Main Article Content

Abstract

Aero gas turbine maintenance strategies are likely to see profound changes in the future. The remarkable size of the aftermarket for both military and civil aero gas turbines has already changed the nature of the business case. The aftermarket is large, more lucrative and not subject to the cyclical downturns of the original equipment sales. The competition which this considerably profitable after market creates will spur advances in diagnostic techniques. Of particular importance is advanced gas path diagnostics where, in recent years, engineering science research has opened pathways using somewhat surprising technologies. The paper will present work covering linear and non-linear gas path analysis, genetic algorithms, neural networks, fuzzy logic and hybrid systems. Much of the costs associated with the gas turbine after market relates to the gas path and these techniques are seen to play an important role

Keywords

No Keywords

Article Details

How to Cite
Singh, R. (2023). The Role of Gas Path Diagnostics in the Changing Gas Turbine After-market. Journal of Aerospace Sciences and Technologies, 57(1), 58–72. https://doi.org/10.61653/joast.v57i1.2005.680

References

  1. Singh, R., "Advances and Opportunities in Gas Path Diagnostics", Proceedings of the 2003 ISABE Conference, ISABE, 2003-1008, 2003.
  2. Marinai L., Probert D. and Singh R., "Prospects for Aero Gas-turbine Diagnostics: A Review", Applied Energy, Vol.79, No.1, pp. 109-126, 2004, September 2004.
  3. Dues, T., "Engine Life Management (ELM), USAF Perspective", Aero Engine Life Management In the 21st Century Conference, 2-3 March 2004, London, UK, ASME.
  4. Reckert, R., "Reliability Centered Maintenance (RCM) for Naval Aviation Propulsion and Power Systems", Aero Engine Life Management In the 21st Century Conference, 2-3 March 2004, London, UK, ASME.
  5. Howse, M., "Aero Gas Turbines - An Ever-Changing Engineering Challenge", Royal Aeronautical Society Whittle Lecture, 3 February 2004.
  6. Kanelopoulos, K., Stamatis, A. and Mathioudakis, K., "Incorporating Neural Networks into Gas Turbine Performance Diagnostics", International Gas Turbine and Aero-Engine Congress and Exhibition, Orlando, Florida, USA, ASME 97-GT-35, 1997.
  7. Provost, M.J., "The Use of Optimal Estimation Techniques in the Analysis of Gas Turbines", Ph.D. Thesis, School of Mechanical Engineering, Cranfield University, United Kingdom, 1995.
  8. Marinai, L., "Gas Path Diagnostics and Prognostics for Aero-engines using Fuzzy Logic and Time Series Analysis", Ph.D. Thesis, School of Engineering, Cranfield University, United Kingdom, 2004.
  9. Bechini, G., "Observability Study and Gas Path Diagnostics Using Fuzzy Logic as a Contribution to Make Informed Decisions on the Operation of Turbogas Systems", Tesi di Laurea, Facoltà di Ingegneria, Corso di Laurea in Ingegneria Meccanica, Universita’ di Pisa, Italy, 2004.
  10. Li, Y.G., 2002: Performance-analysis-based Gas Turbine Diagnostics: A Review. Proceedings of the Institution of Mechanical Engineers, Vol. 216, Part A, pp. 363-377.
  11. Singh, R., Zedda, M. and Gulati, A., "Advanced Diagnostic Techniques for Gas Turbines - An Overview", 5th International Conference on Stationary and Power Generating Gas Turbines Operation and Maintenance, London, United Kingdom. pp.26-28, October 1999.
  12. Doel, D., "Gas Path Analysis - Problems and Solutions", 17th Symposium of Aircraft Integrated Monitoring Systems, Bonn, Germany. pp.21-23 September , 1993.
  13. Doel, D., "TEMPER: Gas-path Analysis Tool for Commercial Jet Engines", Transactions of ASME, Journal of Engineering for Gas Turbines and Power, Vol.116, No.1, ASME 92-GT- 315, 1994.
  14. Consumi, M. and Agostino, L. D., "A Statistical Inference Approach to Gas Path Analysis of a Turbofan", AIAA Joint Propulsion Conference and Exhibit, Cleveland, Ohio, USA, 13-15 July 1998.
  15. Lunderstaedt, R.A., Fiedler, K. and Schmidt, K., "Some Experiments and Ideas on GPA Before Reaching Steady State of Engine", 16th AIAA Symposium on Aircraft Integrated Monitoring Systems, Germany, 1992.
