炸药爆轰瞬态温度的光谱法测定

在双谱线原子发射光谱测温原理的基础上,设计了对炸药爆轰的瞬态温度进行实时测量的光纤光谱测试系统,利用光学纤维将炸药爆轰的光谱信号传入测光系统,用多通道数据采集器处理数据,系统的时间分辨率可高达0.1μs,所选择的两条谱线的波长分别为CuI 510.5和CuI 521.8nm,为炸药爆温的测量提供了一种简单有效的方法。利用该测温系统,通过对炸药爆轰光谱的测量,获得了实时瞬态爆轰温度-时间分布曲线。     

导爆管起爆器瞬态电火花温度的光谱法测定

应用双谱线原子发射光谱测温法的原理，建立了一套石英光导纤维传输的瞬态实时双谱线测温系统，它的时间分辨率最高可达0.1цs，所采用的两条谱线的波长分别为Cu I 510.5和Cu I 521.8nm。利用该套装置，研究了在不同电压下导爆管起爆器的放电火花温度随时间的变化，以及不同放电条件下的电火花持续时间。试验表明：对给定的起爆器火花的温度，是在2100-4200K范围内变化，放电时间随充电电压的提高而增长。     

原子发射光谱双谱线法测量固体火箭发动机内燃气温度

发展了一种利用原子发射双谱线法，测试固体火箭发动机燃烧室内燃气温度的方法，设计了相应的测试系统。该方法利用石英光学纤维，将固体火箭发动机内高温高压燃气的光谱辐射信号传入测量系统；选用了两条波长间隔小的谱线，大大减少了光谱辐射率，光谱透射率等对光谱测量的影响，设计使用了耐压测量探头，保证在高压，强腐蚀条件下，系统的密封性和光的透过率，对装填有SQ－2推进剂的固体火箭发动机燃烧室内的气流温度进行了在线检测，测量时间分辨率可高达0．5μs。     

原子发射双谱线法测火焰温度的实验研究

通过光谱仪测量火焰中K(766.5,769.9 nm)原子发射谱线的相对强度比来获得火焰温度。介绍了测量原理、测量方法、实验系统。在黑体炉炉膛达到热力学平衡状态下,进行原子发射双谱线法和热电偶测温的对比实验,结果两种方法所测温度相关性较好,实验证明了该方法的可行性。用该方法测量煤粉和木材的火焰温度,结果和实际相符合。     

燃烧状态及煤粉粒径对火焰光谱的影响

本文利用CCD光纤光谱仪,对不同燃烧状态下的煤粉火焰光谱进行测量。发现通过光谱法测得的火焰温度和使用热电偶测得的火焰温度存在一定的偏差。光谱法的温度较热电偶的温度高100-700℃,燃烧条件变差时热电偶的温度下降,光谱法的温度升高,两者偏差增大,光谱法温度的波动范围增加。随着一次风煤粉浓度下降, K的发射谱线强度下降。相同燃烧条件下,煤粉细度提高使得光谱法测得的温度下降,温度波动加剧。     

火焰特征发射谱线研究

本文利用CCD光纤光谱仪,通过实验确定了木基燃料燃烧火焰光谱中出现的特征谱线是K,Na 的原子发射谱线,测定了特征谱线出现时的火焰温度,指出可以通过特征谱线的出现与否来确定火焰的温度范围。还发现火焰的光谱形状和火焰的燃烧状态密切相关,包含大量和燃烧有关的信息,并且对煤烟颗粒有较强的抗干扰性。通过对火焰光谱形状的分析可判断出火焰的燃烧状况,进行燃烧诊断。     

激光诱导击穿火焰等离子体光谱研究

采用PI-MAX-II型增强型电荷耦合器件, 用Nd:YAG纳秒脉冲激光器输出的1064 nm强光束击穿在一个大气压的空气中燃烧的酒精灯火焰, 对激光诱导击穿酒精灯火焰产生的等离子体光谱进行了初步研究. 根据美国国家标准与技术研究院原子发射谱线数据库, 对等离子体中的主要元素的特征谱线进行了标识和归属. 通过激光诱导击穿空气等离子体光谱、激光诱导击穿酒精灯火焰等离子体光谱、激光诱导酒精喷灯火焰等离子体光谱的对比分析, 发现不同燃烧状况下的光谱中各原子谱线的相对强度是不同的. 这些结果对于使用激光诱导击穿技术分析和研究碳氢燃料在空气中的燃烧特性具有重要的意义和参考价值, 同时也为将该技术应用于燃烧诊断提供了实验依据.     

