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基于全连接神经网络的分层旋流火焰燃烧振荡预报
周宇晨1,张弛1,2,韩啸1,林宇震1,2
1.北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室,北京 100191;2.先进航空发动机协同创新中心,北京 100191
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。
关键词:  燃气轮机  燃烧振荡  燃烧主动控制  神经网络  预报
DOI:10.13675/j.cnki.tjjs.200082
分类号:V231.2
基金项目:国家自然科学基金(91641109);国家重大科技专项(2017-Ⅲ-0004-0028)。
Prediction of Combustion Oscillation Based on Time-Averaged Images of Stratified Swirl Flame Using Fully-Connected Neural Network
ZHOU Yu-chen1, ZHANG Chi1,2, HAN Xiao1, LIN Yu-zhen1,2
1.National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering,Beihang University,Beijing 100191,China;2.Collaborative Innovation Center for Advanced Aero-Engine,Beijing 100191,China
Abstract:
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 than 90%). Besides, the network using degraded resolution as inputs might still behave well with an accuracy over 90% 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 2ms using the proposed data-driven methods, which provide support for real-time prediction of combustion oscillation.
Key words:  Gas turbine engines  Combustion oscillation  Active combustion control  Neural networks  Instability prediction