air damping of oscillating mems structures: modeling and ...1. vtt technical research centre of...

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Air Damping of Oscillating MEMS Structures: Modeling and Comparison with Experiment S. Gorelick 1 , J.R. Dekker 1 , M. Leivo 1 , U. Kantojärvi 1 , 1. VTT Technical Research Centre of Finland, Tietotie 3, Espoo, P.O.Box 1000, FI-02044, Finland Introduction: Air damping can be detrimental to the performance of vibrating MEMS components. Quantitative evaluation of the damping is challenging due to the complex interaction of air with moving structures and typically requires numerical simulations. A full three-dimensional analysis can be computationally very expensive, time consuming and not feasible. Here, we present a simplified two-dimensional modeling of damping per unit length of selected MEMS structures. The simulated air damping results were compared with experimental measurements of corresponding piezoactuated resonators: in-plane and out-of-plane tuning forks, two types of out-of-plane cantilevers and a torsional micromirror. The applicability of the simplified model is verified by a good (2-30%) agreement between the simulated and measured Q-values. The simulated systems aimed at modeling the air damping of selected MEMS devices. The test devices were fabricated using c-SOI technology (cavity Si on insulator). The air flow damping invloves several types of flow. The devices were actuated by means of thin (1 μm) aluminium nitride piezolayers processed on top of the released structures. Out-of-plane cantilever. Cross-sections 100×50 (C1) and 50×50 μm (C2) In-plane tuning fork. Cross-section 100×50 μm (TF1) Out-of-plane tuning fork. Cross-sections 26×50 and 52×50 μm (TF2) Torsional mirror. Cross-section 400×50 μm (M) Simplified 2D COMSOL flow model: Initially deformed beam with a tip displacement A is subdivided into narrow cross-sections of width dx and mass dm, each displaced by an intial amplitude A i , such that the envelope of the {A i } resembles the initial mode shape of the beam. The cross- sections oscilate vertically and synchronously at the resonance frequency of the original beam due to the action of numerical spring forces dk. The approximation is justified if the beam length is much greater than its other dimensions (the air flow profile can be assumed 2D), and the flow is laminar with negligible interaction of air flows induced by neighbouring cross-sections. The simulations were in time domain. The Q-values were estimated from the logarithmic decrement of the amplitudes A i . Reynolds number (Re): 0.01…5.27. The flow is laminar. Knudsen number (Kn): 3.5…7×10 -3 (gap sizes are 10-20 μm). Slip flow dynamics is more applicable. Mach number (M): Max velocities are < 8 m s -1 (<< 330 m s -1 ). Incompressible flow. Experimental characterisation: The characterisation of the devices was based on measuring their electrical frequency- admittance curves around the resonance. The mechanical Q- values both in vacuum and air were derived from the R m L m C m -C 0 equivalent circuit fits. Damping due to the viscious damping force (Q in air) is then device f0, kHz Q in air Q vacuum Q flow Q simulated Agreement C1 80 150 6500 153 168 91% C2 80 180 6530 185 265 70% TF1 250 1200 40000 1240 1190 96% TF2 1000 5600 16000 8615 8820 97% M 50 175 50000 176 214 82% Authors would like to thank Authors would like to thank Collaborative Project Collaborative Project EUROStars EUROStars HighResSense HighResSense (TEKES, (TEKES, Bruco Bruco Integrated Circuits BV, Integrated Circuits BV, Innoluce Innoluce BV, SILEX BV, SILEX Microsystems AB, VINNOVA and NL Agency, VTT) Microsystems AB, VINNOVA and NL Agency, VTT) for financial support for financial support *contact: *contact: [email protected] [email protected] visit : visit : http://www.vtt.fi http://www.vtt.fi The fabrication of the samples used in this study was funded by The fabrication of the samples used in this study was funded by Collaborative Project Collaborative Project PiezoMEMS PiezoMEMS (TEKES, Murata Electronics (TEKES, Murata Electronics Oy Oy, TDK , TDK-EPC, EPC, Okmetic Okmetic Oy Oy and VTT) and VTT) The studied test systems involve various types of motion within pre-etched cavities (in-plane , out-of-plane , torsional ) and in a wide range of frequencies (10 4 …10 6 Hz ). The Q-values from simplified 2D simulation agree very well with the experimentally measured values. The good agreement of the simulation and experiment validates the model and its applicability for modeling of air damping in other MEMS systems.

