DocumentCode :
2969167
Title :
Comparative compliance of representative lead designs for surface mounted components
Author :
Kotlowitz, Robert W.
Author_Institution :
AT&T Bell Lab., Whippany, NJ, USA
fYear :
1989
fDate :
22-24 May 1989
Firstpage :
791
Lastpage :
831
Abstract :
Equations for the directional spring constants for common compliant lead designs for surface-mounted (SM) components are given. The lead configurations include the straight J-lead, dimpled J-lead, gull-wing lead, butt-lead (I-lead), and S-bend lead. The updated lead geometries and analysis method represent an expanded treatment of previous lead compliance studies by the author. The present objectives are to demonstrate applications of the analytic tool developed and identify the directional stiffness parameters that should be considered when assessing the compliance of a specific lead design. Comparative lead compliance evaluation has been performed for different SM components tested using accelerated function cycling or circuit-board dynamic bending. The solder-joint cycles-to-failure data indicate that significant differences in attachment fatigue performance can be correlated with disparate lead compliance among the SM packages tested
Keywords :
elastic constants; fatigue testing; lead bonding; soldering; surface mount technology; I-lead; S-bend lead; accelerated function cycling; attachment fatigue performance; butt-lead; circuit-board dynamic bending; compliant lead designs; dimpled J-lead; directional spring constants; directional stiffness parameters; gull-wing lead; lead compliance evaluation; lead geometries; packages; solder-joint cycles-to-failure data; straight J-lead; surface mounted components; Circuit testing; Equations; Fatigue; Geometry; Lead; Life estimation; Performance evaluation; Samarium; Springs; Surface treatment;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic Components Conference, 1989. Proceedings., 39th
Conference_Location :
Houston, TX
Type :
conf
DOI :
10.1109/ECC.1989.77841
Filename :
77841
Link To Document :
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