Rutger Thijssen1, Tobias J Kippenberg2, Albert Polman1, Ewold Verhagen1. 1. Center for Nanophotonics, FOM Institute AMOLF , Science Park 104, 1098XG Amsterdam, The Netherlands. 2. École Polytechnique Fédérale de Lausanne (EPFL) , Lausanne, Switzerland.
Abstract
We demonstrate parallel transduction of thermally driven mechanical motion of an array of gold-coated silicon nitride nanomechanical beams, by using near-field confinement in plasmonic metal-insulator-metal resonators supported in the gap between the gold layers. The free-space optical readout, enabled by the plasmonic resonances, allows for addressing multiple mechanical resonators in a single measurement. Light absorbed in the metal layer of the beams modifies their mechanical properties, allowing photothermal tuning of the eigenfrequencies. The appearance of photothermally driven parametric amplification indicates the possibility of plasmonic mechanical actuation.
We demonstrate parallel transduction of thermally driven mechanical motion of an array of gold-coated silicon nitride nanomechanical beams, by using near-field confinement in plasmonic metal-insulator-metal resonators supported in the gap between the gold layers. The free-space optical readout, enabled by the plasmonic resonances, allows for addressing multiple mechanical resonators in a single measurement. Light absorbed in the metal layer of the beams modifies their mechanical properties, allowing photothermal tuning of the eigenfrequencies. The appearance of photothermally driven parametric amplification indicates the possibility of plasmonic mechanical actuation.
Arrays of nanomechanical resonators
have many applications, ranging from force and mass sensing[1,2] to collective nonlinear dynamics[3] and
mechanical memories and computing.[4] In
particular, large numbers of integrated mechanical sensors can enable
sensitive, rapid, label-free, and massively parallel detection of
biochemical species and trace gases.[5,6] By varying
the frequency of the oscillators in an array, the sensing bandwidth
can be effectively increased. Parallelization can also address some
of the difficulties associated with scaling down mechanical oscillator
size, which is generally favorable for sensitivity: difficulties that
include reduced power handling capability[7,8] and
reduced effective interaction cross section (i.e., the sensor surface
area). Another challenge that nanoscale mechanical systems pose is
how to efficiently transduce mechanical motion to a measurable signal,
crucial to any sensor’s operation. In the case of a sensor
consisting of multiple mechanical oscillators, it is often useful
to create a system that can be measured using a single input and single
output,[9] by separating the oscillators
in frequency. Mechanical arrays have been demonstrated using various
readout schemes: electrical readout,[10] using
optical diffraction,[11] and using (deformable)
optical waveguides.[12]Here, we demonstrate
the parallel transduction of the motion of
an array of nanobeams using a single laser beam focused on the array.
The transduction is mediated by surface plasmon Fabry–Pérot
resonances in the narrow metal-coated slots between the nanobeams.
We show how this principle[13,14] can be extended to
measuring individual mechanical resonator modes in an array of nanobeams.
We use metal–dielectric–metal plasmon resonances, which
are very sensitive to the width of the dielectric region.[15] Motion of the oscillator then changes the plasmonic
configuration, thus changing the transmission of the cavity.The small size of plasmonic resonators allows high mode overlap
with nanomechanical modes. At the same time, the free-space addressability
of localized surface plasmon resonances allows the use of simple optical
elements to couple light to and from the cavity, without having to
resort to for instance nanoscale positioning of waveguides, as is
necessary for many photonic crystal cavity[16] and microcavity[17] optomechanical implementations.
This free-space addressability makes measuring multiple mechanical
oscillators with a single laser beam a relatively straightforward
process.During the measurement, the beams absorb some of the
incident light.
We demonstrate that this leads to photothermal modification of the
beams’ eigenfrequencies.[18−21] We discuss the induced mechanical coupling between
the nanobeams. At high enough driving powers, the photothermal heating
can parametrically amplify the motion of the beams. This photothermal
amplification effect has been observed in a variety of optomechanical
systems: in metal-coated cantilevers,[22,23] in semiconductor
membranes using electron–hole pair relaxation,[24] and in microdisks.[25] Photothermoelastic
interactions may thus allow for both tuning and actuation in these
systems.
