• DocumentCode
    2404945
  • Title

    Modelling imperfect inspection and maintenance in defence aviation through bayesian analysis of the KIJIMA type I general renewal process (GRP)

  • Author

    Jacopino, Andrew ; Groen, Frank ; Mosleh, Ali

  • Author_Institution
    Dept. of Defence, Defence Materiel Organ., Canberra, ACT
  • fYear
    2006
  • fDate
    23-26 Jan. 2006
  • Firstpage
    470
  • Lastpage
    475
  • Abstract
    To ensure the effective and efficient operation of Defence aviation equipment there is a clear need for a component life model that is representative of the true life of a component. However, the large and often sophisticated RAM models used to manage defence aviation platforms, through various engineering and logistics activities, use models that cannot accurately represent this life. The main difference is in the underlying repair assumption. Specifically, the Ordinary Renewal Process (ORP) uses an as-good-as-new repair assumption while the Non-Homogenous Poisson Process (NHPP) uses an as-bad-as-old repair assumption. However, it is highly unlikely that any component, typically referred to as a Repairable Item (RI), will readily fit into either repair assumption. Therefore, despite the best endeavours of both engineering and logistics staff given the underlying repair assumption and the limitation these impose on the model, any solution will be suboptimal. Accordingly, there is a need for a RI life model that can contend with imperfect maintenance, imperfect inspection and can adapt to the limitations in data and include a number of additional factors including aging of the component, number of repairs, effectiveness of the repair, skill of the technicians, etc. Eight cases were developed as part of the overall modelling scheme. These eight cases are further divided into 2 main types; the first type representing cases where failure times are known and the second type where failure times are unknown. The cases incrementally modify these types through the addition of factors including multiple failure modes and their inter-dependence, and imperfect inspection and maintenance, in order to achieve a more realistic representation. Each of these cases were then solved using utilising a Markov Chain Monte Carlo (MCMC) sampling procedure, concentrating only on the analysis of the KIJIMA Type I GRP model with an underlying Weibull Time-To- Failure (TTF) distribution. The M- - CMC was made possible through the use of a Slice Sampling and Auxiliary Variable techniques. The resulting models have the ability to accurately model, and specifically predict, the future failure trends. Furthermore, the model allows the analyst to compare the maintenance effectiveness either in isolation, or in comparison (benchmarking) of various maintenance activities/facilities
  • Keywords
    Markov processes; Monte Carlo methods; Weibull distribution; belief networks; benchmark testing; failure analysis; inspection; logistics; maintenance engineering; military avionics; Bayesian analysis; GRP; KIJIMA Type I general renewal process; Markov Chain Monte Carlo sampling; NHPP; ORP; RAM model; Weibull time-to-failure distribution; auxiliary variable techniques; benchmarking; component life model; defence aviation equipment; engineering staff; failure modes; imperfect inspection; imperfect maintenance; logistics staff; nonhomogenous poisson process; ordinary renewal process; repairable item; slice sampling; Aging; Aircraft propulsion; Australia; Bayesian methods; Cost function; Engineering management; Inspection; Logistics; Predictive models; Sampling methods;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 2006. RAMS '06. Annual
  • Conference_Location
    Newport Beach, CA
  • ISSN
    0149-144X
  • Print_ISBN
    1-4244-0007-4
  • Electronic_ISBN
    0149-144X
  • Type

    conf

  • DOI
    10.1109/RAMS.2006.1677418
  • Filename
    1677418