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Page 1: Air Damping of Oscillating MEMS Structures: Modeling and ...1. VTT Technical Research Centre of Finland, Tietotie 3, Espoo, P.O.Box 1000, FI-02044, Finland Introduction: Air damping

Air Damping of Oscillating MEMS Structures: Modeling and Comparison with Experiment

S. Gorelick1, J.R. Dekker1, M. Leivo1, U. Kantojärvi1, 1. VTT Technical Research Centre of Finland, Tietotie 3, Espoo, P.O.Box 1000, FI-02044, Finland

Introduction: Air damping can be detrimental to the performance ofvibrating MEMS components. Quantitative evaluation of the damping ischallenging due to the complex interaction of air with moving structuresand typically requires numerical simulations. A full three-dimensionalanalysis can be computationally very expensive, time consuming and notfeasible. Here, we present a simplified two-dimensional modeling ofdamping per unit length of selected MEMS structures. The simulated airdamping results were compared with experimental measurementsof corresponding piezoactuated resonators: in-plane and out-of-planetuning forks, two types of out-of-plane cantilevers and a torsionalmicromirror. The applicability of the simplified model is verified by a good(2-30%) agreement between the simulated and measured Q-values.

The simulated systems aimed atmodeling the air damping of selectedMEMS devices. The test deviceswere fabricated using c-SOItechnology (cavity Si on insulator).The air flow damping invlovesseveral types of flow. The deviceswere actuated by means of thin (1µm) aluminium nitride piezolayersprocessed on top of the releasedstructures.

Out-of-plane cantilever. Cross-sections 100×50 (C1) and

50×50 µm (C2)

In-plane tuning fork. Cross-section 100×50 µm (TF1)

Out-of-plane tuning fork.Cross-sections 26×50 and 52×50

µm (TF2)

Torsional mirror. Cross-section 400×50 µm (M)

Simplified 2D COMSOL flow model: Initially deformedbeam with a tip displacement A is subdivided into narrowcross-sections of width dx and mass dm, each displacedby an intial amplitude Ai, such that the envelope of the {Ai}resembles the initial mode shape of the beam. The cross-sections oscilate vertically and synchronously at theresonance frequency of the original beam due to theaction of numerical spring forces dk. The approximation isjustified if the beam length is much greater than its otherdimensions (the air flow profile can be assumed 2D), andthe flow is laminar with negligible interaction of air flowsinduced by neighbouring cross-sections. The simulationswere in time domain. The Q-values were estimated fromthe logarithmic decrement of the amplitudes Ai.

Reynolds number (Re):0.01…5.27. The flow islaminar.

Knudsen number (Kn):3.5…7×10-3 (gap sizesare 10-20 µm). Slip flowdynamics is moreapplicable.

Mach number (M): Maxvelocities are < 8 m s-1

(<< 330 m s-1).Incompressible flow.

Experimental characterisation:

The characterisation of thedevices was based on measuringtheir electrical frequency-admittance curves around theresonance. The mechanical Q-values both in vacuum and airwere derived from the RmLmCm-C0equivalent circuit fits. Dampingdue to the viscious damping force(Q in air) is then

device f0, kHz Qin air

Q vacuum

Qflow

Q simulated

Agreement

C1 80 150 6500 153 168 91%C2 80 180 6530 185 265 70%

TF1 250 1200 40000 1240 1190 96%TF2 1000 5600 16000 8615 8820 97%M 50 175 50000 176 214 82%

Authors would like to thankAuthors would like to thankCollaborative Project Collaborative Project EUROStarsEUROStars HighResSenseHighResSense (TEKES, (TEKES, BrucoBruco Integrated Circuits BV, Integrated Circuits BV, InnoluceInnoluce BV, SILEX BV, SILEX Microsystems AB, VINNOVA and NL Agency, VTT) Microsystems AB, VINNOVA and NL Agency, VTT) for financial support for financial support

*contact:*contact: [email protected]@vtt.fi

visit :visit : http://www.vtt.fihttp://www.vtt.fi

The fabrication of the samples used in this study was funded by The fabrication of the samples used in this study was funded by Collaborative Project Collaborative Project PiezoMEMSPiezoMEMS (TEKES, Murata Electronics (TEKES, Murata Electronics OyOy, TDK, TDK--EPC, EPC, OkmeticOkmetic OyOy and VTT)and VTT)

The studied test systems involve various types of motion within pre-etchedcavities (in-plane, out-of-plane, torsional) and in a wide range offrequencies (104…106 Hz). The Q-values from simplified 2D simulationagree very well with the experimentally measured values. The goodagreement of the simulation and experiment validates the model and itsapplicability for modeling of air damping in other MEMS systems.