Thermo-mechanical analysis of solder joint fatigue and creep in a flip chip on board package subjected to temperature cycling loading

Author(s):  
J.H.L. Pang ◽  
Tze-Ing Tan ◽  
S.K. Sitaraman
1991 ◽  
Vol 113 (2) ◽  
pp. 121-128 ◽  
Author(s):  
R. G. Ross

Differential expansion induced fatigue resulting from temperature cycling is a leading cause of solder joint failures in spacecraft. Achieving high reliability flight hardware requires that each element of the fatigue issue be addressed carefully. This includes defining the complete thermal-cycle environment to be experienced by the hardware, developing electronic packaging concepts that are consistent with the defined environments, and validating the completed designs with a thorough qualification and acceptance test program. This paper describes a useful systems approach to solder fatigue based principally on the fundamental log-strain versus log-cycles-to-failure behavior of fatigue. This fundamental behavior has been useful to integrate diverse ground test and flight operational thermal-cycle environments into a unified electronics design approach. Each element of the approach reflects both the mechanism physics that control solder fatigue, as well as the practical realities of the hardware build, test, delivery, and application cycle.


Author(s):  
Mohammad Masum Hossain ◽  
Dereje Agonafer ◽  
Puligandla Viswanadham ◽  
Tommi Reinikainen

The life-prediction modeling of an electronic package requires a sequence of critical assumptions concerning the finite element models. The solder structures accommodate the bulk of the plastic strain that is generated during accelerated temperature cycling due to the thermal expansion mismatch between the various materials that constitute the package. Finite element analysis is extensively used for simulating the effect of accelerated temperature cycling on electronic packages. There are a number of issues that need to be addressed to improve the current FEM models. One of the limitations inherent to the presently available models is the accuracy in property values of eutectic 63Sn/37Pb solder or other solder materials (i.e. 62Sn/36Pb/2Ag). Life prediction methodologies for high temperature solders (90Pb/10Sn, 95Pb/5Sn, etc.) or lead-free based inter-connects materials, are almost non-existent due to their low volume use or relative infancy. [1] Another major limitation for the models presently available is excluding the effect of intermetallic compound (Cu6Sn5, Cu3Sn) formation and growth between solder joint and Cu pad due to the reflow processes, rework and during the thermal aging. The mechanical reliability of these intermetallic compounds clearly influences the mechanical integrity of the interconnection. The brittle failures of solder balls have been identified with the growth of a number of intermetallic compounds both at the interfaces between metallic layers and in the bulk solder balls. In this paper, the effect of intermetallic compound in fatigue life prediction using finite element modeling is described. A Chip Scale Package 3D Quarter model is chosen to do the FE analysis. Accelerated temperature cycling is performed to obtain the plastic work due to thermal expansion mismatch between the various materials. Solder joint fatigue life prediction methodologies were incorporated so that finite element simulation results were translated into estimated cycles to failure. The results are compared with conventional models that do not include intermetallic effects. Conventionally available material properties are assumed for the eutectic 63Sn/37Pb solder and the intermetallic material properties. The importance of including intermetallic effect in finite element modeling will be discussed.


Author(s):  
Xueming Jiang ◽  
Pengrong Lin ◽  
Yuezhong Song ◽  
Yingzhuo Huang ◽  
Binhao Lian ◽  
...  

Author(s):  
D. Farley ◽  
Y. Zhou ◽  
A. Dasgupta ◽  
J. F. J. Caers ◽  
J. W. C. de Vries

An LGA (Land Grid Array) laminate-based epoxy-molded RF SiP (system-in-package) containing four wirebonded and three flip-chip dice is qualified for quasi-static mechanical flexure using a PoF (Physics-of-Failure) approach. The process includes: design and execution of accelerated stress testing; failure analysis to identify the failure mode and mechanism; and mechanistic simulations to assess acceleration factors for extrapolation of the failures to field environments for selected failure mechanisms. Illustrative qualification results are presented for solder joint fatigue.


