International Journal of Reliability, Risk and Safety: Theory and Application

International Journal of Reliability, Risk and Safety: Theory and Application

Health Monitoring Algorithm for Turbofan Engine Using Cascade Feedforward Neural Networks

Document Type : Original Research Article

Authors
Aerospace Faculty, Malek-Ashtar University of Technology, Tehran, Iran
Abstract
Today, health monitoring systems for turbine engines have become a vital requirement in the aviation industry. In this paper, different fault detection methods of turbine engines are reviewed based on previous research to reveal the importance of the problem and existing challenges. The existing methods use the engine signals for diagnostics, which are heavily affected by operating conditions and disturbances. The faults effect on the performance charts of the F100-PW-220 engine is detected by neural network technique to alleviate the signal variation problem. Some common faults in this type of engine are modeled, including compressor fouling, turbine blade corrosion, and fuel injection problems. The proposed method is effective in a wide range of engine working conditions such as first moments of take-off with afterburner, take-off at 0.1 M, subsonic cruise flight at 0.8 M without afterburner in 10000, 20000, and 40000 feet altitude, supersonic cruise flight at 1.6 M with afterburner in the same altitudes. The cascade neural network with probabilistic transfer functions is used in this paper and shows satisfactory fault detection, while the required training dataset is much less than the previous works. This method facilitates the fast implementation of the system due to the small training dataset and improves the diagnostics accuracy over operational time.
Keywords
Subjects

