期刊文献+

基于全连接神经网络的分层旋流火焰燃烧振荡预报 被引量:3

Prediction of Combustion Oscillation Based on Time-Averaged Images of Stratified Swirl Flame Using Fully-Connected Neural Network
下载PDF
导出
摘要 为了指导主动控制系统抑制燃烧振荡,有必要针对不同的燃烧振荡预报手段开展研究和验证。以甲烷预混同心分层旋流火焰的时均图像为基础,采用降低图像分辨率和提取火焰结构特征参数这两种不同的方式对火焰图像信息进行简化处理,并使用全连接神经网络对燃烧振荡进行预报研究。结果发现,两种方式都可以较为准确地预报燃烧振荡,精度均达到90%以上。预报精度随着图像分辨率的增加而升高,在极低的图像分辨率(3×3)下,预报精度也能达到90%以上。此外,对根据火焰平均图像提取的结构特征参数进行了敏感性分析,捕捉到了系统稳定性的转变,但参数变化范围受训练集限制。提出的基于数据驱动方法对燃烧振荡的预报时间<2ms,为实现燃烧振荡实时在线预报提供了支持。 In order to guide the active control system to suppress the combustion instabilities,relevant researches on combustion oscillation prediction based on different methods should be carried out to verify their availabilities.The time-averaged images of premixed internally-staged-swirling stratified flame of CH4 are adopted here as the basis of our research.In order to simplify the information contented in flame images,two pre-processing methods on images are used here,which are resolution degradation and extracting properties of flame structure variables.The neural networks with fully connected layers are implemented to predict combustion oscillation with pre-processed data.It is found that both methods can obtain good prediction accuracies(better than90%).Besides,the network using degraded resolution as inputs might still behave well with an accuracy over90%at an extremely low resolution(3×3).A positive correlation of prediction accuracy and resolutions is found.In the terms of flame structure features,the transition of flame stability dynamics is captured under a limited range of parameter variations.The combustion oscillation prediction time is less than 2 ms using the proposed data-driven methods,which provide support for real-time prediction of combustion oscillation.
作者 周宇晨 张弛 韩啸 林宇震 ZHOU Yu-chen;ZHANG Chi;HAN Xiao;LIN Yu-zhen(National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beihang University,Beijing 100191,China;Collaborative Innovation Center for Advanced Aero-Engine,Beijing 100191,China)
出处 《推进技术》 EI CAS CSCD 北大核心 2021年第9期2038-2044,共7页 Journal of Propulsion Technology
基金 国家自然科学基金(91641109) 国家重大科技专项(2017-Ⅲ-0004-0028)。
关键词 燃气轮机 燃烧振荡 燃烧主动控制 神经网络 预报 Gas turbine engines Combustion oscillation Active combustion control Neural networks Instability prediction
  • 相关文献

参考文献3

二级参考文献61

  • 1郭志辉,王帅,李磊,张澄宇,孙晓峰.贫燃预混旋流火焰燃烧不稳定性的实验[J].航空动力学报,2009,24(12):2637-2642. 被引量:18
  • 2Cho J H, Lieuwen T C. Laminar premixed flame response to equivalence ratio oscillations [J]. Combustion and Flame, 2005, 140(1 -2) :116 - 129. 被引量:1
  • 3Lieuwen T. Physics of premixed combustion-acoustic wave interactions, combustion instabilities in gas turbine engines: operational experience, fundamental mechanisms, and modeling [ M ]. Reston : Progress in Astronautics and Aeronautics, AIAA,2005 : 315- 366. 被引量:1
  • 4Brewster B S, Cannon S M, Farmer J R, et al. Modeling of lean premixed combustion in stationary gas turbines[J]. Progress in Engergy and Combustion Science, 1999, 25(4): 353 -385. 被引量:1
  • 5Huang Y, Wang S, Yang, V. Flow and flame dynamics of lean premixed swirl injectors, combustion instabilities in gas turbine engines: operational experience, fundamental mechanisms, and modeling [ M ]. Reston: Progress in Astronautics and Aeronautics, AIAA , 2005:213 - 276. 被引量:1
  • 6Huang Y, Sung H G, Hsieh S Y, et al. Large eddy simulation of combustion dynamics of lean-premixed swirl-stabilized combustor[ J]. Journal of Propulsion and Power, 2003,19(5) :782 -794. 被引量:1
  • 7Huang Y, Yang V. Bifurcation of flame structure in a lean-premixed swirl-stabilized combustor: transition from stable to unstable flame [ J ]. Combustion and Flame, 2004,136(3) :383 -389. 被引量:1
  • 8Huang Y, Wang S, Yang V. Systematic analysis of leanpremixed swirl - stabilized combustion [J]. AIAA Journal,2006, 44(4): 724 -734. 被引量:1
  • 9Wang S W, Hsieh S Y, Yang V. Unsteady flow evolution in swirl injector with radial entry, part 1 : stationary conditions[ J]. Physics of Fluids, 2005, 17(4). 被引量:1
  • 10Wang S W, Yang V. Unsteady flow evolution in swirl injector with radial entry, part 2: external excitations[J]. Physics of Fluids, 2005, 17 (4). 被引量:1

共引文献31

同被引文献21

引证文献3

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部