Title :
High performance heat sink for surface mount applications
Author :
McKeown, S.A. ; LeVasseur, Robert D.
Author_Institution :
General Electric Aerospace, Binghamton, NY, USA
Abstract :
Surface-mounted electronic module configurations are sensitive to thermal cycling because the reduced compliance between the component and module increases the thermally induced strain in the solder joint. Providing a thermal match between the component and the module reduces this strain, reduces low-cycle fatigue damage, and increases solder joint life. One way of achieving this thermal match is through the use of a thermally matched heat sink. In addition to having the required coefficient of thermal expansion (CTE), heat sinks for surface-mount avionic configurations require low weight and high thermal conductivity. A heat sink has been developed that has thermal conductivity close to aluminum, a CTE close to ceramic, and a weight density only 8% higher than aluminum. The flexural modulus of this heat sink is 40% higher than aluminum, which results in improved vibration performance. It is laminated, consisting of a thicker layer of graphite between thinner layers of copper-clad molybdenum,.<>
Keywords :
heat sinks; modules; surface mount technology; thermal conductivity of solids; thermal expansion; Mo-Cu-C; SMT; coefficient of thermal expansion; copper-clad molybdenum; electronic module configurations; graphite; high-performance heat sink; surface mount applications; surface-mounted electronic module configurations; thermal conductivity; thermal cycling; thermally matched heat sink; Aerospace electronics; Aluminum; Ceramics; Conducting materials; Electronics packaging; Heat sinks; Lead; Surface-mount technology; Thermal conductivity; Thermal expansion;
Conference_Titel :
Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
Conference_Location :
Los Angeles, CA, USA
DOI :
10.1109/DASC.1991.177158