• DocumentCode
    1769902
  • Title

    Highly Accelerated Life Testing for avionics devices

  • Author

    Catelani, Marcantonio ; Ciani, Lorenzo

  • Author_Institution
    Dept. of Inf. Eng., Univ. of Florence, Florence, Italy
  • fYear
    2014
  • fDate
    29-30 May 2014
  • Firstpage
    418
  • Lastpage
    422
  • Abstract
    In avionics application one of the most important competition factors is the reliability, given that the failure occurrence may leads to a critical state for the functioning of the aircraft. Some avionics apparatus are intolerant of failures, as lives may depend on the reliable functioning of equipment. Highly Accelerated Life Testing (HALT) is a time compression testing protocol that utilizes a step stress approach in subjecting products to varied thermal and vibration stresses. It is used to uncover design limitations and weaknesses in the preliminary design phase, helping designers to find and fix errors before they occur during the application in the field. The goal of HALT testing is to break the product by subjecting the test unit to progressively higher stress levels, incorporating thermal dwells, rapid temperature transitions, varied vibration stresses, and a combination of temperature and vibration to precipitate inherent defects. In this paper the HALT process related to an avionic equipment is described and a specific test plant is discussed.
  • Keywords
    aircraft testing; avionics; failure analysis; life testing; reliability; thermal stresses; vibrations; HALT testing; avionic equipment; avionics devices; failure occurrence; highly accelerated life testing; reliability; step stress approach; temperature transitions; test plant; thermal dwells; thermal stresses; time compression testing protocol; vibration stresses; Aerospace electronics; Life estimation; Reliability engineering; Stress; Testing; Vibrations; HALT; Highly Accelerated Life Testing; avionics; reliability;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Metrology for Aerospace (MetroAeroSpace), 2014 IEEE
  • Conference_Location
    Benevento
  • Type

    conf

  • DOI
    10.1109/MetroAeroSpace.2014.6865961
  • Filename
    6865961