DocumentCode :
158109
Title :
Prediction of remaining useful life (RUL) of ball-grid-array (BGA) interconnections during testing on the board level
Author :
Gucik-Derigny, David ; Zolghadri, Ali ; Bechou, L. ; Suhir, E.
Author_Institution :
IMS Lab., Univ. of Bordeaux, Talence, France
fYear :
2014
fDate :
1-8 March 2014
Firstpage :
1
Lastpage :
9
Abstract :
In this paper, a printed circuit board (PCB) carrying surface mounted devices (SMD) subjected to impact or vibration loads applied to its support contour is considered. A model-based prognosis approach is employed to assess the remaining useful life (RUL) of the ball-grid-array (BGA) solder joint interconnections. The approach deals with the interaction (coupling) of the “fast” PCB vibration model and the “slow” low cycle fatigue damage model of BGA solder joint interconnections. The final goal is to predict the dynamic response of the board and the RUL of the solder joint material of the BGA interconnections. As the complete knowledge of these interconnected models are typically not available, a two-stage filtering process is used to estimate the fast and slow dynamics involved. The RUL of the BGA solder joint interconnections is then estimated based on the identified models.
Keywords :
ball grid arrays; printed circuit interconnections; printed circuit testing; remaining life assessment; solders; surface mount technology; BGA solder joint interconnections; RUL; SMD; ball-grid-array solder joint interconnections; board level testing; dynamic response; fast PCB vibration model; impact loads; model-based prognosis approach; printed circuit board; remaining useful life; slow low cycle fatigue damage model; solder joint material; support contour; surface mounted devices; two-stage filtering process; vibration loads; Assembly; Damping; Handheld computers; Load modeling; Noise; Strain; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2014 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5582-4
Type :
conf
DOI :
10.1109/AERO.2014.6836228
Filename :
6836228
Link To Document :
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