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基于火焰图像诊断的模型燃烧室燃烧不稳定特性
引用本文:郑丹伟,刘勇,张祥.基于火焰图像诊断的模型燃烧室燃烧不稳定特性[J].航空动力学报,2021,36(7):1481-1488.
作者姓名:郑丹伟  刘勇  张祥
作者单位:南京航空航天大学能源与动力学院航空发动机热环境与热结构工业和信息化部重点实验室,南京210016
基金项目:国家自然科学基金(91741118)
摘    要:提出了一种基于火焰图像诊断的旋流燃烧室燃烧不稳定特性研究方法.分析甲基滤镜下高速CCD(charge coupled device)拍摄的火焰面振荡图像,发现不稳定工况下的旋流火焰在以较高频率抖动的同时伴随着周期性的火焰脱落,其脱落信息可由火焰面轴向峰值位置体现.对CCD图像进行数字图像处理获得轮廓线,统计其边缘轴向最...

关 键 词:火焰图像  燃烧不稳定  火焰脱落频率  本征模态函数  傅里叶变换
收稿时间:2020/10/13 0:00:00

Combustion instability characteristics of model combustor based on flame image diagnosis
ZHENG Danwei,LIU Yong,ZHANG Xiang.Combustion instability characteristics of model combustor based on flame image diagnosis[J].Journal of Aerospace Power,2021,36(7):1481-1488.
Authors:ZHENG Danwei  LIU Yong  ZHANG Xiang
Institution:Key Laboratory of Aero-engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:A method for studying combustion instability of swirl combustor based on flame image diagnosis was proposed. The flame surface oscillation image taken by the high-speed CCD (charge coupled device) under the methyl filter was analyzed. It was found that the swirl flame was jittered at high frequency with periodic flame shedding, and the shedding information can be reflected by the axial peak position of the flame surface. Digital image processing was performed on the CCD image to obtain the contour line. Then the coordinates of the farthest point in the axis of its edge were counted as the peak position of the flame jittered. Based on image analysis, the flame shedding threshold was determined, the pulse timing signals when flame shedding occurred under different working conditions were obtained, and also the flame shedding frequency of each working condition was calculated. The study found that the frequency was close to the main peak of the Fourier spectrum of the respective third-order eigenmode functions of the flame jitter timing, CH* timing, and combustion chamber pressure pulsation timing signals. The existence mode and law of the unstable flame separation frequency in the time sequence signal were verified under multiple working conditions. It was found that for the combustion chamber of this model, the ignition frequency increased with the decrease of the oil-gas ratio. When the oil-gas ratio was about 0.0096, it reached the critical point of flame shedding and then presented a slow downward trend.
Keywords:flame image  combustion instability  flame shedding frequency  intrinsic mode function  Fourier transform
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