• DocumentCode
    2440075
  • Title

    Hybrid Change Detection for Aircraft Engine Fault Diagnostics

  • Author

    Hu, Xiao ; Eklund, Neil ; Goebel, Kai ; Cheetham, William

  • Author_Institution
    General Electr., Schenectady
  • fYear
    2007
  • fDate
    3-10 March 2007
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    Change detection is an important task for remote monitoring, fault diagnostics and system prognostics. When a fault occurs, it will often times cause changes in measurable quantities of the system. Early detection of changes in system measurements that indicate abnormal conditions helps the diagnostics of the fault so that appropriate maintenance action can be taken before the fault progresses, causes secondary damage to the system and the equipment experiences downtime. In this paper, we investigate the performance of a suite of change detection algorithms. A set of synthetic time series data with different change patterns are generated based on the empirical distribution of real engine performance data so that the individual change detection algorithm can be evaluated and compared against each other. At last, the results from the individual change detection algorithms are fused together to demonstrate that the ensemble of the change detection algorithms generates better performance than any individual detection algorithm.
  • Keywords
    aerospace engines; fault diagnosis; time series; aircraft engine fault diagnostics; fault diagnostics; hybrid change detection; remote monitoring; system prognostics; Aircraft propulsion; Change detection algorithms; Computational intelligence; Costs; Detection algorithms; Equipment failure; Fault detection; Power generation economics; Sequential analysis; Signal processing algorithms;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2007 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    1-4244-0524-6
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2007.352848
  • Filename
    4161643