Numerical Example

Input data

Structural element

#1 (Package)

U2 (Substrate)

0 (Bonding Material)

Young’s modulus, kg/mm2

8775

2320

TBD

Poisson’s ratio

0.28

0.32

0.35

Shear modulus, kg/mm2

3428

879

TBD

CTE. 1/°C

6.5E-6

15.0E-6

X

Thickness, mm

2.0

1.5

0.05

Half package (assembly) length. / = 7.5 mm Measured force (within the elastic region) T = 0.325 kg/mm Corresponding (measured) displacement, = 2.6 x 10“5 mm Force at failure 7} = 36.0 kg/mm

Calculated data

Axial compliances:

Total interfacial compliance of the assembly Parameter of the interfacial shearing stress Shearing stress at the assembly end Stress at failure

Interfacial compliances of the assembly components

Interfacial compliance of the bonding layer Shear modulus of the bonding material

Tentative Young’s modulus

Possible Characterization of the Solder Material Properties

The developed model was also used to explain a paradoxical situation that was originally detected on the basis of finite element analysis (FEA) by Jorma Kivilahti and Tommi Reinikainen [48]: deep enough transverse grooves in the adherends (“pins”)

Transverse grooves in the adherends lead to lower and more uniformly distributed interfacial stresses

FIGURE 8.2 Transverse grooves in the adherends lead to lower and more uniformly distributed interfacial stresses.

(Figure 8.2) resulted in an appreciable reduction in, and to the more uniform distribution of, the interfacial shearing and peeling stresses. This phenomenon, important from the standpoint of testing solder materials, was explained based on analytical modeling by Suhir and Reinikainen [49, 50]. The model indicates that the observed phenomenon is due primarily to the increase in the interfacial compliance of the bonding structure: the grooves “convert” the adherend (“pin”) portions located between the inner portions of the grooves and the bonding (adhesive, solder) layer into parts of the bonding structure, thereby increasing the compliance of this structure with respect to the shearing load. This positive effect overwhelms, as far as the magnitude and the distribution of the interfacial stresses are concerned, the negative effect of the increased axial compliance of the loaded portions of the adherends (“pins”), because of the grooves.

The analytical predictions agree well with the FEA data, despite the FEA overestimation of the increase in the interfacial stresses in the proximity of the joint edges (as is known, FEA method, which is based on one of the numerical methods of the elasticity theory, leads to singular stresses at the edges of assemblies comprised of dissimilar materials).

The obtained information explains the physics of the phenomenon in question, and the developed analytical models can be used in the analysis and physical design of soldered lap shear joints. It is also concluded that analytical modeling is able not only to come up with relationships that clearly indicate “what affects what and what is responsible for what,” but, more importantly, can explain the physics of phenomena that neither the FEA modeling (“simulation”), nor even actual experimentation is able to. It is recommended that such tests are considered to obtain the mechanical properties of the solder materials for further analytical or FEA modeling.

CONCLUSION

elastic moduli of the bonding material if the interfacial displacement is also measured. In the author’s opinion, the suggested methodology, based on the concept of the interfacial compliance, could become a basis for a new effective experimental method for assessing the interfacial shearing strength and elastic moduli of the bonding material in electronics. The methodology can be used particularly in application to the recently suggested sintered silver bonding materials to evaluate their bonding strength from the measured force-at-failure and shear modulus from the measured shearing force and displacement.

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