Characterization of the Complete Stress State in Thin-film CMOS Layered Materials Via Postbuckling

Figure 1

Figure 1: Post-release out-of-plane deformation of micromachined structures (see ref. 2).

Characterization of thin-film layered materials is critical for many MEMS devices. Residual stresses from production determine both the final shape and the performance of microdevices and should therefore be accurately determined. Stresses are typically extracted using simple test structures (clamped beams and cantilevers, see Figures 1a-b) that allow for mean and gradient residual stress estimation [1]. However, current approaches to material characterization have two major limitations. First, their accuracy is directly proportional to their cost. This is especially true for mean compressive stress, where more accurate estimates require a larger number of different test structures. Second, they oversimplify test-structure boundary conditions by considering them to be ideal (e.g., perfectly clamped in the case of buckled beams for mean compressive stress determination [1] ). To overcome these issues, we have developed a new methodology for characterizing the complete stress state (effective mean and gradient stresses) in CMOS layered materials that also assesses the non-ideality of clamped boundaries [2] . The approach uses a closed-form solution of the buckling problem of micromachined beams including non-ideal boundaries (Figure 1c). Table 1 shows show the results relative to the characterization of four different CMOS material combinations. The outcomes show mean stresses ranging between 15 and 105MPa, thus demonstrating the method’s capability to characterize structures subjected to both large and small compressive stresses. This capability is in contrast with traditional critical length methods that encounter difficulties in quantifying small compressive stresses due to their inability to distinguish between mean stress and gradient stress effects [2] . For the CMOS materials examined here, the accuracy was ± 2MPa for mean stresses and ±3MPa/µm for gradients. Boundary non-ideality is found to be 90% of perfectly clamped condition for the CMOS-released films, having such a significant effect on the extracted stresses that it must be considered.

Table 1: Characterization of thin-film CMOS layered materials using analytical models (see ref. 2)
Beam Composition Effective Young’s modulus
[GPA]
Effective mean (compressive) stress
[MPa]
Effective gradient stress
[MPa/μm]
Effective boundary condition
[-]
A:PolySi/Dielectric
Composite
129 105 ± 2.1 37 ± 2.9 0.89 ± 0.05
B: Dielectric Composite 111 90.35 ± 2.3 42 ± 3.1 0.9 ± 0.05
C: Al/Poly/Dielectric Composite 132 37.1 ± 1.5 25.9 ± 2.8 0.905 ± 0.05
D: Al/Dielectric Composite 113 15 ± 1.8 -2.7 ± 2.1 0.9 ± 0.05

References
  1. M.J. Madou, Fundamentals of Microfabrication: The Science of Miniaturization, 2nd Edition, CRC Press, New York, USA. [] []
  2. F. Fachin, M. Varghese, S.A. Nikles, B.L. Wardle, “Characterization of the Complete Stress State in Thin-Film CMOS Layered Materials,” in Proc. Hilton Head, 2010, In press. [] []

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