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
Link To Document