mems resonator - comsol multiphysics · 23-10-2012 nxp mems resonator presentation by drs. helger...
TRANSCRIPT
23-10-2012 NXP
MEMS resonator
Presentation by
Drs. Helger van Halewijn
1
Excerpt from the Proceedings of the 2012 COMSOL Conference in Milan
MEMS resonator overview package
• Resonator size 500 x 700 x 150 micron • Single silicon on CMOS technology • High frequency stability, low time jitter, low temperature
drift. • Low motion damping Q-factor > 40000 (≈ 50 MHz)
23-10-2012
NXP 2
Overview of dogbone resonator
23-10-2012 NXP
actuation gap
anchor “mass ” of resonator
spring
3
Schematic of dogbone resonator
23-10-2012 NXP 4
Some parameters studied in COMSOL
• During production in waferfab all dimensions variations can influence the performance
• Q-factor, resonance stability 1. Dimensions resonator head 2. Anchor loss 3. Thickness Si 4. Oxidation layer 5. Air pressure (vacuum)\ 6. Thermal losses. 7. Viscous Drag 8. Electrostatic actuation+fringing 9. Mode coupling.
23-10-2012 NXP 5
Non linear resonance frequency
• Resonance frequency
1. k spring constant 2. m mass system 3. V driving voltage 4. w width 5. h height 6. g gap 23-10-2012 NXP
203
sin( ) DCel AC
DCres
V xF V tg
V whkfm mg
ηη ω
ε
= +
−=
6
Q-factor estimation
• Reciprocal addition.
• Anchor loss : Qanchor≈ 104 -107 dimension • Thermo-elastic loss Qte≈ 104-106 material • Surface loss: Qsur≈ 106-108 debris or cracks • Air damping: Qair≈ 102 – 107 vacuum quality, leakage • Viscous drag Qdrag ≈ 105-107 vacuum quality
• All seperate Q factors are estimated with COMSOL.
23-10-2012 NXP
1
1 1N
itot iQ Q=
=∑
7
Overview resonance mode at 56 MHz
23-10-2012 NXP 8
Acoustic loss at anchor.
23-10-2012 NXP 9
Acoustic loss: Gray domains, PML
23-10-2012 NXP 10
• Red arrows
indicate PML-layers.
• In PML complete acoustic absorption.
• Blue domains represent normal material properties.
• Eigenfrequency analyses.
Acoustic loss: dimensional variations in the structure.
23-10-2012 NXP 11
23-10-2012
NXP 12
Capacitances
•Area of gate within green lines is 41084 μm2 (drain area excluded)
Fringe effects, from simple to real system
Simulated Cap = 338 fF
Dominated by drain bottom capacitance
23-10-2012 NXP 13
23-10-2012
NXP 14
1. Simple hand calculation Drain C1 = 322 fF 2. Gate C2 = 1270 fF and Source C3 = 18700 fF 3. Capacitance C12=22.5 fF and C23=51 fF 4. Using mathematical formula
5. Cgate = 1264 fF 6. Comsol result is Cgate Comsol= 1266 fF OK 7. Csource and Cdrain have similar accuracies.
Calculation + Simulation Gate Capacitance
312
2312 111
CCC
CCCgate
++
++=
23-10-2012
NXP 15
Capacitance as function of resistivity
1. Results from Comsol 2. Including effects like air height and
substrates thickness 3. Resonator operates at 0.3 – 1.2 Ωcm (
equivalent to 80 – 330 S/m) 4. Capacitance variation is < 2% in resistivity
range 5. All simulations are performed with 56 MHz
Gate
1.00E-14
1.00E-13
1.00E-12
1.00E-11
1.00E-04 1.00E-03 1.00E-02 1.00E-01 1.00E+00
1.00E+01
1.00E+02
1.00E+03
1.00E+04
Conductance [S/m]
Cap
acita
nce
[F]
Y11 100 200Y11 100 300Y11 200 200Y11 200 300
Feedthrough Capacitance
1.00E-14
1.00E-13
1.00E-12
1.00E-11
1.00E-04 1.00E-03 1.00E-02 1.00E-01 1.00E+00 1.00E+01 1.00E+02 1.00E+03 1.00E+04
Conductance [S/m]
Cap
acita
nce
[F]
Y11Y21 100 200Y11Y12 100 300Y11Y12 200 200Y11Y12 200 300
Drain
1.00E-14
1.00E-13
1.00E-12
1.00E-11
1.00E-04 1.00E-03 1.00E-02 1.00E-01 1.00E+00 1.00E+01 1.00E+02 1.00E+03 1.00E+04
Conductance [S/m]
Cap
acita
nce
[F]
Y22 100 200Y22 100 300Y22 200 200Y22 200 300
Asymmetric amplitude under electrical load (V bias)
• At 10 Volt, a harmonic behavior.
