• DocumentCode
    1558397
  • Title

    Life cycle testing of a sealed 24-V, 42-Ah nickel-cadmium aircraft battery

  • Author

    Kulin, Timothy M.

  • Author_Institution
    Eagle-Picher Ind. Inc., Joplin, MO, USA
  • Volume
    12
  • Issue
    10
  • fYear
    1997
  • fDate
    10/1/1997 12:00:00 AM
  • Firstpage
    17
  • Lastpage
    22
  • Abstract
    Extensive research has been conducted in the design and manufacture of very long life sealed maintenance free nickel-cadmium aircraft batteries. This study presents data on a 100% depth of discharge (DOD) life test performed on a nominal capacity 42-Ah battery. The purpose of this study is to validate design concepts, determine the life characteristics of the newly designed sealed Ni-Cd batteries, and develop baseline information on failure rates and mechanisms. The data from this experiment can be used to compare depth of discharge versus battery life with similar tests such as the lower DOD experiments performed on spacecraft batteries. This information is important in the ongoing development of long life batteries and in developing failure models for life prediction
  • Keywords
    aircraft; failure analysis; life testing; reliability; secondary cells; 24 V; Ni-Cd; aircraft battery; baseline information; battery life; depth of discharge; design concepts validation; failure mechanisms; failure models; failure rates; life cycle testing; life prediction; long life batteries; maintenance free battery; sealed battery; Aircraft manufacture; Batteries; Electrodes; Life testing; Performance evaluation; Space vehicles; System testing; Temperature; Thermal resistance; US Department of Defense;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.624323
  • Filename
    624323