数据来确定可能的NO检测限。因此,通过KrF*准分子激光激发N2的自发拉曼散射,比较了nox掺杂与未掺杂气体混合物对燃烧温度的影响。结果表明,空间分辨n2 -拉曼测温是可行的,通过对30次平均射击的研究,其精度约为3%。在第一阶段测量的温度分布表明,由于化学和热损失影响的反应性差异,燃烧体积的边缘和内部区域之间存在显著的温差。此外,当在NO掺杂的N2混合物中平均10次单次射击时,确定NO检测限为30 ppm。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of the first Raman scattering thermometry during the first stage ignition in a rapid compression machine and determination of detection limits for NO-LIF

The interaction of recirculated NOX with two-stage fuels in the early combustion process is not fully understood, especially at lower temperatures. Recently developed kinetic combustion models try to reproduce these interactions. To validate and improve these new models, accurate quantitative measurements of temperature in the combustion process are necessary. Previous works used Rayleigh or LIF techniques and have not reached an accuracy appropriate for the kinetic models. The present work demonstrates the feasibility of 1D spatially-resolved temperature measurements in a rapid compression machine with Raman scattering for the first time. The temperature data is measured with high precision during the first stage ignition of n-pentane as a two-stage fuel. Additionally, the temperature data is needed to determine possible NO detection limits. Therefore, the influence on combustion temperatures from NOX-doping are compared with undoped gas mixtures is determined by spontaneous Raman scattering of N2 excited by a KrF* excimer laser. The results show that spatially resolved N2-Raman thermometry is feasible with a precision of approximately 3 % by investigating 30 averaged shots. The measured temperature profile in the first stage reveals a remarkable temperature difference between the edges and the inner area of the combustion volume due to differences in the reactivity, which is affected by chemistry and heat loss. Additionally, the NO detection limit is determined to be 30 ppm when averaging 10 single shots during an NO-doped N2 mixture.

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