  16. Lunderstaedt, R.A. and Junk, R.H., "Application of the Gas Path Analysis for the Nonstationary Operation of a Jet Engine", ISABE 97-7062, 1997.
  17. Stamatis, A., Mathioudakis, K., Berios, G. and Papailiou, K., "Jet Engine Fault Detection with Differential Gas Path Analysis at Discrete Operating Points. AIAA-1989-1244, 1989.
  18. Stamatis, A. and Papailiou, K.D., "Discrete Operating Conditions Gas Path Analysis", AGARD Conference Preprint No. 448, Quebec, Canada, 1988.
  19. Urban, L.A. and Volponi, A.J., "Mathematical Methods of Relative Engine Performance Diagnostics", SAE 922048, 1992.
  20. Urban, L.A., "Gas Path Analysis - A Tool for Engine Condition Monitoring", 33rd Annual International Air Safety Seminar, Christchurch, New Zealand, 1980.
  21. Urban, L.A., "Gas Path Analysis Applied to Turbine Engine Condition Monitoring", AIAA 72-1082, 1972.
  22. Urban, L.A., "Parameter Selection for Multiple Fault Diagnostics of Gas Turbine Engines", Journal of Engineering for Gas Turbines and Power, Transactions of the ASME, 74-GT-62, 1974.
  23. Volponi, A.J., "Gas Path Analysis - An Approach to Engine Diagnostics", 35th Symposium of Mechanical Failures Prevention Group, Gaithersburg, MD, USA, 1982.
  24. Alag, G. and Gilyard, G., "A Proposed Kalman Filter Algorithm for Estimation of Unmeasured Variables for an F100 Turbofan Engine", 26th Joint Propulsion Conference, Orlando, Florida, USA,16-18 July 1990, AIAA 90-1920.
  25. Kerr, L.J., Nemec, T.S. and Gallops, G.W., "Realtime Estimation of Gas Turbine Engine Damage using a Control Based Kalman Filter Algorithm", 36th International Gas Turbine and Aero-Engine Congress and Exposition, Orlando, FL, USA, 3-6 June 1991, ASME 91-GT-216.
  26. Provost, M.J., "COMPASS: A Generalized Ground Based Monitoring System", AGARD Conference Preprint No. 448, Quebec, Canada, 1988.
  27. Volponi, A.J., Depold, H.,Ganguli, R. and Daguang, C., "The use of Kalman Filter and Neural Network Methodologies in Gas Turbine Performance Diagnostics: A Comparative Study", ASME Turbo Expo 2000, Munich, Germany, 8-11 May 2000, ASME 2000-GT-547.
  28. Doel, D.L., "An Assessment of Weighted-least-squares-based Gas Path Analysis", Transactions of ASME, Journal of Engineering for Gas Turbines and Power, Vol. 116, No. 2. ASME 93-GT-119, 1994.
  29. DePold, H.R. and Gass, F.D., "The Application of Expert Systems and Neural Networks to Gas Turbine Prognostics and Diagnostics. ASME 98-GT-101, 1998.
  30. Dodd, N. and Martin, J., "Using Neural Networks to Optimize Gas Turbine Aero Engines", Computing and Control Engineering Journal, pp. 129-135, June 1997.
  31. Eustace, R., "Neural Network Fault Diagnosis of a Turbofan Engine", 11th ISABE Symposium, Tokyo, Japan, 19-24 September 1993, ISABE 93-7091.
  32. Eustace, R. and Merrington, G., "Fault Diagnosis of Fleet Engines Using Neural Networks", ISABE 957085, 1995.
  33. Illi, O.J. Jr., Greitzer, F.L., Kangas, L.J. and Reeve, T., "An Artificial Neural Network System for Diagnosing Gas Turbine Fuel Faults", Mechanical Failure Prevention Group Conference, Wakefield, USA, 1994.
  34. Junk, R. and Lunderstaedt, R., "Model Optimization of a Gas Turbine with Fault Affected Reference Measurements by Neural Networks for State and Sensor Diagnosis", AAIDA/AAAF/DGLR/RAeS 5th European Propulsion Forum, Pisa, Italy, 1995.
  35. Pong-Jeu Lu., Ming-Chuan Zang., Tzu-Cheng Hsu. and Jin Zhang., "An Evaluation of Engine Fault Diagnostics Using Artificial Neural Networks", ASME Turbo Expo 2000, Munich, Germany, 8-11 May 2000, ASME 2000-GT-0029.
  36. Romessis, C., Stamatis, A. and Mathioudakis, K., "A Parametric Investigation of the Diagnostic Ability of the Probabilistic Neural Networks on Turbofan Engines", ASME Turbo Expo 2001, New Orleans, USA, 4-7 June 2001, ASME 2001-GT-0011.
  37. Torella, G. and Lombardo, G., "Utilization of Neural Networks for Gas Turbine Engines", 12th ISABE Symposium, 1995.
  38. Zedda, M. and Singh, R., "Fault Diagnosis of a Turbofan Engine using Neural Networks: A Quantitative Approach", 34th AIAA /SAE/ASME/ASEE Joint Propulsion Conference and Exhibit, Cleveland, Ohio, USA, 13-15 July 1998, AIAA 98-3062,
