• DocumentCode
    3584388
  • Title

    PROMIS - A generic PHM methodology applied to aircraft subsystems

  • Author

    Smeulers, J.P.M. ; Zeelen, R. ; Bos, A.

  • Author_Institution
    TPD, TNO, Delft, Netherlands
  • Volume
    6
  • fYear
    2002
  • fDate
    6/24/1905 12:00:00 AM
  • Firstpage
    457802
  • Abstract
    This paper describes the basic concepts of the PROMIS methodology for system´s Prognostic Health Management (PHM). The key elements of the PROMIS methodology are: (i) system health is monitored by continuously measuring so-called Condition Parameters (CPs), representing the physical condition of critical system components, (ii) CPs are derived using model-based estimation processes so that the existing set of sensors is exploited as much as possible, and (iii) the remaining lifetime of components is calculated using aging models and the expected system load.
  • Keywords
    ageing; aircraft testing; condition monitoring; PROMIS; aging model; aircraft subsystem; component lifetime; condition parameters; prognostic health management; system health monitoring; Aging; Aircraft; Condition monitoring; Costs; Filters; Life testing; Logistics; Prognostics and health management; Sensor systems; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1036156
  • Filename
    1036156