基于激光的燃烧场温度诊断方法综述

在燃烧相关的研究中，温度场、速度场、组分场、压力场的时空分布特性非常重要.为了计算热传导、热对流和热辐射或捕捉火焰区域，最直接的方法是获取燃烧场的温度.近年来，基于激光的非接触诊断技术快速发展，Rayleigh散射温度测量、激光诱导荧光、激光诱导磷光、Raman散射测温法、相干反Stokes Raman散射、简并四波混频、可调谐二极管激光吸收光谱等技术已经被成功地应用在温度诊断研究中.文章综述了上述激光测温技术的基本工作原理和应用条件，为从事相关领域工作的研究人员提供一定的参考.      

LIPS技术测量CH_4/空气预混火焰温度

简述了激光诱导偏振光谱技术的测温原理和实验方法,并利用激光诱导偏振光谱技术测量了常压CH4/空气预混火焰的温度分布。该技术灵敏度高,且不受碰撞猝灭的影响,适于诊断各种实际的燃烧过程。通过研究激光能量与信号强度的关系,获得了激光功率密度与信号强度的关系曲线以及实验中的最佳激光功率密度;记录并测量了燃烧场中OH分子A2∑＋-X2Π（0,0）跃迁带中P 1（2）和Q 1（8）两条吸收线的强度,用双线法计算了相应的温度,给出了CH4/空气预混火焰中不同化学配比条件下燃烧场温度的空间分布,实验结果与CARS的测量结果吻合较好。     

煤油燃烧场主要组分浓度测量

利用自发振动拉曼散射技术测量了煤油燃烧场主要组分的摩尔分数。基于355nm激光激发振动拉曼散射建立了自发拉曼散射实验系统,测量了空气中主要组分的摩尔分数,分析了该技术的测量精度;测量了煤油蒸气在355nm激光激励下产生的荧光光谱,分析了荧光信号对拉曼信号的干扰;对不同燃烧条件下的煤油燃烧场进行了诊断,获得了贫油条件下煤油燃烧场主要组分(N2,O2,H2O,CO2等)的拉曼光谱,计算了组分摩尔分数及其随燃烧时间的变化规律。     

燃烧场参数的激光诊断技术研究

 介绍了燃烧场参数的激光诊断技术的研究进展，给出了用自发拉曼散射、激光诱导荧光、相干反斯托克斯拉曼散射法诊断燃烧场温度和组分的实验系统和部分实验结果，单次测量火焰的温度和组分浓度相对误差小于10%；利用平面激光诱导荧光技术获得了稳定燃烧场二维OH荧光图像，并分析了激光作用区域火焰二维温度场的分布。     

激光光谱技术在燃烧诊断中的应用

激光光谱燃烧诊断技术由于测量的非介入性、高分辨率和高灵敏度,成为了燃烧科学中的研究热点.文中综述了自发拉曼散射技术(VRS)、相干反斯托克斯拉曼散射技术(CARS)和平面激光诱导荧光技术(PLIF)的原理、方法、特点及其发展现状.并展望了它们在燃烧科学中的应用前景.     

PLIF法定量测量甲烷-空气火焰二维温度场分布

利用平面激光诱导荧光(PLIF)技术,通过选择适合的OH自由基激励线,定量测量了甲烷-空气燃烧火焰的二维温度场分布。给出炉面中心上方火焰温度随离炉面高度的变化和距炉面12 mm高处沿炉面水平方向变化的实验测量结果并进行了讨论与分析。与利用相干反斯托克斯喇曼散射（CARS）技术进行测温的实验结果相比,该测量的相对不确定度优于5％。     

