DocumentCode :
358596
Title :
Extending the fatigue life of SGA interconnects for aerospace applications
Author :
Larson, Michael C. ; Verges, Melody A.
Author_Institution :
Dept. of Mech. Eng., Tulane Univ., New Orleans, LA, USA
Volume :
5
fYear :
2000
fDate :
2000
Firstpage :
319
Abstract :
The effect of residual stresses on the fatigue life of a solder grid array (SGA) interconnect is modeled using fracture mechanics. A fatigue crack growth model is proposed for an interconnect subject to cyclic shear loading in conjunction with either a constant crack-opening or a constant crack-closing stress. The residual stresses stem from the constant mean curvature shape of the interconnect and depend upon the volume of solder and the distance between the printed circuit board and chip carrier. Experiments are reported which support the residual force approximations. The fracture model can be used to predict how the relative fatigue life of a solder interconnect can be extended
Keywords :
avionics; ball grid arrays; fatigue cracks; fracture mechanics; interconnections; internal stresses; reflow soldering; PCB to chip carrier distance; aerospace applications; constant crack-closing stress; constant crack-opening stress; constant mean curvature shape; cyclic shear loading; fatigue crack growth model; fatigue life; forces on liquid bridge; fracture mechanics modelling; residual force approximations; residual stresses effect; solder grid array interconnects; Aerospace engineering; Delay effects; Fatigue; Geometry; Integrated circuit interconnections; Mechanical engineering; Packaging; Printed circuits; Residual stresses; Temperature;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.878504
Filename :
878504
Link To Document :
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