micromechanical nanographite resonators20nanograph… · sam fishlock, harold chong, john mcbride,...
TRANSCRIPT
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Characterisation of nanographite
for MEMS resonators
Sam Fishlock, Harold Chong, John McBride,
Sean O’Shea, Suan Hui Pu MRS Fall 2015
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Carbon materials for MEMS and NEMS • Investigated materials: diamond-like carbon, graphite, graphene
• Applications: switches, low friction materials and resonators
• Good mechanical properties and device scalability
• AIM: Demonstrate fabrication and characterisation of nanographite MEMS
resonators without transfer
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CVD onto catalyst
Transfer onto substrate
Low yield for fragile NEMS
Our plan:
direct deposition
K.M. Milaninia, Appl. Phys. Lett. 95 (2009)
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Nanocrystalline graphite deposition
• 6-inch silicon wafer substrate
• Oxford instruments Nanofab PECVD
• Scalable and reproducible →
standard microfabrication process
Temperature (°C) 750
Methane flow (sccm) 75
Hydrogen flow (sccm) 60
Pressure (mTorr) 1500
RF Power (W) 100
M.E. Schmidt et. Al, Mater. Res. Exp. 1 (2014). www.azom.com
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Material characterisation • Raman and SEM confirm nanocrystalline grain structure
• Electrical resistivity 10.0 mΩ cm
• XRR measurement – density ρ 1900 kg/m3
• Typical roughness 3 nm RMS from AFM contact mode
• Film thickness between 8 and 340 nm
Resistivity by
electrical
measurements
100 nm
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Film stress
Stress gradient in
the film…
… causes curvature
in cantilevers
Applied stress
Average compressive stress causes
buckling in doubly clamped beams
20 um 20 um
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Device fabrication
• Surface micromachining, optical lithography
• Pattern and etch
nanographite into
beam shape
• E-beam evaporated
Ni/Ti electrodes
• HF vapour isotropic
etch for beam release
Nanographite
PECVD Silicon dioxide
SC Silicon substrate
KEY:
Anchor
Undercut
Undercut changes stress in beam section
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Simulation
• Modelled as classic beams under tension where Natural frequency f varies
with : Length L , Stiffness E, density ρ ,Stress S and Moment of Inertia I :
• Finite element simulation shows added
length due to the undercut ~ 3%
Nominal length
Effective length
2 2
2 21
EI SLf
L EI
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Laser source
Split beam – Doppler
shift used to calculate
vibration amplitude
Actuation and measurement
• DC VDC + AC V0 voltage creating electrostatic force F to actuate the beam
• Sweep AC voltage at frequency f and measure the vibration using vibrometer
Measured 1st
vibration mode
2 2
0
1 12 sin 2
2 2DC DC
C CF V V V V ft
r r
Actuation
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Resonance results
• Verification from the finite element model
• Young’s modulus from the cantilevers is 23 GPa
• Frequency of the doubly clamped beams dominated by stress
0
5
10
15
20
25
30
35
10 20 30 40 50 60
Fre
qu
en
cy
(kH
z)
Thickness / length2 (m-1)
Experimental
results
Linear (FE
Simulation)
Simulation for Young’s modulus
→ 23 GPa
0
100
200
300
400
500
600
700
0 10 20 30 40 50 60
Fre
qu
en
cy (
kH
z)
Thickness / length2 (m-1)
Experimental results
Linear (Analytical
stressed model)
Linear (Analytical
stress free)
Cantilever results Doubly clamped beam results
9 MPa tensile stress
Device lengths 75 to150 µm. Thickness 300 nm to 340 nm
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Results - quality factor
30 mTorr
Q ~ 1300
Ambient
Q ~ 20
• Quality factor ‘Q’ – energy loss at resonance. Calculated from the FWHM
of fitted curve
• Losses are intrinsic, clamping, extrinsic
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Increasing bias voltage
Tuning the natural frequency
• Increasing the DC bias causes electrostatic spring softening to change the
natural frequency
• 0.2 % per volt average tunability in linear range
10
250
260
270
280
290
300
310
320
330
340
350
0 500 1000 1500 2000 2500 3000
Fre
quency
(kH
z)
DC Bias2 (V2)
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Conclusions
• Route to standard fabrication of thin nanographite and nanographene
devices by PECVD
• Electrostatically actuated and tuned resonator device
• Low modulus, high stress material → used the stress gradient to create
tensile devices which raises the vibration frequency
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• Dr Suan Hui Pu
• Dr Harold Chong
• Prof John McBride
• Dr Kian Kiang
• Dr Owain Clark
• Mr Michael Perry
• Dr Sean O’Shea
• Dr Xiaosong Tang
• Mr Andrew Breeson
• Dr Meysam Mirshekarloo
• Mr Lim Poh Chong
Sincere thanks to co-authors and technical help
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Thankful acknowledgment of funding from:
• A*STAR research attachment scheme, Singapore
• Faculty of Engineering and the environment, University of Southampton
• Malaysian Ministry of Higher Education grant FRGS/2/2014/TK03/USMC/02/1
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0
5
10
15
20
25
30
35
10 20 30 40 50 60
Fre
qu
en
cy
(kH
z)
Thickness / length 2 (m-1)
Experimental
results
Linear (FE
Simulation)
0
100
200
300
400
500
600
700
0 10 20 30 40 50 60
Fre
qu
en
cy (
kH
z)
Thickness / length2 (m-1)
Experimental results
Linear (Analytical
stressed model)
Linear (Analytical
stress free)
Thank you - Any questions?
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