  1. Demirci, C. Hajiyev and A. Schwenke, "Fuzzy logic‐based automated engine health monitoring for commercial aircraft," Aircraft engineering and aerospace technology, vol. 80, no. 5, pp. 516-525, 2008. doi: https://doi.org/10.1177/1748006X21989661.
  2. Nadjafi and P. Gholami, "Bayesian inference of reliability growth-oriented Weibull distribution for multiple mechanical stages systems," International Journal of Reliability, Risk and Safety: Theory and Application, vol. 3, no. 1, pp. 77-84, 2020. doi: https://doi.org/10.30699/IJRRS.3.1.9.
  3. Culley et al., “More intelligent gas turbine engines,” North Atlantic Treaty Organization, France, Rep. AC/323(AVT-128)TP/255, 2009.
  4. K. Yedavalli and R. K. Belapurkar, "Application of wireless sensor networks to aircraft control and health management systems," Control Theory and Applications, vol. 9, pp. 28-33, 2011. doi: https://doi.org/10.1007/s11768-011-0242-9.
  5. M. Bidgoli, M. A. S. Ashtiani and M. Mahmoudi, "Intelligent performance monitoring of aircraft engine using fuzzy logic," in 13th International Conference of Iranian Aerospace Society, Tehran, Iran, 2014. (in Persian)
  6. A. Urban, "Parameter selection for multiple fault diagnostics of gas turbine engines," Journal of Engine Power, vol. 10, no. 7, pp. 225-230, 1975, doi: https://doi.org/10.1115/1.3445969.
  7. Fuster, A. Ligeza and A. Martin, "Abductive diagnostic procedure based on an and/or/not graphs for expected behaviour: Application to gas turbine," in 10th International Congress and Exhibition on Condition Monitoring and Diagnostic Engineering Management, Espoo, Finland, 1997, pp. 511-520.
  8. A. Urban, Gas turbine engine parameter interrelationships, 2nd ed. Pennsylvania: Hamilton Standard Division of United Aircraft Corporation, 1969.
  9. Stamatis, K. Mathioudakis, M. Smith and K. Papailiou, "Gas turbine component fault identification by means of adaptive performance modeling," American Society of Mechanical Engineers, vol. 79085, pp. 90-GT-376, 1990. https://doi.org/10.1115/90-GT-376.
  10. E. Dietz, E. I. Kiech and M. Ali, "Jet and rocket engine fault diagnosis in real time," Journal of Neural Network Computation, vol. 1, no. 1, pp. 5-18, 1989.
  11. G. Li, "A gas turbine diagnostic approach with transient measurements," Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, vol. 217, no. 2, pp. 169-177, 2003, doi: https://doi.org/10.1243/09576500360611317.
  12. Verma, N. Roy and R. Ganguli, "Gas turbine diagnostics using a soft computing approach," Applied mathematics and computation, vol. 172, no. 2, pp. 1342-1363, 2006, doi: https://doi.org/10.1016/j.amc.2005.02.057.
  13. S. Wang, W. M. Wang, Y. Q. Shi and Y. Zhang, "Gas turbine condition monitoring and prognosis: A review," Advanced Engineering Forum, vol. 2, pp. 694-699, 2011. doi: https://doi.org/10.4028/ www.scientific.net/AEF.2-3.694.
  14. Ebrahimi and K. Mollazade, "Intelligent fault classification of a tractor starter motor using vibration monitoring and adaptive neuro-fuzzy inference system," Insight-non-destructive Testing and Condition Monitoring, vol. 52, no. 10, pp. 561-566, 2010, doi: https://doi.org/10.1784/insi.2010.52.10.561.
  15. A. Farsi, "Identification of size and location of bearing damage via deep learning," International Journal of Reliability, Risk, and Safety: Theory and Application, vol. 4, no. 1, pp. 69-74, 2021, doi: https://doi.org/10.30699/IJRRS.4.1.9.
  16. Abdul-aziz, M. R. Woike, J. D. Lekki and G. Y. Baaklini, "Health monitoring of a rotating disk using a combined analytical-experimental approach," National Aeronautics and Space Administration, Ohio, USA, Rep. 2009-215675, 2009.
  17. Mohammadi, E. Naderi, K. Khorasani and S. Hashtrudi-Zad, "Fault diagnosis of gas turbine engines by using dynamic neural networks," in IEEE International Conference on Quality and Reliability (ICQR), 2010, pp. 365-376, doi: https://doi.org/ 10.1115/GT2010-23586.
  18. Pinelli, P. R. Spina and M. Venturini, "Gas turbine health state determination: Methodology approach and field application," International Journal of Rotating Machinery, vol. 2012, no. 1, p. 2012, Art. no. 142173, doi: https://doi.org/ 10.1155/2012/142173.
  19. Puggina and M. Venturini, "Development of a statistical methodology for gas turbine prognostics," Journal of Engine Gas Turbine Power, vol. 134, no. 2, 2012, Art. no. 022401, doi: https://doi.org/10.1115/1.4004185.
  20. Tahan, E. Tsoutsanis, M. Muhammad and Z. A. Karim, "Performance-based health monitoring, diagnostics and prognostics for condition-based maintenance of gas turbines: A review," Applied Energy, vol. 198, pp. 122-44, 2017, doi: https://doi.org/10.1016/j.apenergy.2017.04.048.
  21. Adamowicz and G. Żywica, "Advanced gas turbines health monitoring systems," Diagnostyka, vol. 19, no. 2, pp. 77-87, 2018, doi: http://dx.doi.org/10.29354/diag/89730.
