Mechanics of Microstructures

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1 Mechanics of Microstructures Topics Plane Stress in MEMS Thin film Residual Stress Effects of Residual Stress Reference: Stephen D. Senturia, Microsystem Design, Kluwer Academic Publishers, January 200.

2 Plane Stress in MEMS In MEMS devices, a thin film deposited or formed on a substrate has some in-plane stress, referred to as Residual Stress. Plane stress arises typically due to mismatches in thermal epansion between the film and the substrate. The two components of in-plane normal stress along the principle aes are E ( σ νσ ) = y = ( σ y νσ ) = = y y E Biaial Plane Stress: and y strain components are equal to each other σ σ = σ = y = E ( νσ νσ ) y E σ = ν

3 Plane Stress in MEMS Peel Forces High stress concentration at the attachment point of the film leads to etra forces called peel forces that tend to detach the film from the substrate Debonding of tensile films tends to occur at the edges of patterned features

4 Residual Stress due to Thermal Epansion The linear thermal epansion coefficient (CTE) of a material is defined as the rate of change of uniaial strain with temperature d α T = (/K) Typical range: dt Assuming that the CTE remains constant for moderate temperature ecursions, the increase (or decrease) in strain for a finite temperature change can be written as ( T ) = ( T ) + α T o ( T o ): Strain at the original temperature To T T = T T o Incremental change in temperature

5 Residual Stress in Thin Films due to Thermal Epansion Let us assume that the film is much thinner than the substrate and is deposited onto the substrate in a stress-free state at temperature T d The sample is then cooled to room temperature T r The thermal strain of the substrate is given by s = α Ts T T = T d T r

6 Residual Stress in Thin Films due to Thermal Epansion Assume that the film is much thinner than the substrate. In this case, as a good approimation we can assume that the film must contract by the same amount as the substrate. = f, attached s f, attached = α Ts T If the film were not attached to the substrate, it would eperience a thermal strain according to its own thermal epansion coefficient f, free = α Tf T

7 Residual Stress in Thin Films due to Thermal Epansion The etra strain, i.e., the difference between the actual strain (attached case) and the unattached strain in the film (free case) is called the thermal mismatch strain f, mismatch ( α ) T = α Tf Ts The biaial strain develops an in-plane biaial stress give by σ f, mismatch = E ν f, mismatch

8 Effects of Residual Stresses What are the effects of Residual stresses? Nonuniform residual stresses in cantilevers, due either to a gradient in the material properties through the cantilever thickness or to the deposition of a different material onto a structure, can cause the cantilevers to curl In doubly-supported beams, residual stress modify the bending stiffness, and lead to important nonlinear spring effects when the deflections become comparable to the beam thickness Compressive residual stresses can cause buckling by out of plan bending

9 Before Release Residual Stress in Cantilevers Compression Compression Aial Stress: Prior to release the beam material has an average compressive stress σ o, and also a stress gradient from the deposition σ σ = σ M = o σ o Tension H / 2 ( H 2) Internal bending moment: Wσd σ M σ σ σ = WH 6 2 Tension σ σ

10 Residual Stress in Cantilevers After Release (before bending) Compression Compression σ o Compression σ σ Tension Once the beam is released, the beam length increases slightly, relieving the compressive stress so that the average stress goes to ero. However the stress gradient is still present. This stress gradient creates a moment that bends the beam. In other words, the stress variation created by bending eactly cancels the initial stress gradient. This bending produces a decrease in the tensile stress at the bottom of the beam and simultaneously a decrease in the compressive stress at the top of the beam. Thus, after bending the stress is ero everywhere in the beam. σ σ σ

11 Residual Stress in Cantilevers After Release Compression Compression σ o Tension σ σ σ σ Tension σ Radius of Curvature: The radius of curvature of the beam after bending is given by ρ = 2 Using 2 M = WH σ 6 ρ = EWH 3 2 M EH σ We know = ρ M EI and I = WH 2 The radius of curvature is epressed as a function of stress gradient 3

12 Residual Stress Effects in Cantilevers Compressive Stress Tensile Stress Is there something wrong in this figure! Source: Gabriel M. Rebei, RF MEMS: Theory, Design, and Technology, John Wiley & Sons, st edition (June 5, 2002).

13 Low spring constant Fleure Designs anchor Fleure (a) (b) (c) (d) (e) (f) Reference: W. Young and R. G. Budynas, Roark s Formulas for Stress and Strain, McGraw Hill, 2002.

14 Residual Stress due to Thermal Epansion The volume thermal epansion coefficient that accounts for linear epansions in three dimensions is given by V V = ( + )( + )( + ) y V V = 3α T T

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