• DocumentCode
    3584266
  • Title

    Pathan - A new approach to gas turbine diagnostics

  • Author

    Peacock, Koy E.

  • Author_Institution
    Thermodyne-Amos Ltd., UK
  • Volume
    6
  • fYear
    2002
  • fDate
    6/24/1905 12:00:00 AM
  • Firstpage
    6
  • Abstract
    The health of the various gas turbine components leaves a signature in the gas path so complete gas path analysis yields an understanding of engine state. Since instrumentation cannot be fitted in engine hot regions there are available two non-complimentary sets of information: manufacturer-supplied new engine performance; incomplete gas path data for the degraded engine. Pathan synthesises these, producing an analysis describing actual performance of the engine and its components while instrument scatter, outage and calibration drift are automatically eliminated. This is a position paper. Examples are given of results gained from in industrial engine although an aeronautical example using jet thrust has been successful. High accuracy, which holds tip well with reducing instrument streams, results so while Pathan is improved with an increased installed instrumentation, it retains accuracy with a deficient instrument package. It therefore opens up a range of operational options for new installations and retrofit.
  • Keywords
    condition monitoring; gas turbines; Pathan; aeronautical engine; gas path state analysis; gas turbine diagnostics; health monitoring system; industrial engine; instrumentation; jet thrust; statistical analysis; Aerospace industry; Calibration; Degradation; Engines; Instruments; Manufacturing industries; Packaging; Performance analysis; Scattering; Turbines;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1036140
  • Filename
    1036140