DocumentCode :
2273971
Title :
Electronics reliability prognosis through material modeling and simulation
Author :
Nasser, Loren ; Curtin, Maggie
Author_Institution :
VEXTEC Corp., Brentwood, TN
fYear :
0
fDate :
0-0 0
Abstract :
Electronic systems, such as power supplies, are complex multilayered devices consisting of different materials with inherent variability. Thermal gradient cycling occurs during system operation which eventually results in thermo-mechanical fatigue induced material failure. Such material failures can result in immediate electronic system shutdown with no advanced fault or warning signals. This NAVAIR sponsored SBIR project uses state-of-the-art material modeling to predict degradation of circuit board elements as a means for "simulated fault detection". This effort has been focused on the specific aspect of solder fracture and fatigue since electronic industry statistics have attributed this failure issue as a driving factor in system reliability. This project demonstrates feasibility for using conventional sensing, combined with thermal modeling, to predict solder degradation due to thermal cycling as a means to prognosticate electronic power supply system reliability. Current status, as well as future plans, of electronic prognosis development is discussed
Keywords :
circuit reliability; fatigue cracks; fault simulation; power supply circuits; solders; electronic prognosis development; electronics reliability prognosis; material failure; material modeling; material simulation; power supply system reliability; simulated fault detection; solder degradation; solder fracture; thermal gradient cycling; thermal modeling; thermo-mechanical fatigue; Circuit faults; Fatigue; Materials reliability; Power supplies; Power system modeling; Power system reliability; Predictive models; Printed circuits; Thermal degradation; Thermomechanical processes;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
Type :
conf
DOI :
10.1109/AERO.2006.1656125
Filename :
1656125
Link To Document :
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