Non-linear engine component fault diagnosis from a limited number of measurements using a combinatorial approach

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 2 A, Issue , 2002, Pages 109-118

  Aretakis, N ^a   Mathioudakis, K ^a   Stamatis, A ^a  

^a NATIONAL TECHNICAL UNIVERSITY OF ATHENS   (Greece)

Author keywords

[No Author keywords available]

Indexed keywords

FAULT DIAGNOSIS; NONLINEAR GAS PATH ANALYSIS;

COMPRESSORS; JET ENGINES; PRESSURE; TEMPERATURE; VECTORS;

TURBOFAN ENGINES;

EID: 0037002925     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30031     Document Type: Conference Paper

References (17)

1. Urban L.A., Volponi A.J., 1992, "Mathematical methods of relative engine performance diagnostics", SAE 1992 transactions, 101, journal of aerospace, technical paper 922048.
2. Barwell M. J., 1987, "Compass-Ground Based Engine Monitoring Program for General Applications", SAE technical paper 871734.
3. Provost M.J., 1988, "Compass: A generalized ground based monitoring system", paper 42, AGARD-CP-448, Engine Condition Monitoring, Technology and Experience.
4. Doel D., 1994, "TEMPER-a gas path analysis tool for commercial jet engines", ASME Journal of Engineering for Gas Turbines and Power, Jan 1994, 116, pp 82-89, also ASME paper, 92-GT-315.
5. Doel D., 1994, "An assessment of weighted-least-squares based gas path analysis", ASME Journal of Engineering for Gas Turbines and Power, April 1994, 116, pp 366-373, also ASME paper 93-GT-119.
6. Volponi A., "Sensor Error Compensation in Engine Performance Diagnostics", ASME paper 94-GT-58.
7. Stamatis A., Mathioudakis K., Berios G., Papailiou K.,1991, "Jet Engine Fault Detection with Discrete Operating Points Gas Path Analysis", Journal of Propulsion, 7, No 6, Dec 1991, pp 1043-1048.
8. Kobayashi T., Simon D., 2001, "A hybrid neural-genetic algorithm technique for aircraft engine performance diagnostics", 37th AIAA/ASME /SAE/ASEE Joint Propulsion Conference and Exhibit, 8-11 July 2001, Salt Lake City, Utah, paper AIAA-2001-3763.
9. Groenstredt T.V., 2001. "A multi point gas path analysis tool for gas turbine engines with a moderate level of instrumentation", XV ISABE, Bangalore, India, Sept. 3-7, 2001, paper ISABE-2001-1139.
10. Gulati A., Taylor D., Sign R., 2001, "Multiple operating point analysis using genetic algorithm optimization for gas turbine diagnostic", XV ISABE, Bangalore, India, Sept. 3-7, 2001, paper ISABE-2001-1139.
11. Stamatis A., Mathioudakis K., Papailiou K.D., 1990, "Adaptive simulation of gas turbine performance", Journal of engineering for gas turbines and power, April 1990 112, pg. 168-175.
12. Urban, 1975, "Parameter Selection for multiple fault diagnostics of gas turbine engines", AGARD CP-165, Diagnostic and Engine Condition Monitoring, June 1975, paper 19.
13. Tsalavoutas A., Mathioudakis K., Stamatis A., Smith M., 2000, "Identifying faults in the variable geometry system of a gas turbine compressor", ASME paper, 2000-GT-33.
14. Mathioudakis K., Stamatis A., Tsalavoutas A. and Aretakis N., "Performance analysis of industrial gas turbines for engine condition monitoring", Proceedings Of The Institution of Mechanical Engineers, Part A, Journal of Power and Energy, 215 No A2, March 2001, pp 173-184.
15. Stamatis A., Mathioudakis K., Ruiz J., Curnock B., 2001, "Real time engine model implementation for adaptive control & performance monitoring of large civil turbofans", ASME paper, 2001-GT-362.
16. Kamboukos Ph., Oikonomou P., Stamatis A., Mathioudakis K., "Optimizing Diagnostic Effectiveness Of Mixed Turbofans By Means Of Adaptive Modelling And Choice Of Appropriate Monitoring Parameters", AVT Symposium on "Monitoring and Management of Gas Turbine Fleets for Extended Life and Reduced Costs", Manchester, UK, 8-11 October 2000.
17. Curnock B. 2000, "Obidicote Project- Work Package 4. Steady-state test cases". Rolls-Royce Report DNS62433.