• At 80 Volt bias an inharmonic term can easily be seen.
• At 56 MHz, oscillation time is 40 nsec.
• COMSOL time step < 1 nsec
23-10-2012 NXP 16
Static stress due to process cycles
23-10-2012
NXP 17
Static stress at perifery due to curing procedures at various process conditions Stress concentrations in resonator legs.
•Ue 1.1 µm
•Ue 7.1 µm •Ue 13.1 µm
Q-factor of resonator under Stress
23-10-2012
NXP 18
0
50000
100000
150000
200000
250000
300000
0.E+00 2.E-06 4.E-06 6.E-06 8.E-06 1.E-05
Q fa
ctor
Underetch [μm]
Q-factor as function of Underetch and Stress
0 MPa 2.6 MPa 5.3 MPa 10.5 MPa 21.0 MPa 31.5 MPa
Thermal losses in resonator
• Q-factor can be written as:
• E = Youngs Modulus [Pa] • α = expansioncoefficient [1/m] • To = ambient temperature [K] • ρ = density [kg/m3] • ω = frequency [rad/s] • τ = thermal relaxation [s]
23-10-2012 NXP 19
2
2
11 ( )
o
therm p
E TQ C
α ωτρ ωτ
=+
Thermal losses in resonator
23-10-2012 NXP 20
Temperature fluctuations of about ±100C, at 56 MHz. This mechanism is due to material properties.
23-10-2012 NXP
Thickness Oxidation: Q factor and frequency shift
• Simulation with single layer.
• Mesh is adapted at layers lower than 20 nm.
• Minimum layer thickness 2.5 nm.
• In Comsol, Solid mechanics and shells are combined.
Q factor Straight resonator
0
2000000
4000000
6000000
8000000
10000000
12000000
14000000
0 10 20 30 40 50 60
SiO2 Layer thickness [nm]
Q fa
ctor
55000000
55200000
55400000
55600000
55800000
56000000
56200000
56400000
0 20 40 60
Freq
uenc
y [H
z]
SiO2 Layer thickness [nm]
Frequency Straight resonator
21
Squeezed film effect including stress
23-10-2012 NXP 22
1000
10000
100000
10 100 1000 10000 100000
Q-fa
ctor
Pressure [Pa]
Q-factor compared with measurements KIM
Q-factor 12nm
Q-factor 20nm
KIM
• Q > 40000 at appropriate conditions
• Sliding effect on large surface negligable
• Q-factor is slightly dependant on mesh size of the surface where the film damping is applied.
Overview: Influence of Polyamide Capping above resonator
23-10-2012 NXP 23
10,000
100,000
1,000,000
10,000,000
100,000,000
-30.00 -20.00 -10.00 0.00 10.00 20.00 30.00 40.00 50.00Q
-fact
or
Frequency shift [ppm]
Q factor and Capping stress, Polyimide only
UnderEtch 5.4 [μm]
UnderEtch 1.4 [μm]
-10 MPa
-100 MPa
100 MPa
31 MPa
10MPa
Permanent frequency shifts: ≈ 20 ppm Well within specs.
Conclusion • Production steps in CMOS technlogy have their own
influence on the performance of the resonator. • COMSOL paved the way to better understanding to control
specs in production. (Q-factor, dimensions, stress and material loss factors)
• MEMS module was used together with the mechanical module. – Prestressed Analysis, eigenfrequency – Prestressed Analysis, frequency domain. – Heat module, Squeezed film and much more.
• Thanks to Dr. H van de Vlist (NXP, Nijmegen)
Dr. J. van Beek (NXP, Eindhoven) 23-10-2012
NXP 24