• DocumentCode
    280732
  • Title

    Packaging requirements [avionics]

  • Author

    Hunt, K.J.R.

  • Author_Institution
    Electromag. Eng. Group, BAe plc, Filton, UK
  • fYear
    1990
  • fDate
    33009
  • Firstpage
    42522
  • Lastpage
    613
  • Abstract
    The proposed modular avionics packaging scheme includes a range of digital, bus structured modules together with interface and power supply modules. The rack assembly is likely to be a complete Faraday cage structure providing the first line environmental protection against electromagnetic hazard (EMH), moisture and fluids but only offering minimal protection against the basic mechanical environment. Conducted EMH protection would be incorporated within the rack which should, ideally, allow for backplane removal through the front cover aperture. Input, output and power supply connectors should only be positioned at the ends of the rack such that the front cover can provide the maximum protection for the `active´ modules. Each module within the avionics fit is likely to incorporate one or more card assemblies manufactured with surface mount technology (SMT) components on both sides of a centrally mounted connector and heatsink rib
  • Keywords
    aircraft instrumentation; electromagnetic compatibility; modules; packaging; protection; Faraday cage structure; SMT; aircraft; bus structured modules; cooling; electromagnetic hazard; environmental protection; modular avionics packaging; power supply modules; protection; rack; reliability; surface mount technology;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Future Military Avionic Architectures, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    191131