  39. Ganguli, R., "Application of Fuzzy Logic for Fault Isolation of Jet Engines", ASME Turbo Expo 2001, New Orleans, USA, 4-7 June 2001, ASME 2001-GT-0013.
  40. Ganguli, R., "Data Rectification and Detection of Trend Shifts in Jet Engine Gas Path Measurements Using Median Filters and Fuzzy Logic", ASME Turbo Expo 2001, New Orleans, USA, 4-7 June 2001, ASME 2001-GT-0014.
  41. Marinai, L., Singh, R. and Curnock, B., "Fuzzylogic-based Diagnostic Process for Turbofan Engines", 16th ISABE Conference, Cleveland, Ohio, USA, 31 August-5 September 2003.
  42. Doel, D., "The Role for Expert Systems in Commercial Gas Turbine Engine Monitoring", ASME 90GT-374, 1990.
  43. Green, A. and Allen, D., "Artificial Intelligence for Real Time Diagnostics and Prognostics of Gas Turbine Engines", 33rd AIAA/SME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, USA, 1997.
  44. Torella, G., "Probabilistic Expert Systems for Diagnostics and Trouble Shooting of Gas Turbine Apparatuses", 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, USA, 2024 June 1999.
  45. Zedda, M. and Singh, R., "Gas Turbine Engine and Sensor Fault Diagnosis Using Optimization Techniques. 35th AIAA/ASME/SAE/ASSE Joint Propulsion Conference and Exhibit, Los Angeles, CA, USA, 1999.
  46. Zedda, M. and Singh R., "Gas Turbine Engine and Sensor Diagnostics", 14th ISABE Symposium, Florence, Italy, 1999.
  47. Gulati, A., Zedda, M. and Singh, R., "Gas Turbine Engine and Sensor Multiple Operating Point Analysis Using Optimization Techniques", 36th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference, Huntsville, USA, AIAA-2000-3716, 2000.
  48. Gulati, A.,Taylor, D. and Singh, R., "Multiple Operating Point Analysis Using Genetic Algorithm Optimization for Gas Turbine Diagnostics", 15th ISOABE Symposium, Bangalore, India, 3-7 September 2001, ISABE-2001-1139.
  49. Sampath, S., Gulati, A. and Singh, R., "Fault Diagnostics Using Genetic Algorithm for Advanced Cycle Gas Turbine", ASME Turbo Expo 2002, Amsterdam, The Netherlands,
  50. Sampath, S. and Singh, R., "Performance Assessment and Fault Diagnostics for Advanced Cycle Marine Gas Turbine", 6th INEC, Glasgow, United Kingdom, 23-25 April 2002.
  51. Mathioudakis, K. and Sieverding, C.H (edited by)., "Gas Turbine Condition Monitoring and Fault Diagnosis", Lecture Series 2003-01, Von Karman Institute for Fluid Dynamics, Belgium, 2003.
  52. Escher, P.C. and Singh, R., "An Object-oriented Diagnostics Computer Program Suitable for Industrial Gas Turbines", 21st (CIMAC) International Congress of Combustion Engines, Switzerland, 15-18 May 1995.
  53. Ogaji, S.O.T. and Singh, R., "Gas Path Fault Diagnosis Framework for a Three-shaft Gas Turbine", Proceedings of the Institution of Mechanical Engineers, Vol.217, Part A, pp.149-157, 2003.
  54. Michalewicz, Z., "Genetic Algorithms + Data Structures = Evolution Programs", Springer Verlag, 3rd Edition, 1996.
  55. Merrington, G.L., "Identification of Dynamic Characteristics for Fault Isolation Purposes in a Gas Turbine Using Closed-Loop Measurements. Engine Condition Monitoring Technology and Experience, October 1988. AGARD-CP-448.
  56. Li, Y.G., "A Gas Turbine Diagnostic Approach with Transient Measurements", Proceedings of the Institution of Mechanical Engineers, Vol. 217, Part A, pp. 169-177, 2003.
  57. Marinai, L., Singh, R., Curnock, B. and Probert D., "Detection and Prediction of the Performance Deterioration of a Turbofan Engine", TS-005, International Gas Turbine Congress 2003, Tokyo, November 2-7 2003.
  58. Singh, R., "Civil Aero Gas Turbines: Strategy and Technology", Chairman’s Address, Aerospace Division, Institution of Mechanical Engineers, London, April 2001.
  59. Campbell, D., "Propulsion for the 21st Century NASA Glenn Research Centre Perspective", Royal Aeronautical Fedden Lecture, Cranfield University, UK, November 2002.
  60. Whellens, M.W. and Singh, R., "Propulsion System Optimisation for Minimum Global Warming Potential, 23rd ICAS Congress, Toronto, Canada, September 2002.

Similar Articles

<< < 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 > >> 

You may also start an advanced similarity search for this article.