• DocumentCode
    1851412
  • Title

    Performing the AVIP durability analysis using the finite element method

  • Author

    Trembinski, Ted ; Reganato, Frank

  • Author_Institution
    AIL Syst. Inc., Deer Park, NY, USA
  • fYear
    1993
  • fDate
    24-28 May 1993
  • Firstpage
    738
  • Abstract
    Improving avionics hardware reliability through the use of durability analysis is a primary objective of the U.S. Air Force Aeronautical Systems Division´s Avionics Integrity Program (AVIP). Embedding this process into an integrated product development (IPD) approach provides a design solution tailored to the equipment´s operational environment. This enables improved hardware reliability and availability at reduced life cycle cost due to the reduction or elimination of unscheduled maintenance events. Identifying and correcting potential deficiencies and optimizing the equipment design to the usage environment and defining manufacturing processes in the development phase of the program are the ultimate objectives of IPD and AVIP
  • Keywords
    aircraft instrumentation; finite element analysis; printed circuit testing; reliability; stress analysis; surface mount technology; AVIP; AVIP durability analysis; Avionics Integrity Program; IPD; SMT PCB; U.S. Air Force; availability; avionics; finite element method; hardware reliability; integrated product development; maintenance; reduced life cycle cost; working stress criterion; Aerospace electronics; Availability; Costs; Design optimization; Finite element methods; Hardware; Maintenance; Manufacturing processes; Performance analysis; Product development;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1993. NAECON 1993., Proceedings of the IEEE 1993 National
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-1295-3
  • Type

    conf

  • DOI
    10.1109/NAECON.1993.290848
  • Filename
    290848