单脉冲喇曼散射技术测量高压燃烧场组分浓度

介绍了自发喇曼散射技术的基本原理、实验方法及对高压燃烧场的测量结果。利用Nd:YAG激光的三倍频输出激发振动喇曼散射,在单脉冲条件下测量了高压模拟燃烧室内不同化学配比条件下以氢气-空气预混燃烧场为主要组分(N2,O2,H2O,H2等)的喇曼光谱,获得了主要组分浓度随燃烧时间、燃烧场压力的变化规律。实验中利用偏振技术有效地提高了信噪比。通过优化激光光束形状及光路设计避免了等离子体光谱对喇曼信号的干扰。     

利用拉曼散射测量燃烧场的组分浓度及温度

介绍了利用拉曼散射测量燃烧流场温度及组分浓度的物理方法和实验测量结果。利用可调谐KrF准分子激光激发振动拉曼散射（VRS）测量了甲烷－空气燃烧火焰内不同空间的主要组分分子（CH4、N2、O2、H2O等）浓度及温度,测量误差小于10％;另外用N2的拉曼谱拟合测量了火焰的温度,测量精度高于5％。在实验中采用了偏振技术及波长调谐提高了信噪比和测量精度。     

预混,圆杆稳定的V型火焰中湍流——燃烧的相互作用

一、引言 湍流燃烧具有重要的理论和实用意义。近年来随着激光测量技术和电子计算机技术的高速发展,为研究湍流和湍流燃烧提供了强有力的工具,使得湍流燃烧的理论研究和实验研究有了很大的进展。但是由于湍流燃烧本身的复杂性,湍流如何加快火焰传播速度     

基于激光的测量技术在燃烧流场诊断中的应用

分析了工业发动机湍流燃烧场诊断的需求和面临的挑战,介绍了燃烧流场组分浓度、温度和速度等主要参数的激光测量技术,给出了其基本原理、在燃烧场诊断中的应用和国内外研究现状,分析了不同技术的特点及其适用性。简介了多参数综合诊断的作用和进展。对目前诊断和测量存在的主要问题和发展趋势进行了探讨。     

Several applications of laser diagnostics for visualization of combustion phenomena

Several applications of laser diagnostic techniques to visualize combustion phenomena are presented, including reactive Mie scattering for flow, Rayleigh and Raman spectroscopy for major species, laser-induced fluorescence for minor species, and laser extinction, scattering, and laser-induced incandescence for soot. These techniques have been applied to diffusion flame oscillation, a recirculation zone in a burner, laminar and turbulent lifted flames, flame propagation along a vortex tube, and soot zone characteristics, to demonstrate the usefulness of the techniques to provide a better understanding of physical mechanisms.     

Structure and dynamic behavior of combustion visualized by 2-D laser diagnostics

This paper describes studies of structure and dynamic behavior of combustion by use of laser-aided two-dimensional flame visualization. Attentions are given to the recent development of the laser sheet imaging techniques of velocity, temperature and concentration and its application to flame visualization. Visualization of turbulent diffusion flames by use of RIV (Rayleigh scattering Image Velocimetry) and OH-PLIF conducted by the authors are presented together with the short review of laser diagnostics of combustion.     

The stabilization mechanism and structure of turbulent hydrocarbon lifted flames

The structure and stabilization mechanism of turbulent lifted non-premixed hydrocarbon flames have been investigated using combined laser imaging techniques. The techniques include Rayleigh scattering, laser induced predissociation fluorescence of OH, LIF of PAH, LIF of CH₂O, and planar imaging velocimetry. The geometrical structure of multi-reaction zones and flow field at the stabilization region have been simultaneously measured in 16 hydrocarbon flames. The data reveal the existence of triple flame structure at the stabilization region of turbulent lifted flames. Increasing the jet velocity leads to an increase of the lift-off height and to a broadening of the lift-off region. Further analysis of the stabilization criterion at the lift-off height based on the premixed nature of triple-flame propagation and flow field data has been presented and discussed.     

