Machine Learning and IoT Trends for Intelligent Prediction of Aircraft Wing Anti-Icing System Temperature

被引:18
作者
Abdelghany, E. S. [1 ,2 ]
Farghaly, Mohamed B. [3 ]
Almalki, Mishari Metab [4 ]
Sarhan, H. H. [5 ]
Essa, Mohamed El-Sayed M. [6 ]
机构
[1] Al Baha Univ, Fac Engn, Mech Power Dept, POB 1988, Al Baha, Saudi Arabia
[2] Egyptian Aviat Acad, Inst Aviat Engn & Technol IAET, Aeronaut Engn Dept, Giza 12815, Egypt
[3] Fayoum Univ, Fac Engn, Mech Engn Dept, Al Fayyum 63514, Egypt
[4] Al Baha Univ, Fac Engn, Dept Elect Engn, POB 1988, Al Baha 65431, Saudi Arabia
[5] Port Said Univ, Fac Engn, Mech Engn Dept, Port Said 42526, Egypt
[6] Egyptian Aviat Acad, Inst Aviat Engn & Technol IAET, Elect Power & Machines Dept, Giza 12815, Egypt
关键词
wing anti-icing system; aerodynamics; piccolo tube; IoT; artificial neural network; CFD; conjugate heat transfer; HEAT-TRANSFER; SIMULATION; FLOW;
D O I
10.3390/aerospace10080676
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Airplane manufacturers are frequently faced with formidable challenges to improving both aircraft performance and customer safety. Ice accumulation on the wings of aircraft is one of the challenges, which could result in major accidents and a reduction in aerodynamic performance. Anti-icing systems, which use the hot bleed airflow from the engine compressor, are considered one of the most significant solutions utilized in aircraft applications to prevent ice accumulation. In the current study, a novel approach based on machine learning (ML) and the Internet of Things (IoT) is proposed to predict the thermal performance characteristics of a partial span wing anti-icing system constructed using the NACA 23014 airfoil section. To verify the proposed strategy, the obtained results are compared with those obtained using computational ANSYS 2019 software. An artificial neural network (ANN) is used to build a forecasting model of wing temperature based on experimental data and computational fluid dynamics (CFD) data. In addition, the ThingSpeak platform is applied in this article to realize the concept of the IoT, collect the measured data, and publish the data in a private channel. Different performance metrics, namely, mean square error (MSE), maximum relative error (MAE), and absolute variance (R2), are used to evaluate the prediction model. Based on the performance indices, the results prove the efficiency of the proposed approach based on ANN and the IoT in designing a forecasting model to predict the wing temperature compared to the numerical CFD method, which consumes a lot of time and requires high-speed simulation devices. Therefore, it is suggested that the ANN-IoT approach be applied in aviation.
引用
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页数:34
相关论文
共 52 条
[1]   High bypass turbofan engine and anti-icing system performance: Mass flow rate of anti-icing bleed air system effect [J].
Abdelghany, E. S. ;
Sarhan, H. H. ;
El Saleh, A. ;
Farghaly, Mohamed B. .
CASE STUDIES IN THERMAL ENGINEERING, 2023, 45
[2]  
Abdelghany E.S., 2016, P 17 INT C APPL MECH, VVolume 17, P1
[3]  
Abdelghany E.S., 2016, P 54 AIAA AEROSPACE, V1, DOI [10.2514/6.2016-1367, DOI 10.2514/6.2016-1367]
[4]   Study the Effect of Winglet Height Length on the Aerodynamic Performance of Horizontal Axis Wind Turbines Using Computational Investigation [J].
Abdelghany, Eslam S. ;
Sarhan, Hesham H. ;
Alahmadi, Raed ;
Farghaly, Mohamed B. .
ENERGIES, 2023, 16 (13)
[5]  
Asaumi N., 2018, J GAS TURBINE SOC JP, V46, P476
[6]  
Avi A., 2020, Master Thesis
[7]  
Broeren A.P., 2013, 5 AIAA ATM SPAC ENV, DOI 10.2514/6.2013-2824
[8]   Heat transfer correlation for anti-icing systems [J].
Brown, JM ;
Raghunathan, S ;
Watterson, JK ;
Linton, AJ ;
Riordon, D .
JOURNAL OF AIRCRAFT, 2002, 39 (01) :65-70
[9]   Aircraft ice accretion prediction using neural network and wavelet packet transform [J].
Chang, Shinan ;
Leng, Mengyao ;
Wu, Hongwei ;
Thompson, James .
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2016, 88 (01) :128-136
[10]   Investigation of fluid flow and heat transfer characteristics for a thermal anti-icing system of a high-altitude and long-endurance UAV [J].
Cheng, Jen-Chieh ;
Chen, You-Ming .
JOURNAL OF MECHANICS, 2021, 37 :467-483