Multimodal Hybrid Aero-Engine Mechanical Wear Fault Diagnosis Algorithm Based on Two-Channel Data Input Types

IF 2.7 3区 工程技术 Q1 ENGINEERING, MULTIDISCIPLINARY
Qifan Zhou, Yingqing Guo, Guicai Li, Kejie Xu, Kun Wang
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引用次数: 0

Abstract

Aero-engines are complex and sophisticated systems combining mechanical, thermal, and fluidic domains. Abnormal wear of mechanical components is becoming more prevalent due to severe changes in flight conditions and the external environment, which may lead to drastic performance degradation and accidents. Therefore, the diagnosis of such wear and tear faults is urgent, and based on this need, more researchers and scholars are focusing their attention on it. To address the current shortcomings of fault diagnosis algorithms that only rely on one-dimensional datasets or two-dimensional image analysis and the low accuracy of final fault identification, an innovative hybrid algorithm is proposed in this study. The algorithm integrates one-dimensional time series data and two-dimensional image data, converts the one-dimensional dataset into a two-dimensional image dataset through the Gramian Angle Field technique, and subsequently uses a dual-channel GRU-CNN (Convolutional Neural Network-Gated Recurrent Unit) algorithm model designed for fault diagnosis, which can simultaneously analyze and map the features and fault modes of the one-dimensional dataset and the two-dimensional image. In order to extract features with richer semantic information and stronger discriminative ability, a multimodal fusion technique is employed, which successfully addresses the limitations of the wear-and-tear feature distributions of the two datasets using the cross-extraction fusion method and combines the advantages of both in terms of trend distributions of the time series and edge feature distributions of the image sequences, respectively. The best fault diagnosis results were achieved by using the strong mapping relationship between the saliency feature expression and the fault modes. The final analysis shows that the recognition rate of typical mechanical wear of aero-engines exceeds 97%, thus achieving the desired goal.

基于双通道数据输入类型的多模态混合航空发动机机械磨损故障诊断算法
航空发动机是复杂而精密的系统,结合了机械,热和流体领域。由于飞行条件和外部环境的剧烈变化,机械部件的异常磨损越来越普遍,可能导致剧烈的性能下降和事故。因此,对此类磨损故障的诊断迫在眉睫,基于这一需求,越来越多的研究人员和学者开始关注这一问题。针对目前故障诊断算法仅依赖一维数据集或二维图像分析以及最终故障识别准确率低的缺点,本研究提出了一种创新的混合算法。该算法将一维时间序列数据与二维图像数据整合,通过Gramian角场技术将一维数据集转换为二维图像数据集,随后采用专为故障诊断设计的双通道GRU-CNN(卷积神经网络-门控循环单元)算法模型,可以同时分析和映射一维数据集和二维图像的特征和故障模式。为了提取语义信息更丰富、判别能力更强的特征,采用多模态融合技术,成功解决了交叉提取融合方法对两种数据集磨损特征分布的局限性,结合了两者在时间序列趋势分布和图像序列边缘特征分布方面的优势。利用显著性特征表达式与故障模式之间的强映射关系,获得了最佳的故障诊断结果。最终分析表明,航空发动机典型机械磨损识别率超过97%,达到预期目标。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
5.70
自引率
6.90%
发文量
276
审稿时长
5.3 months
期刊介绍: The International Journal for Numerical Methods in Engineering publishes original papers describing significant, novel developments in numerical methods that are applicable to engineering problems. The Journal is known for welcoming contributions in a wide range of areas in computational engineering, including computational issues in model reduction, uncertainty quantification, verification and validation, inverse analysis and stochastic methods, optimisation, element technology, solution techniques and parallel computing, damage and fracture, mechanics at micro and nano-scales, low-speed fluid dynamics, fluid-structure interaction, electromagnetics, coupled diffusion phenomena, and error estimation and mesh generation. It is emphasized that this is by no means an exhaustive list, and particularly papers on multi-scale, multi-physics or multi-disciplinary problems, and on new, emerging topics are welcome.
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