Turbofan engine health status prediction with neural network pattern recognition and automated feature engineering

被引:1
|
作者
Szrama, Slawomir [1 ]
机构
[1] Poznan Univ Tech, Aviat Div, Poznan, Poland
来源
关键词
Aircraft turbofan engine; Health status prediction; Neural network pattern recognition; Artificial neural network; Prognostic health monitoring; Turbine engine failure analysis; FAULT-DETECTION; DIAGNOSIS; MACHINE;
D O I
10.1108/AEAT-04-2024-0111
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
PurposeThis study aims to present the concept of aircraft turbofan engine health status prediction with artificial neural network (ANN) pattern recognition but augmented with automated features engineering (AFE).Design/methodology/approachThe main concept of engine health status prediction was based on three case studies and a validation process. The first two were performed on the engine health status parameters, namely, performance margin and specific fuel consumption margin. The third one was generated and created for the engine performance and safety data, specifically created for the final test. The final validation of the neural network pattern recognition was the validation of the proposed neural network architecture in comparison to the machine learning classification algorithms. All studies were conducted for ANN, which was a two-layer feedforward network architecture with pattern recognition. All case studies and tests were performed for both simple pattern recognition network and network augmented with automated feature engineering (AFE).FindingsThe greatest achievement of this elaboration is the presentation of how on the basis of the real-life engine operational data, the entire process of engine status prediction might be conducted with the application of the neural network pattern recognition process augmented with AFE.Practical implicationsThis research could be implemented into the engine maintenance strategy and planning. Engine health status prediction based on ANN augmented with AFE is an extremely strong tool in aircraft accident and incident prevention.Originality/valueAlthough turbofan engine health status prediction with ANN is not a novel approach, what is absolutely worth emphasizing is the fact that contrary to other publications this research was based on genuine, real engine performance operational data as well as AFE methodology, which makes the entire research very reliable. This is also the reason the prediction results reflect the effect of the real engine wear and deterioration process.
引用
收藏
页码:19 / 26
页数:8
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