• DocumentCode
    2682587
  • Title

    An integrated reliability evaluation model of aircraft flight test

  • Author

    Zhang, Wenjin ; Lan, Nan ; Sun, Ping

  • Author_Institution
    Sch. of Reliability Eng., Beihang Univ., Beijing, China
  • fYear
    2011
  • fDate
    12-15 June 2011
  • Firstpage
    208
  • Lastpage
    211
  • Abstract
    In aircraft flight test phase, in order to verify whether the aircraft has reached the reliability requirements, we need to assess its reliability. Firstly, in this paper we review the reliability estimation method under multi-profiles that can be used to evaluate the reliability of aircraft during the flight test process and analyze its shortcoming. Then, in order to expand the amount of data, we describe how to incorporate the environment conversion factors into the reliability estimation method under multi-profiles. By the way, taking into account the varied population-environment feature of data, an integrated evaluation model of flight test of reliability was established. This model is making up the weak points of previous models, and improving the accuracy of reliability evaluation. Finally, this method applied in a real engineering example is described.
  • Keywords
    aircraft testing; environmental factors; estimation theory; reliability theory; aircraft flight test; environment conversion factors; integrated reliability evaluation model; reliability estimation method; Accuracy; Aircraft; Aircraft manufacture; Atmospheric modeling; Data models; Reliability engineering; aircraft flight; environment conversion factors; integrated evaluation; multiple profiles; reliability estimation; the varied population-environment data;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability, Maintainability and Safety (ICRMS), 2011 9th International Conference on
  • Conference_Location
    Guiyang
  • Print_ISBN
    978-1-61284-667-5
  • Type

    conf

  • DOI
    10.1109/ICRMS.2011.5979264
  • Filename
    5979264