• DocumentCode
    2912120
  • Title

    Method for detection and confirmation of multiple failure modes with numerous survivor data

  • Author

    Powell, Mark A.

  • Author_Institution
    Attwater Consulting, Webster, TX, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    13
  • Abstract
    Modern aerospace systems are often subject to multiple modes of failure. Unless the failure modes have radically different statistical characteristics, it can be very difficult to recognize in failure data that multiple failure modes are in play. When using graphical inferential methods for reliability analysis, the potential for multiple failure modes may be suggested by a bent regression line. Subsequent analysis of these modes is usually performed by segregating the data to separate sets to be processed separately for each failure mode, usually segregated about the bend in the regression line. This data segregation process raises a number of questions, especially when numerous survivor data are to be processed. The primary issue with a survivor datum in this case is that it reflects that the system has not yet failed, in any mode. Assigning a survivor datum to any particular failure mode data set for separate processing appears completely arbitrary, and may produce spurious results that may then result in unnecessary costs or unacceptable risks in preventative maintenance.
  • Keywords
    aerospace industry; data analysis; failure analysis; preventive maintenance; reliability; statistical analysis; bent regression line; data segregation process; graphical inferential methods; modern aerospace systems; multiple failure modes; numerous survivor data; preventative maintenance; reliability analysis; statistical characteristics; AC generators; Data models; Equations; Joints; Mathematical model; Numerical models; Reliability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747588
  • Filename
    5747588