Skip to main content
Log in

SR-30 turbojet engine real-time sensor health monitoring using neural networks, and Bayesian belief networks

  • Published:
Applied Intelligence Aims and scope Submit manuscript

Abstract

This paper describes the use of artificial intelligence-based techniques for detecting and isolating sensor failures in a turbojet engine. Specifically, three artificial intelligence (AI) techniques are employed: artificial neural networks (NNs), statistical expectations, and Bayesian belief networks (BBNs). These techniques are combined into an overall system that is capable of distinguishing between sensor failure and engine failure—a critical capability in the operation of turbojet engines.

The turbojet engine used in this study is an SR-30 developed by Turbine Technologies. Initially, NNs were designed and trained to recognize sensor failure in the engine. The increased random noise output from failing sensors was used as the key indicator. Next, a Bayesian statistical method was used to recognize sensor failure based on the bias error occurring in the sensors. Finally, a BBN was developed to interpret the results of the NN and statistical evaluations. The BBN determines whether single or multiple sensor failures signify engine failure, or whether sensor failures represent separate, unrelated incidences. The BBN algorithm is also used to distinguish between bias and noise errors on sensors used to monitor turbojet performance. The overall system is demonstrated to work equally well during start-up and main-stage operation of the engine. Results show that the method can efficiently detect and isolate single or multiple sensor failures within this dynamic environment.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Similar content being viewed by others

References

  1. Simon DL (2000) An overview of the NASA aviation safety program propulsion health monitoring element. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 36th, Huntsville, AL AIAA paper: 2000-3624

  2. Garg S (2004) Controls and health management technologies for intelligent aerospace propulsion systems. 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA paper: 2004-949

  3. Tumer IY, Anupa Bajwa (1999) A survey of aircraft engine health monitoring systems. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 35th, Los Angeles, CA, AIAA paper: 1999-2528

  4. Menke TE, Maybeck PS (1995) Sensor/actuator failure detection in the VISTA F-16 by multiple model adaptive estimation. IEEE Transactions on Aerospace and Electronic Systems, 31(4):1218–1229

    Article  Google Scholar 

  5. Hsu PL, Lin KL, Shen LC (1995) Diagnosis of multiple sensor and actuator failures in automotive engines. IEEE Transactions on Vehicular Technology, 44(4)

  6. Rago C, Raman RP, Mehra K, Fortenbaugh R (1998) Failure detection and identification and fault tolerant control using the IMM-KF with applications to the eagle-eye UAV. Proceedings of the 37th IEEE Conference on Decision & Control Tampa, Florida

  7. Deckert JC, Desai NN, Deyst JJ, Willsky AS (1977) F-8 DFBW sensor failure identification using analytical redundancy. IEEE Transactions on Automatic Control, AC-22:795–803

    Article  Google Scholar 

  8. Patton RJ, Chen J (1992) Robust fault detection of jet engine sensor systems using eigenstructure assignment. Journal of Guidance, Control, and Dynamics 15:1491–1497

    Article  Google Scholar 

  9. Cikanek HA (1986) Space shuttle main engine failure detection. IEEE Control Systems Magazine

  10. Guo TH, Musgrave J (1995) Neural network based sensor validation for reusable rocket engines paper-WP13. Proceeedings of the American Control Conference, Seattle, Washington

  11. Mattern DL, Jaw LC, Guo TH, Graham R, McCoy W (1998) Using neural networks for sensor validation. NASA-TM-1998-208483 and also AIAA paper: 98-3547, 34th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, 12–15

  12. Kobayashi T, Simon DL (2003) Application for bank of Kalman filters for aircraft engine fault diagnosis. NASA-TM-2003-212526

  13. DeLatt JC, Merrill WC (1990) A real time microcomputer implementation of sensor failure detection for Turbofan engines. IEEE Control Systems Magazine, pp 29–37

  14. Frank PM (1990) Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy—a survey and some new results. Automatica 26:459–474