Experimental Methods
To fabricate arrays of parallel
mechanical nanobeams, 110 nm of
gold is sputter coated on commercially available high-stress stoichiometric
silicon nitride membranes of 50 nm thickness (Norcada, Canada). Using
a focused ion beam (30 keV Ga+ ions, current 10 pA), we
mill nine 18-μm-long slits in a single pass, creating eight
nanomechanical beams, each separated by a slit width of 20 nm. The
beam widths are fabricated to range in incrementing steps from 475
to 550 nm wide. The difference in beam widths lifts the degeneracy
of the in-plane eigenfrequencies and allows the identification of
individual beams from the transduced mechanical spectrum. The out-of-plane
mechanical eigenfrequencies are to first order independent of beam
width and are therefore more difficult to separate spectrally. However,
the out-of-plane and in-plane eigenmodes are well separated in frequency
(∼2.2 and ∼3.7 MHz, respectively), and we will mostly
consider the latter below.Figure 1a
shows a scanning electron microscopy
(SEM) image of the fabricated array, taken with the gold-coated side
of the membrane upward and the sample tilted at 52°. The narrow
gaps between the nanobeams are clearly visible; a larger gap is seen
for the two outer sides, where the silicon nitride membrane bends
downward due to its in-plane stress.
Figure 1
Experimental geometry. (a) SEM micrograph
of array structure, tilted
at 52°, taken on the gold side of an array of eight parallel
microbeams (beam length: 18 μm; thickness: 50 nm Si3N4, 110 nm Au; beam widths: 475 to 550 nm; gap width:
20 nm). (b) Schematic cross section of the nanomechanical beam array.
Red spots indicate plasmonic Fabry–Pérot resonances
excited in the slits between the Au layers by a 1550 nm CW laser.
(c) Frequency spectrum of light intensity transmitted through the
array, showing five distinct resonances caused by five of eight nanomechanical
beams in the array.
The sample is then placed
in a custom-built confocal transmission
microscope, which resides inside a vacuum chamber that is evacuated
to 10–3 mbar to reduce viscous air drag on the nanobeams.
A 1550 nm wavelength CW erbium-doped fiber laser is focused onto the
sample, polarized orthogonal to the slits, and incident from the gold-coated
side of the nanobeams, as shown in the schematic cross section in
Figure 1b. Different focusing conditions were
used, as will be described later on.Experimental geometry. (a) SEM micrograph
of array structure, tilted
at 52°, taken on the gold side of an array of eight parallel
microbeams (beam length: 18 μm; thickness: 50 nm Si3N4, 110 nm Au; beam widths: 475 to 550 nm; gap width:
20 nm). (b) Schematic cross section of the nanomechanical beam array.
Red spots indicate plasmonic Fabry–Pérot resonances
excited in the slits between the Au layers by a 1550 nm CW laser.
(c) Frequency spectrum of light intensity transmitted through the
array, showing five distinct resonances caused by five of eight nanomechanical
beams in the array.
Nanomechanical Transduction
Mechanical displacement affects the optical response of the slots,
changing the transmitted power. In the present geometry, the motion
of eight parallel nanobeams is measured simultaneously. Figure 1c shows the frequency spectrum measured by defocusing
the laser beam to a spot diameter of ∼5 μm, so that all
plasmonic gaps are illuminated, and detecting a power of approximately
12 μW. The peaks are related to the thermal motion of individual
mechanical modes. Interestingly, only five resonant mechanical modes
are observed in the spectrum, with varying amplitude. To analyze this,
we first discuss how the motion of the eight beams is transduced to
the measured intensity.Parallel mechanical transduction. Schematic
of transduction through
(a) constant-width and (b) alternating-width gaps. SEM micrographs
of center of arrays of (c) constant-width gap (20 nm) and (d) alternating-width
gap (20 and 50 nm) array structures. (e) Transmission through slit
as a function of slit width d, extracted from FDTD
simulations. The red line is a linear fit to the transmission through
slits of width greater than 35 nm.The motion of each of the beams is probed by its two adjacent
slits,
each of which supports a plasmonic resonance. The transmitted power
through each slit can be written as η(d), where is the
optical power density (in W/m2) interacting with slit i and η(d) is an effective scattering
cross section into the transmission
channel, which is a function of the slit width d.For in-plane motion, the two slits
at either side of the beam have
widths d1(x) = + x and d2(x) = – x, respectively,
where denotes the mean width of slit i, and x is the displacement of the beam
(we take the mean displacement x̅ = ⟨x(t)⟩ = 0). The total transmitted
power is, as such, T = η( + x) + η( – x). This power is modulated through
oscillations
of the beam, as to first (linear) orderFor a plane wave incident on a nanobeam surrounded
by two identical slits, this would lead to completely vanishing transduction
of motion as and . Figure 2a shows
a schematic of this geometry. An SEM image of such an array is shown
in Figure 2c. This equation can be expanded
to include the shape of the mechanical mode, by integrating along
the length of the beam, weighting the integral by the laser intensity
along the beam length. This will lead to a linear correction factor
for eq 1.
