DocumentCode :
1643966
Title :
Advanced cooling techniques comparison for airborne electronic circuits
Author :
Assouad, Yannick ; Caplot, Michel ; Gautier, Thierry
Author_Institution :
Thomson-CSF Radars & Contre-Mesures, Elancourt, France
fYear :
1997
Firstpage :
131
Lastpage :
141
Abstract :
A comparison of the performances of four different cooling techniques of modular avionics modules (233×150 mm) has been conducted. The cooling methods which have been investigated are conduction through a metallic (aluminum) core embedded in the module and Air Flow Through (AFT) module on one part, using theoretical evaluations, Liquid Flow Through (LFT) module and heat pipe using test results on the other part. The comparison yields the following conclusions. Conduction and AFT modules are limited to a maximum power dissipation in the range of 50 W. Heat pipes allow power dissipations in the range of 150 to 200 W but depending on the technology, their performances can be greatly decreased by gravity, vibrations and acceleration effects; moreover, the market for flat heat pipes of the kind necessary for modular avionics modules is not strong enough yet to support a substantial industrial production. LFT is the best cooling technique since it can allow power dissipations of more than 600 W, which covers more than foreseen needs for modular avionics modules
Keywords :
avionics; cooling; heat pipes; modules; 50 to 600 W; Air Flow Through module; Liquid Flow Through module; airborne electronic circuit; cooling; heat pipe; metallic core conduction; modular avionics module; power dissipation; Acceleration; Aerospace electronics; Aluminum; Consumer electronics; Electronics cooling; Fluid flow; Gravity; Power dissipation; Production; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Semiconductor Thermal Measurement and Management Symposium, 1997. SEMI-THERM XIII., Thirteenth Annual IEEE
Conference_Location :
Austin, TX
ISSN :
1065-2221
Print_ISBN :
0-7803-3793-X
Type :
conf
DOI :
10.1109/STHERM.1997.566790
Filename :
566790
Link To Document :
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