Author(s):  
Chin Hock Toh ◽  
Arun Raman ◽  
Thomas Fitzgerald ◽  
Madhuri Narkhede ◽  
Alfred A. La Mar ◽  
...  

This paper summarizes the intermetallic compounds (IMC) formation at the interface between thermal interface material (TIM) and nickel/gold plated integrated heat spreader (IHS) at varying Au thickness, and its impact on thermal reliability. Indium solders due to their high thermal conductivity are commonly used as the TIM to dissipate heat from silicon die to the thermal lids for new generation microprocessors with higher operating die temperatures. Indium solders readily wet the Au plating on thermal lids to form IMC during soldering. Optimal Au thickness is essential; Au thickness should be thick enough for reliable soldering, but must also be thin enough to offset the high cost and to prevent formation of a brittle Au-rich IMC layer in the solder joint. AuIn2 is the preferred IMC for indium-gold soldering and does not embrittle the solder joint. Resulting IMC type depends on the Au:In ratio which can be predicted by a In-Au binary phase diagram. On this basis, critical Au plating thickness to form AuIn2 IMC can be estimated using the known density values for electroplated gold and indium. In this study, Au thicknesses ranging from 0.035 to 0.2μm with a fixed gold pad size were electrolytically plated on a nickel plated copper lid. Assembled units were then subjected to Temperature Cycling-B (TCB). An in-house developed metrology for measuring junction-to-case thermal impedance (Rjc) is described. In this study, varying the thermal lids Au-plating thickness between 0.035 to 0.2 μm only lead to slight increase in center and corner Rjc values through 115 cycles TCB. The maximum center Rjc degradation post thermal cycling observed was only ∼ 1.7% on the lids with Au pad thickness between 0.035 – 0.04 μm. There were also no clear indications of impact of Au pad thickness on center and corner Rjc performance at EOL or post 115 cycles TCB. Thermal lids/TIM interface integrity remains unchanged for the range of Au pad thickness considered. However, detailed scanning electron microscopy and energy dispersive spectroscopy showed thicker Au plating results in greater incidence of AuIn2 IMC nodules beneath In-Ni-Au ternary IMC layer at end of line (EOL) ie post packaging and test. AuIn2 IMC is formed right after assembly and is what that holds the solder to the lid. As such, it follows that the presence of a more continuous and possibly greater number of AuIn2 IMC nodules can be expected to provide a better lid-solder joint at EOL.


2019 ◽  
Vol 286 ◽  
pp. 02002
Author(s):  
H. Hamdani ◽  
B. Radi ◽  
A. El Hami

In the mechatronic devices, the finite element analyses are the most used method to determine time-dependent solder joint fatigue response under accelerated temperature cycling conditions, the deterministic analyses are the most used methods. However, the design variables show variability and randomness which will affect the lifetime prediction quality. This paper focuses on solder joint reliability in tape-based chip-scale packages(CSP) with the consideration of uncertainties in material parameters.


2007 ◽  
Vol 353-358 ◽  
pp. 2932-2935
Author(s):  
Yong Cheng Lin ◽  
Xu Chen ◽  
Xing Shen Liu ◽  
Guo Quan Lu

The reliability of solder joints in flip chip assemblies with both compliant (flex) and rigid (PCB) substrates was studied by accelerated temperature cycling tests and finite element modeling (FEM). In-process electrical resistance measurements and nondestructive evaluations were conducted to monitor solder joint failure behavior, hence the fatigue failure life. Meanwhile, the predicted fatigue failure life of solder joints was obtained by Darveaux’s crack initiation and growth models. It can be concluded that the solder joints in flip chip on flex assembly (FCOF) have longer fatigue life than those in flip chip on rigid board assembly (FCOB); the maximum von Mises stress/strain and the maximum shear stress/strain of FCOB solder joints are much higher than those of FCOF solder joints; the thermal strain and stress in solder joints is reduced by flex buckling or bending and flex substrate could dissipate energy that otherwise would be absorbed by solder joint. Therefore, the substrate flexibility has a great effect on solder joint reliability and the reliability improvement was attributed to flex buckling or bending during temperature cycling.


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