    Article  MATH  Google Scholar 

  15. Litt JS, Simon DL, Garg S, Guo TH, Mercer C, Millar R, Behbahani A, Bajwa A, Jensen DT (2005) A survey of intelligent control and health management technologies for aircraft propulsion systems. NASA/TM—2005-213622

  16. Li YG (2002) Performance analysis based gas turbine diagnostics: a review. http://hdl.handle.net/1826/1008

  17. Sterritt M, Shapcott M (2000) Exploring dynamic Bayesian belief networks for intelligent fault management systems. IEEE, International Conference on Systems, Man and Cybernetics 5:3646–3652

  18. Liu E, Zhang D (2002) Diagnosis of component failures in the space shuttle main engines using Bayesian belief networks: a feasibility study. 14th IEEE International Conference on Tools with Artificial Intelligence (ICTAI’02), pp 181

  19. Mast TA, Reed AT, Yurkovich S, Ashby M, Adibhatla S (1999) Bayesian belief networks for fault identification in aircraft gas turbine engines. Proceedings of the IEEE International Conference on Control Applications, Kohala Coast-Island of Hawai’i, Hawai’i, USA pp 22–27

  20. Paris D, Trevino L, Watson M (2005) A framework for integration of IVHM technologies for intelligent integration for vehicle management. IEEE Aerospace Conference, Big Sky, Montana

  21. Williamson J (2005) Bayesian nets and causality: philosophical and computational foundations. Oxford University Press, Oxford

    MATH  Google Scholar 

  22. Merrill WC, Delaat JC, Bruton W (1988) Advanced detection, isolation, and accommodation of sensor failures: real-time evaluation. AIAA J. of Guidance, Control and Dynamics, 11 (6)

  23. Watanabe A, Davis R, Ölçmen MS, Polites M, Trevino L (2004) Soft computing technology experiments on a turbine technologies SR-30 engine. AIAA paper: 2004-1303, 42nd Aerospace Sciences and Exhibit Conference, Reno, NV, 5–8

  24. Watanabe A, Ölçmen MS, Leland R, Whitaker KW, Trevino LC (2004) Soft computing applications on SR-30 turbojet engine. 1st AIAA Intelligent Systems, Technical Conference, Chicago, IN, September 20–22, paper AIAA-2004-6444

  25. Punska O (1999) Bayesian approaches to multi sensor data fusion. Master of Philosopy Dissertation, Cambridge University, Signal Processing and Communications Laboratory Department, Cambridge, UK

  26. Wasserman PD (1989) Neural computing- theory and practice. Van Nostrand and Reinhold book company, New York, pg 18

  27. Bishop CM (1995) Neural networks for pattern recognition. Oxford, Oxford University Press pg 77

  28. Meyer C, Maul W (1991) Application of neural networks to the SSME startup transient. NASA Contractor Report 187138

  29. Murphy KP (2001) The bayes nets toolbox for MATLAB. Computing Science and Statistics. 33

  30. Yedidia JS, Freeman WT, Weiss Y (2002) Understanding belief propagation and its generalizations. Mitsubishi Electric Research Laboratories, Technical Report, TR-2001-22. http://www.merl.com/papers/docs/TR2001-22.pdf

  31. http://www.cs.berkeley.edu/∼jordan/courses/281A-fall04/lectures/lec-11-16.pdf

  32. Ghahramani Z, Beal MJ (2001) Propagation algorithms of variational Bayesian learning. Neural Information Processing Systems 13, eds. T.K. MIT Press

  33. Figueroa F, Mahajan A (1994) Generic model of autonomous sensor. Mechatronics 4(3): 295–315

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Nott, C., Ölçmen, S.M., Karr, C.L. et al. SR-30 turbojet engine real-time sensor health monitoring using neural networks, and Bayesian belief networks. Appl Intell 26, 251–265 (2007). https://doi.org/10.1007/s10489-006-0017-z

Download citation

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10489-006-0017-z

Keywords

Navigation