大气颗粒物重金属元素分析技术研究进展

大气颗粒物已经成为当前大气环境首要污染物,而其中重金属由于具有非降解性和滞后性,严重威胁人类生命和自然环境,已成为当前研究热点。对分析大气颗粒物中重金属元素所用原子吸收光谱法、电感耦合等离子体原子发射光谱法、电感耦合等离子体质谱法、荧光光谱法、中子活化法、辉光放电原子发射光谱法、微波等离子体原子发射光谱法和激光诱导击穿光谱法进行了综述,并尝试对这些技术的不足之处提出一些改进建议：连续光源原子吸收光谱法同时测定多种元素,原子发射光谱法直接测定颗粒物,高分辨率激光剥蚀电感耦合等离子质谱法测定固体样品,低散射同步加速荧光法测定大气颗粒物和k₀中子活化法测定对流层发射性元素。大气颗粒物重金属元素的时空分布差异和人类对环境空气质量要求的提高以及现代仪器科学技术的高速发展促使大气颗粒物重金属元素分析技术朝着实时、快速、检出限低、直接测定和操作简便的方向发展。     

富氧空气-乙炔火焰原子吸收光谱法测定钙和镁的研究

空气-乙炔火焰原子吸收光谱法常用于对钙、镁的测定,但由于火焰温度低,化学干扰严重,结果不太理想;氧化二氮-乙炔火焰虽然可消除化学干扰,但需考虑电离效应,且耗气量大,氧化二氮不易得到。翁永和等报导了用富氧空气-乙炔火焰原子吸收光谱法测定铝的研究,并指出这是一种很有前途的新型高温火焰。     

基于辐射法和原子发射光谱法的转炉口火焰温度测量

转炉炼钢的终点控制包括钢水出钢时温度及其成分的控制,炉口火焰能够反映炉内脱碳速率及转炉运行参数等。工业炉燃烧火焰可见光谱段,普遍存在着钾(K)和钠(Na)等碱金属元素的原子发射谱线,利用K的特征谱线相对比值可以计算火焰温度。基于辐射双色法,三色法和谱线相对强度法对转炉口火焰温度进行了测量;数据处理过程中对特征谱线进行了基线拟合提取,小波脊线拟合提取;特征谱线进行了Gauss函数和Lorenz函数拟合。结果表明,辐射测温法对谱线比较敏感,选择合理的波段能够有效,精确地测量火焰温度;采用谱线相对强度法受制于特征谱线的数学模型、谱线的跃迁机率、能级的简并度及火焰的光学厚度,需要分辨率非常高的光谱仪才能进行高温转炉火焰中电子温度的测量。     

Studies on Temporal Resolution Characteristics of Flame Temperature for Flame Atomic Absorption Spectroscopy

In this paper we report a method and experiment system developed by us to useful for temporal and spatial temperature distribution of the flame for atomic obsorption spectroscopy in detail. The method and system principle is based on the modified sodium line reversal method. The studies on temporal (20–50 μsec range) and spatial (π 1mm) resolution of the flame temperature aim at establishing optimum analysis conditions and improving analysis characteristics of flame atomic absorption/emission spectroscopy.     

FTIR光谱遥测红外药剂的燃烧温度

本文利用遥感FTIR光谱，对红外药剂的燃烧特性进行了研究。在分辨率为4cm^-1时，收集4700－740cm^-1波段的光谱。从HF等燃烧产物发射的分子振转基带精细结构的谱线强度分布，可以对燃烧温度进行遥感测定，并给出了燃烧温度随时间的变化关系，实验结果表明燃烧表面附近温度梯度很大，存在着急剧的变化温度场，同时也说明，在不干扰火焰温度场的情况下，利用遥感FTIR光谱对剧烈的、非稳态快速燃烧的火焰温度进行连续实时的遥感测量，是一种快速、准确、灵敏度高的测温方法，显示了它在燃烧温度测量、产物浓度测试以及燃烧机理研究等方面的应用前景。     

Two-photon polarization spectroscopy applied for quantitative measurements of atomic hydrogen in atmospheric pressure flames

Two-photon – polarization spectroscopy has been applied for the first time to determine absolute number densities and kinetic temperatures of atomic hydrogen via the 1 S–2 Stransition in flames at atmospheric pressure. This sensitive laser spectroscopic technique, so far mainly developed and applied for quantitative plasma diagnostics, is also well suited for real combustion processes, because the signal is directly related to the two-photon absorption itself and therefore not limited by quenching or photo-ionization. It can be applied with high spatial and temporal resolution in a wide range of pressure and temperature. Furthermore, a well-established calibration procedure allows for a precise determination of the absolute ground-state density of atomic hydrogen. The measurements also demonstrate that a certain potential of this method comes especially into its own in conjunction with laser radiation of highest spectral quality, i.e. pulsed single-longitudinal mode UV radiation.     

