• DocumentCode
    358387
  • Title

    Helicopter drive system diagnostics through multivariate statistical process control

  • Author

    Mimnagh, Michael L. ; Hardman, William ; Sheaffer, Jonathan

  • Author_Institution
    Dept. of Machinery Silencing, Naval Surface Warfare Center, Philadelphia, PA, USA
  • Volume
    6
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    381
  • Abstract
    The Naval Air Warfare Center has developed a Helicopter Integrated Diagnostic System (HIDS) which performs mechanical diagnostics on a helicopter´s drive system. Diagnostic indicators indicative of the mechanical health of the drive system components are derived from vibration data through a combination of statistical and signal processing methods. This paper discusses the application of a multivariate statistical process known as Hotelling´s T2 analyysis to HIDS diagnostic indicators. Multivariate analysis uses a composite function of multiple quality indicators to produce a single, trendable indicator that characterizes the state of the monitored process. A statistically valid method of creating and adjusting an alarm threshold for the resultant composite indicator is inherent in the method. When applied to mechanical diagnostic indicators from helicopter drive system seeded fault tests, the method produced timely and unambiguous fault identification with a reduced number of false alarms as compared to current diagnostic methods
  • Keywords
    aircraft testing; dynamic testing; fault diagnosis; helicopters; military aircraft; multivariable control systems; statistical process control; vibration measurement; HIDS diagnostic indicators; Helicopter Integrated Diagnostic System; Hotelling´s T2 analysis; Naval Air Warfare Center; alarm threshold; composite function; composite indicator; diagnostic indicators; false alarms; fault identification; helicopter drive; mechanical diagnostic indicators; mechanical diagnostics; mechanical health; multivariate statistical process; multivariate statistical process control; signal processing; vibration data; Aircraft propulsion; Control systems; Fault diagnosis; Helicopters; Intrusion detection; Machinery; Monitoring; Process control; Signal processing; Vibrations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.877914
  • Filename
    877914