  22. Jianzhong, L. Chaoyi, L. Cui, G. Ziwei and W. Rong, "A data-driven health indicator extraction method for aircraft air conditioning system health monitoring," Chinese Journal of Aeronautics, vol. 32, no. 2, pp. 409-416, 2019, doi: https://doi.org/10.1016/j.cja.2018.03.024.
  23. Balakrishnan, A. I. Devasigamani, K. R. Anupama and N. Sharma, "Aero-engine health monitoring with real flight data using whale optimization algorithm based artificial neural network technique," Optical Memory and Neural Networks, vol. 30, pp. 80-96, 2021, doi: https://doi.org/10.3103/S1060992X21010094.
  24. Szrama, "Turbofan engine health status prediction with neural network pattern recognition and automated feature engineering," Aircraft Engineering and Aerospace Technology, vol. 96, no. 11, pp. 19-26, 2024, doi: https://doi.org/10.1108/AEAT-04-2024-0111.
  25. Aditya, T. Nikolaidis, A. C. Manuel and S. Togni, "Implementation of Artificial Intelligence for Aircraft Engine Health Monitoring and Prognostics," in ASME Turbo Expo 2024: Turbomachinery Technical Conference and ExpositionVolume 4: Controls, Diagnostics, and Instrumentation, London, United Kingdom, 2024, doi: https://doi.org/10.1115/ GT2024-127081.
  26. Thakkar and H. Chaoui, "Prognostic and health management of an aircraft turbofan engine using machine learning," in IEEE Vehicle Power and Propulsion Conference, Milan, Italy, 2023, doi: https://doi.org/10.1109/VPPC60535.2023.10403231.
  27. Kurz and K. Brun, "Fouling mechanisms in axial compressors," Journal of Engineering for Gas Turbines and Power, vol. 134, 2012, Art. no. 032401, doi: https://doi.org/10.1115/1.4004403.
  28. D. Fentaye and K. G. Kyprianidis, "An intelligent data filtering and fault detection method for gas turbine engines," in MATEC Web Conference, Vol. 314, 2020, Paper 02007, doi: https://doi.org/10.1051/matecconf/202031402007.
  29. Balan and W. Tabakoff, "A method of predicting the performance deterioration of a compressor-cascade due to sand erosion," in 21st Aerospace Sciences Meeting, Nevada, USA, 1983, doi: https://doi.org/10.2514/6.1983-178.
  30. A. Hamed, W. Tabakoff and R. Wenglarz, "Erosion, deposition, and their effect on performance," in Turbine Aerodynamics, Heat Transfer, Materials, and Mechanics, T. I-P. Shih and V. Yang, Ed. Place of publication: American Institute of Aeronautics and Astronautics (AIAA), 2014, pp. 585-611, doi: https://doi.org/10.2514/5.9781624102660.0585.0612.
  31. Kurz and K. Brun, "Degradation in gas turbine systems," Journal of Engine Gas Turbine Power, vol. 123, no. 1, pp. 70-77, 2001, doi: https://doi.org/10.1115/1.1340629.
  32. S. Sowers, G. Kopasakis and D. L. Simon, "Application of the systematic sensor selection strategy for turbofan engine diagnostics," in Turbo Expo: Power for Land, Sea, and Air, 2008. https://doi.org/10.1115/GT2008-50525.
  33. D. Fentaye and K. G. Kyprianidis, "An intelligent data filtering and fault detection method for gas turbine engines," in MATEC Web Conference, Vol. 314, 2020, Paper 02007, doi: https://doi.org/10.1051/matecconf/202031402007.
  34. B. Meher-Homji and R. Bhargarva, "Condition monitoring and diagnostic aspects of gas turbine transient response," International Journal of Turbo and Jet Engines, vol. 11, no. 1, pp. 99-111, 1994, doi: https://doi.org/10.1515/TJJ.1994.11.1.99.
  35. Kobayashi and D. L. Simon, "A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics," Journal of Propulsion and Power, vol. 21, no. 4, pp. 751-758, 2005, doi: https://doi.org/10.2514/1.9881.
  36. Algarni, M. Tozan and A. Jamal, "Failure forecasting of aircraft air conditioning/cooling pack with field data," Journal of Aircraft, vol. 44, no. 3, pp. 996-1002, 2012, doi: https://doi.org/10.2514/1.26561.
  37. Hare, S. Gupta, N. Najjar, P. D'Orlando and R. Walthall, "System-level fault diagnosis with application to the environmental control system of an aircraft," in SAE 2015 AeroTech Congress and Exhibition, 2015, Paper 2015-01-2583, doi: https://doi.org/10.4271/2015-01-2583.
  38. Silva, N. Najjar, S. Gupta and P. D'Orlando, "Wavelet-based fouling diagnosis of the heat exchanger in the aircraft environmental control system," in SAE 2015 AeroTech Congress and Exhibition, 2015, Paper 2015-01-2582, 2015, doi: https://doi.org/10.4271/2015-01-2582.
  39. Najjar, J. Hare, P. D'Orlando, G. Leaper, K. Pattipati, A. Silva, S. Gupta and R. Walthall, "Heat exchanger fouling diagnosis for an aircraft air-conditioning system," in SAE 2013 AeroTech Congress and Exhibition, 2013, Paper 2013-01-2250, doi: https://doi.org/10.4271/2013-01-2250.
  40. Ma, C. Lu and H. Liu, "Fault diagnosis for the heat exchanger of the aircraft environmental control system based on the strong tracking filter," PloS One, vol. 10, no. 3, 2015, Art. no. e0122829, doi: https://doi.org/10.1371/journal.pone.0122829.
Volume 7, Issue 2
October 2024
Pages 52-61

  • Receive Date 06 September 2024
  • Revise Date 03 November 2024
  • Accept Date 05 November 2024