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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Spatiotemporal Distribution of Soot Temperature for Flames Using Optical Pyrometry Under Unsteady Inlet Airflow Conditions
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Spatiotemporal Distribution of Soot Temperature for Flames Using Optical Pyrometry Under Unsteady Inlet Airflow Conditions

机译:不稳定入口气流条件下光学高温法测定火焰烟ot温度的时空分布

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摘要

Two pyrometric tools for measuring soot temperature response in fuel-rich flames under unsteady inlet airflow conditions are developed. High-speed pyrometry using a high-speed color camera is used in producing soot temperature distributions, with its results compared with those of global soot temperature response measured using a multiwave-length pyrometer. For the former, the pixel red, green, and blue (RGB) values pertaining to respective bandwidths of red, green, and blue filters are used to calculate temperature and for the latter, the emission from whole flame at 660 nm, 730 nm, and 800 nm is used to measure temperature. The combustor, running on jet-A fuel, achieves unsteady inlet airflow using a siren running at frequencies of 150 and 250 Hz and with modulation levels (root mean square (RMS)) 20-50% of mean velocity. Spatiotemporal response of flame temperature measured by the high-speed camera is presented by phase-averaged with average subtracted images and by fast Fourier transform (FFT) at the modulation frequencies of inlet velocity. Simultaneous measurement of combustor inlet air velocity and flame soot temperature using the multiwavelength pyrometer is used in calculating the flame transfer function (FTF) of flame temperature response to unsteady inlet airflow. The results of global temperature and temperature fluctuation from the three-color pyrometer show qualitative agreement with the local temperature response measured by the high-speed camera. Over the range of operating conditions employed, the overall flame temperature fluctuation increases linearly with respect to the inlet velocity fluctuation. The two-dimensional map of flame temperature under unsteady combustion determined using a high-speed digital color camera shows that the local temperature fluctuation during unsteady combustion occurs over relatively small region of flame and its level is greater (~10% to 20%) than that of overall temperature fluctuation (~1%).
机译:开发了两种高温计工具,用于在不稳定的进气气流条件下测量富含燃料的火焰中烟灰温度响应。使用高速彩色相机进行的高速高温测定法用于产生烟灰温度分布,其结果与使用多波长高温计测得的全球烟灰温度响应的结果相比。对于前者,分别使用与红色,绿色和蓝色滤光片各自带宽有关的像素红色,绿色和蓝色(RGB)值来计算温度,对于后者,则使用整个火焰在660 nm,730 nm处的发射, 800 nm用于测量温度。使用喷气A燃料运行的燃烧器使用警笛以150和250 Hz的频率运行,并具有平均速度20-50%的调制水平(均方根(RMS))来实现不稳定的进气流。高速相机测得的火焰温度的时空响应是通过平均相减图像并在入口速度的调制频率下通过快速傅立叶变换(FFT)来表示的。使用多波长高温计同时测量燃烧室进气速度和烟灰温度,可用于计算火焰温度对不稳定进气流量的火焰传递函数(FTF)。三色高温计的总体温度和温度波动的结果与高速相机测得的局部温度响应在质量上吻合。在所采用的工作条件范围内,总火焰温度波动相对于入口速度波动线性增加。使用高速数字彩色摄像机确定的非稳态燃烧下火焰温度的二维图显示,非稳态燃烧过程中的局部温度波动发生在相对较小的火焰区域上,并且其水平大于(〜10%至20%)整体温度波动(〜1%)。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2017年第5期|051502.1-051502.8|共8页
  • 作者单位

    Combustion Research Laboratory, School of Aerospace Systems, University of Cincinnati, Cincinnati, OH 45220;

    Combustion Research Laboratory, School of Aerospace Systems, University of Cincinnati, Cincinnati, OH 45220;

    Combustion Research Laboratory, School of Aerospace Systems, University of Cincinnati, Cincinnati, OH 45220;

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