Neural network models for usage based remaining life computation

Journal of Engineering for Gas Turbines and Power

Volumn 130, Issue 1, 2008, Pages

  Parthasarathy, Girija ^a   Menon, Sunil ^a   Richardson, Kurt ^a   Jameel, Ahsan ^a   McNamee, Dawn ^a   Desper, Tori ^a   Gorelik, Michael ^a   Hickenbottom, Chris ^a  

^a HONEYWELL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; COMPUTER SIMULATION; GAS TURBINES; NEURAL NETWORKS; STRESS ANALYSIS; THERMAL EFFECTS;

DYNAMIC NEURAL NETWORK MODEL; LIFE PREDICTION;

MACHINE COMPONENTS;

COMPRESSORS; COMPUTER SIMULATION; GAS TURBINES; MACHINE COMPONENTS; NEURAL NETWORKS; STRESS ANALYSIS; THERMAL EFFECTS;

EID: 42149148434     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2771248     Document Type: Article

References (17)

1. Larsen, J. M., Russ, S. M., Rosenburger, A. H., John, R., Fecke, T., and Rasmussen, B., 2002, "Achieving the Potential of Material Prognosis for Turbine Engines," DARPA Bidders Conference on Materials Prognosis, Washington, DC.
2. Fujimoto, W. T., 2002, "A Critical Assessment of Fatigue Prediction Methodologies for Rotorcraft Members," Sixth Joint FAA/DoD/NASA Conference on Aging Aircraft, San Francisco, CA.
3. Forth, S. C., Everett, R. A., and Newman, J. A., 2002, "A Novel Approach to Rotorcraft Damage Tolerance," Sixth Joint FAA/DoD/NASA Conference on Aging Aircraft, San Francisco, CA.
4. Kwon, Y. S., Fawaz, S. A., and Ingram, J. E., 2002, "3D Finite Element Modeling of MSD-Cracked Structural Joints," Sixth Joint FAA /DoD/NASA Conference on Aging Aircraft, San Francisco, CA.
5. Cope, D. A., Lacy, T. E., and Luzar, J. J., 2002, "Application of Advanced Fracture Mechanics Methods for KC-135 Fuselage Structural Integrity Evaluation," Sixth Joint FAA/DoD/NASA Conference on Aging Aircraft, San Francisco, CA.
6. Parthasarathy, G., and Allumallu, S., 2004, "Reduced Models for Rotating Component Lifing," Proceedings of ASME Turbo Expo 2004, Vienna, Austria, Jun. 14-17, 2004.
7. Cardona, A., and Idelsohn, S., 1986, "Solution of Non-linear Thermal Transient Problems by a Reduction Method," Int. J. Numer. Methods Eng., 23, pp. 1023-1042.
8. Guyan, R. J., 1965, "Reduction of Stiffness and Mass Matrices," AIAA J., 3(2), p. 380.
9. Busbard, L. B., 1981, "On the Value of Guyan Reduction in Dynamic Thermal Problems," Comput. Struct., 13, pp. 525-531.
10. Botto, D., Zucca, S., Gola, M. M., and Salvano, S., 2002, "A Method for On-line Temperature Calculation of Aircraft Engine Turbine Discs," Proceedings of ASME Turbo Expo 2002, Amsterdam, The Netherlands.
11. Haykin, S., 1999, Neural Networks: A Comprehensive Foundation, 2nd ed., Prentice-Hall, Englewood Cliffs, NJ.
12. Norgaard, M., Ravn, O., Poulsen, N. K., and Hansen, L. K., 2000, Neural Networks for Modeling and Control of Dynamic Systems, Springer-Verlag, London.
13. Norgaard, M., 2000, "Neural Network Based System Identification Toolbox, Version 2," Technical University of Denmark.
14. Ogunnaike, B. A., and Ray, W. H., 1994, Process Dynamics, Modeling, and Control, Oxford University Press, New York.
15. Korb, R., Skorjanz, P, and Jorgl, H. P., 1997, "Black Box Modeling of an Industrial Combustion Plant," SYSID'97, 11th IFAC Symposium on System Identification, Kitakyushu, Japan.
16. Bittani, S., and Lovera, M., 1997, "Identification of Linear Models for a Hovering Helicopter Rotor," 11th IFAC Symposium on System Identification, Kitakyushu, Japan.
17. L., Ljung, 1987, System Identification: Theory for the User, P.T.R. Prentice Hall, Englewood Cliffs, NJ.