• DocumentCode
    3516491
  • Title

    Leakage Fault Detection Method for Axial-Piston Variable Displacement Pumps

  • Author

    Palazzolo, Jerome J. ; Scheunemann, Larry D. ; Hartin, John R.

  • Author_Institution
    Sentient Corp., Williston, VT
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    To address the lack of health monitoring for gas turbine engine accessory components, Sentient developed a promising fault estimation algorithm for axial-piston variable displacement pumps. The key to this success was the development of a physics-based nonlinear model of the system that includes three common types of fluid leakage faults. The modeling effort and simulation results provided the thorough knowledge needed to extract features from the system responses to detect the occurrence of faults. The nominal pump and the pump with a single piston replaced by three different machined pistons were tested to emulate varying stages of piston wear. The experiments demonstrated that the model was able to capture the dynamic behavior of the actual system. By considering several time and frequency domain metrics, a fault estimation method was developed that correctly identified the presence and severity of leakage faults, while using a fraction of the memory and computational resources of other model-based methods.
  • Keywords
    aerospace engines; aerospace instrumentation; condition monitoring; fault diagnosis; gas turbines; pistons; pumps; wear; axial-piston variable displacement pumps; fault estimation algorithm; fluid leakage faults; gas turbine engine; health monitoring; leakage fault detection method; physics-based nonlinear model; piston wear; Engines; Fault detection; Feature extraction; Frequency domain analysis; Frequency estimation; Monitoring; Pistons; Pumps; Testing; Turbines;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526609
  • Filename
    4526609