• DocumentCode
    1344494
  • Title

    Starting & Limiting Values for Reliability Growth

  • Author

    Finkelstein, Jack M.

  • Author_Institution
    Hughes Aircraft Co.; POBox 3310; Fullerton, CA 92634 USA.
  • Issue
    2
  • fYear
    1979
  • fDate
    6/1/1979 12:00:00 AM
  • Firstpage
    111
  • Lastpage
    114
  • Abstract
    Modifications of the Duane model for reliability growth which permit formulating test plans prior to test-data availability are presented herein. The modified model yields finite and nonzero MTBFs at the start and end of development testing. The unmodified Duane model is inadequate for formulating the Development Test plan for a Reliability Program because the MTBF is zero at the start of testing and is unbounded for long tests. The parameters of the modified model; limiting MTBF, initial MTBF, and Duane shape parameter (logarithmic growth rate) are estimatable from handbooks and previous experience prior to the start of development tests. An implicit expression for the Duane-model scale-parameter as a function of the limiting MTBF, initial MTBF, and shape parameter is given. The time required and/or the reliability improvement potential of development tests are obtained from the model to plan the reliability program. When the development tests are underway interval estimates for the modified Duane model parameters, needed to monitor the progress of the reliability program, can be computed.
  • Keywords
    Aircraft; Availability; Condition monitoring; Lifting equipment; Mathematical model; Predictive models; Reliability theory; Shape; Statistical analysis; System testing; Duane model (modification); Reliability growth plan; Test and fix plan;
  • fLanguage
    English
  • Journal_Title
    Reliability, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9529
  • Type

    jour

  • DOI
    10.1109/TR.1979.5220512
  • Filename
    5220512