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Simultaneous High Speed (5 kHz) Fuel-PLIF, OH-PLIF and Stereo PIV Imaging of Pressurized Swirl-Stabilized Flames using Liquid Fuels

机译:使用液体燃料同时对加压旋流稳定火焰进行高速(5 kHz)燃料PLIF,OH-PLIF和立体PIV成像

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This paper describes implementation of simultaneous, high speed (5 kHz) stereo PIV, OH and fuel-PLIF in a pressurized (up to 5.2 atm), liquid fueled, swirl stabilized flame, representative of a gas turbine combustor. The experiments were performed to characterize the flowfield, qualitative heat release and fuel spray distributions, and flame dynamics. Acquiring high speed OH-PLIF in pressurized, liquid fuel systems is difficult due to the fuel's absorption and emission spectra strongly overlapping that of the OH fluorescence spectrum. To overcome the fuel emission polluting the OH signal, the OH and fuel fluorescence signals were partially separated by using two cameras with differing spectral filters and data acquisition timing, as the emission from OH and fuel differ both in spectral width and time. The first camera captured only fuel-PLIF, while the second captured fuel-PLIF and OH-PLIF. The fuel-PLIF images were used to compute two intensity thresholds, separating each image into regions of no fuel, fuel only and an intermediate region. In the region of no fuel, OH was detected in the second camera. In the intermediate region there was a mix of fuel and OH. Instantaneous and time-averaged results are discussed showing the flow field, flame position and dynamics, and spray distribution from the fuel signal for two different multi-component liquid fuels (Jet-A and C-5), at two inlet temperatures of 450 and 570 K, and three pressure of 2.1, 3.5 and 5.2 bar. The flame shape in some cases is described as M-shaped, existing both inside and outside of the annular swirling jet produced by the nozzle, while in other cases no reaction is apparent on the inside. The spray penetration and distribution, and flame position are sensitive to the various conditions, while the flow field topology is qualitatively insensitive. Furthermore, elevated pressure as expected sharpens all spatial gradients in the data.
机译:本文介绍了在加压(最高5.2 atm),液体燃料,旋流稳定火焰(代表燃气轮机燃烧器)中实现同步,高速(5 kHz)立体PIV,OH和燃料PLIF的实现方式。进行实验以表征流场,定性放热和燃料喷雾分布以及火焰动力学。由于燃料的吸收和发射光谱与OH荧光光谱的光谱高度重叠,因此在加压的液体燃料系统中获取高速OH-PLIF非常困难。为了克服污染OH信号的燃料排放,使用两个具有不同光谱滤光器和数据采集时间的摄像机将OH和燃料荧光信号部分分离,因为OH和燃料的发射在光谱宽度和时间上都不同。第一个相机仅捕获燃料PLIF,而第二个相机捕获燃料PLIF和OH-PLIF。燃料PLIF图像用于计算两个强度阈值,将每个图像分为无燃料区域,仅燃料区域和中间区域。在没有燃料的区域中,第二台摄像机检测到OH。在中间区域,混合了燃料和OH。讨论了瞬时和时间平均的结果,这些结果显示了两种不同的多组分液体燃料(Jet-A和C-5)在两个进气温度分别为450和450℃时的流场,火焰位置​​和动力学以及来自燃料信号的喷雾分布。 570 K,三个压力分别为2.1、3.5和5.2 bar。在某些情况下,火焰形状被描述为M形,存在于喷嘴产生的环形旋流的内部和外部,而在其他情况下,内部则看不到任何反应。喷雾的渗透和分布以及火焰位置对各种条件都很敏感,而流场拓扑在质量上不敏感。此外,如预期的那样,压力升高会锐化数据中的所有空间梯度。

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