Laser imaging system for determination of three-dimensional scalar gradients in turbulent flames

An imaging system for the measurement of three-dimensional (3D) scalar gradients in turbulent hydrocarbon flames is described. Combined line imaging of Raman scattering, Rayleigh scattering, and CO laser-induced fluorescence (LIF) allows for simultaneous single-shot line measurements of major species, temperature, mixture fraction, and a one-dimensional surrogate of scalar dissipation rate in hydrocarbon flames, while simultaneous use of two crossed, planar LIF measurements of OH allows for determination of instantaneous flame orientation. In this manner the full 3D scalar dissipation can be estimated in some regions of a turbulent flame on a single-shot basis.     

Reaction zone structures and mixing characteristics of partially premixed swirling CH4/air flames in a gas turbine model combustor

The mixing, reaction progress, and flame front structures of partially premixed flames have been investigated in a gas turbine model combustor using different laser techniques comprising laser Doppler velocimetry for the characterization of the flow field, Raman scattering for simultaneous multi-species and temperature measurements, and planar laser-induced fluorescence of CH for the visualization of the reaction zones. Swirling CH₄/air flames with Re numbers between 7500 and 60,000 have been studied to identify the influence of the turbulent flow field on the thermochemical state of the flames and the structures of the CH layers. Turbulence intensities and length scales, as well as the classification of these flames in regime diagrams of turbulent combustion, are addressed. The results indicate that the flames exhibit more characteristics of a diffusion flame (with connected flame zones) than of a uniformly premixed flame.     

Visualization of multiple scalar and velocity fields in a lifted jet flame

The stabilization of lifted jet diffusion flames has long been a topic of interest to combustion researchers. The flame and flow morphology, the role of partial premixing, and the effects of large scale structures on the flame can be visualized through advanced optical imaging techniques. Many of the current explanations for flame stabilization can benefit from the flow and flame information provided by laser diagnostics. Additionally, the images acquired from laser diagnostic experiments reveal features invisible to the eye and line-of-sight techniques, thereby allowing a deeper insight into flame stabilization. This paper reports visualizations of flame and flow structures from Particle Image Velocimetry (PIV), Planar Laser-Induced Fluorescence (PLIF) and Rayleigh scattering. The techniques are surveyed and the success of visualization techniques in clarifying and furthering the understanding of lifted-jet flame stabilization is discussed.     

1D high-speed Rayleigh measurements in turbulent flames

Time-correlated sampling of quantities in transient combustion processes requires high-speed imaging at repetition rates in the order of typical flame-inherent frequencies. The present study demonstrates the feasibility of temperature measurements in turbulent flames along a line at 10 kHz using Rayleigh scattering. High signal intensities were gained using an 80 W Nd:YAG laser for excitation in combination with an optimized combination of an achromatic lens, an objective lens and a CMOS camera. This allowed achieving signal-to-noise ratios up to 140 at 10 kHz repetition rates. The experimental setup and data processing aspects are described as well as details on the system characteristics are given. Temperature measurements of the DLR-A jet flame with a Reynolds number of 15.200 were compared with high-quality conventional 10 Hz simultaneous Raman/Rayleigh data. The data showed excellent agreement highlighting the reliability of the here demonstrated technique.     

Two-dimensional measurement of density,velocity, and temperature in turbulent high-speed air flows by UV rayleigh scattering

Instantaneous cross-sectional images of turbulent air flows with densities on the order of one atmosphere or less can be obtained in a straightforward manner using far ultraviolet Rayleigh scattering. These images give quantitative values for the air density and show the details of turbulent structure, shock structure, and shock wave/boundary layer interactions. Two-dimensional spatial correlations taken from multiple images give the shape and extent of average turbulent structure as well as the coupling between turbulent structure and other flow features. This technique may be extended to observe velocity fields by either double pulsing the illumination source or by using a narrow linewidth atomic or molecular filter window in front of the detector array. The latter approach also yields temperature. Used in conjunction with flow marking techniques such as RELIEF, coupling between turbulent structure and velocity fluctuations can also be determined. These diagnostic techniques can be extended to combusting flows to observe instantaneous structure, mixing, flame front location, and velocity fields.