利用辐射光谱法在线测量固体火箭推进剂燃烧温度

针对固体火箭发动机恶劣环境下的高温燃烧测量问题,提出了利用辐射光谱法来开展固体火箭推进剂燃烧温度在线测量的方法,采用200～1 100 nm光纤光谱仪测量了高压实验燃烧器下固体火箭推进剂燃烧火焰辐射光谱,总结了其光谱特性,并基于普朗克定律和光谱拟合方法获得了相应的推进剂燃烧温度,这对固体火箭推进剂燃烧诊断与燃烧机理研究具有重要的参考价值。     

一种测量发光火焰温度的数据处理方法研究

火焰温度是燃烧诊断的重要参数之一,它对研究各种燃烧过程具有重要价值。根据多光谱辐射测温所用的参考温度数学模型,提出了一种基于遗传算法的新的数据处理方法。该方法对火焰发射率与波长的关系依次进行了三点直线拟合,并通过遗传算法进行了优化,从而得到了发光火焰的温度和发射率。采用多波长高温计测量了某种固体推进剂燃烧火焰的自辐射光谱,并进行了数据处理。计算结果表明:火焰温度计算值与理论值之差在±100K以内;这种基于遗传算法的新的数据处理方法是测量发光火焰温度的一种可行性方法。     

旋流火焰燃烧温度场二维吸收光谱诊断

针对旋流火焰的复杂流场结构，结合可调谐二极管吸收光谱技术（tunable diode laser absorption spectroscopy，TDLAS）和多光谱层析成像术（hyperspectral tomography，HT），发展了具有空间分辨能力的二维吸收光谱测量技术（tunable diode laser absorption tomography，TDLAT），实现了甲烷/空气旋流火焰不同高度的二维温度场测量.该TDLAT系统吸收波长为7 185.6，7 444.3，6 807.8和7 466.3 cm-1四线，采用分时-直接吸收探测策略，测量频率2.5 kHz，采用13×13路正交光路（空间分辨率7 mm），采用模拟退火算法进行数据重建.经与理论计算结果对比分析，重建结果真实地反映了旋流火焰温度场的二维分布.      

Analysis of Aluminum Dust Cloud Combustion Using Flame Emission SpectroscopySCIEI北大核心CSCD

In this study, aluminum flame analysis was researched in order to develop a measurement method for high-energy-density metal aluminum dust cloud combustion, and the flame temperature and UV-VIS-IR emission spectra were precisely measured using a spectrometer. Because the micron-sized aluminum flame temperature was higher than 2 400 K, Flame temperature was measured by a non-contact optical technique, namely, a modified two-color method using 520 and 640 nm light, as well as by a polychromatic fitting method. These methods were applied experimentally after accurate calibration. The flame temperature was identified to be higher than 2 400 K using both methods. By analyzing the emission spectra, we could identify AlO radicals, which occur dominantly in aluminum combustion. This study paves the way for realization of a measurement technique for aluminum dust cloud combustion flames, and it will be applied in the aluminum combustors that are in development for military purposes.     

Analysis of Aluminum Dust Cloud Combustion Using Flame Emission Spectroscopy

In this study, aluminum flame analysis was researched in order to develop a measurement method for high-energy-density metal aluminum dust cloud combustion, and the flame temperature and UV-VIS-IR emission spectra were precisely measured using a spectrometer. Because the micron-sized aluminum flame temperature was higher than 2 400 K, Flame temperature was measured by a non-contact optical technique, namely, a modified two-color method using 520 and 640 nm light, as well as by a polychromatic fitting method. These methods were applied experimentally after accurate calibration. The flame temperature was identified to be higher than 2 400 K using both methods. By analyzing the emission spectra, we could identify AlO radicals, which occur dominantly in aluminum combustion. This study paves the way for realization of a measurement technique for aluminum dust cloud combustion flames, and it will be applied in the aluminum combustors that are in development for military purposes.     

Simultaneously calibrated two-line atomic fluorescence for high-precision temperature imaging in sooting flames

Simultaneously calibrated, non-linear two-line atomic fluorescence (SC-nTLAF) thermometry for application in turbulent sooting flames has been developed to increase the precision of single-shot, planar measurements of gas temperature. The technique has been demonstrated in both steady and turbulent sooting flames, showing good agreements with previous optical measurements. The SC-nTLAF involves imaging simultaneously laser-induced fluorescence (LIF) of atomic indium in both the target flame and a non-sooting calibration flame for which the temperature distribution is known. The LIF intensities from the reference flame enable correction for fluctuations, not only in the laser power, but also in the laser mode. The resulting precision was found to be ±67 K and ±75 K (based on one standard deviation) in the rich and oxidizing regions of a steady sooting flame for which the measured temperature was 1610 K and 1854 K, respectively, with a spatial resolution of 550 × 550 µm². This corresponds to a relative precision of ∼ 4.1%. The resulting precision in the single-shot temperature images for a well-characterized, lifted ethylene jet diffusion flame (fuel jet Reynolds number = 10,000) compares favorably with previously reported data obtained with shifted-vibrational coherent anti-Stokes Raman spectroscopy (CARS), together with increased spatial resolution. The planar imaging also provides more details of the temperature distribution, particularly in the flame brush region, which offers potential for measurement of more parameters, such as gradients and spatial corrections. The new calibration method has also achieved a significant time-saving in both data collection and processing, which is an estimated total of ∼ 60%–70% compared with conventional nTLAF.