A GM (1, 1) Markov Chain-Based Aeroengine Performance Degradation Forecast Approach Using Exhaust Gas Temperature

Article English OPEN
Ning-bo Zhao; Jia-long Yang; Shu-ying Li; Yue-wu Sun;

Performance degradation forecast technology for quantitatively assessing degradation states of aeroengine using exhaust gas temperature is an important technology in the aeroengine health management. In this paper, a GM (1, 1) Markov chain-based approach is introduced t... View more
  • References (37)
    37 references, page 1 of 4

    Bytington, C. S., Roemer, M. J., Galie, T.. Prognostic enhancements to diagnostic systems for improved condition-based maintenance. ; 6: 2815-2824

    Marinai, L., Probert, D., Singh, R.. Prospects for aero gas-turbine diagnostics: a review. Applied Energy. 2004; 79 (1): 109-126

    Litt, J. S., Simon, D. L., Garg, S.. A survey of intelligent control and health management technologies for aircraft propulsion systems. 2005 (NASA-TM-2005-213622)

    Melcher, K. J., Maul, W. A., Garg, S.. Propulsion health management system development for affordable and reliable operation of space exploration systems. AIAA. 2007 (2007-6237)

    Li, Y. G.. Gas turbine performance and health status estimation using adaptive gas path analysis. Journal of Engineering for Gas Turbines and Power. 2010; 132 (4)-9

    Chen, G.. Forecasting engine performance trend by using structure self-adaptive neural network. Acta Aeronautica et Astronautica Sinica. 2007; 28 (3): 535-539

    Jiang, L. P.. Gas path fault diagnosis system of aero-engine based on grey relationship degree. Procedia Engineering. 2011; 15: 4774-4779

    Wu, X. H., Wen, D., Li, R. G., Chen, Z. Z., Huang, H. Z., Lv, Z. Q.. A model to predict the residual life of aero-engine based upon Support Vector Machine. : 1880-1882

    Ren, S. H., Zuo, H. F.. A combined prediction method for the residual-life of civil aviation engines based on performance degradation. Mechanical Science and Technology For Aerospace Engineering. 2011; 30 (1): 23-29

    Fu, X. Y., Zhong, S. S., Zhang, M. N.. An improved method for aeroengine residual life prediction. Journal of Harbin Institute of Technology. 2013; 45 (5): 51-55

  • Metrics
Share - Bookmark