Figure 2
Parallel mechanical transduction. Schematic
of transduction through
(a) constant-width and (b) alternating-width gaps. SEM micrographs
of center of arrays of (c) constant-width gap (20 nm) and (d) alternating-width
gap (20 and 50 nm) array structures. (e) Transmission through slit
as a function of slit width d, extracted from FDTD
simulations. The red line is a linear fit to the transmission through
slits of width greater than 35 nm.
So far, we considered only the
slits immediately adjacent to the
moving beam to contribute to transduction. While transduction through
these two slits is likely dominating, it is in principle possible
that the slits are optically coupled, leading to transduction involving
other slits. We note that even for interacting slits the symmetry
of the system and its illumination dictate that transduction vanishes
for equal slit widths, if the total size of the array exceeds the
typical coupling length. Assuming an array of slits, labeled from −i to i, the transmission through slit i is a function of the slit’s polarizability p(x). With the
incoming beam centered on the array, we have p(x) = p–(−x), if x denotes the in-plane displacement of the middle beam. This leads
to a change in polarizability (d/dx)p(x) = (d/dx)p–(−x) = −(d/dx)p–(x). The total transmitted field
is then T ∝ ∑∑pp*. Working out the terms in this
equation for a modulation of the widths d–, d of the center two slits leads to (dT/dx) = 0.Two factors can potentially break down this expectation
and lead
to a resonance peak: (1) a different input power density on the two
slits, due to the fact that
a nonuniform (for instance, a focused) beam is used, and (2) a difference
in slit widths . Because
the plasmonic coupling strength
depends on the slit width, η is not linearly dependent on d, such that (dη/dx)() ≠ (dη/dx)() if . This implies
that by changing the width
of the slit on either side of a beam we can allow transduction of
motion to transmitted power. Importantly, it is the nonlinear dependence
of slit transmission η on slit width d (or
on slit area, for that matter) that is crucial to allow transduction.
Such a nonlinear dependence on slit width, shown in Figure 2e, is a defining characteristic of plasmonic response.
In this figure, the black data points are the transmission extracted
from a series of FDTD simulations of slits of differing widths. The
transmission is normalized to the transmission through the 20-nm-wide
slit. The red line is a linear fit to slits of widths between 35 and
100 nm, showing the nonlinear behavior of the plasmonic transmission
for slit widths narrower than 30 nm.In the structure of Figure 1 differences
between slit widths are caused by fabrication imperfections, allowing
observation of the motion of some of the beams in Figure 1c. The outermost slits in the structure are much
wider: in-plane stress in the silicon nitride causes bending in the
membrane surrounding the array structure, leading to a resonance peak
for the two outermost beams. For some of the inner beams, the surrounding
slits are also slightly different.Next, we study the transduction
for an an array in which the slits
were intentionally made alternately narrow (20 nm) and wide (50 nm),
shown schematically in cross section in Figure 2b and in an SEM image in Figure 2d. For these
structures, we expect that (dη/dx)() ≠ (dη/dx)() for all beams, based on finite-difference-time-domain
simulations of metal–insulator–metal slits of varying
width (Figure 2e). Therefore, the motion of
all beams is expected to be transduced. At the laser wavelength of
1550 nm, we find from the FDTD simulations that (dη/dx)(20 nm) = 0.75(dη/dx)(50 nm).[14]We again measured the transduction with
a defocused beam and simultaneously
detected the modulations induced by eight beams with widths ranging
from 475 to 525 nm. This time, we achieve parallel transduction of
motion of all eight beams, as shown in Figure 3, when we detect a power of 15 μW. Note that the signal-to-noise
ratio is limited by the modest mechanical quality factor (typically Q < 1000) in this proof-of-principle demonstration. The
mechanical quality factor can be straightforwardly improved by reducing
the amount of gold near the beam ends.[26] We have now seen that using alternate slit widths (20 and 50 nm)
is a viable method to enable parallel transduction of the motion of
eight parallel resonators using a single focused laser beam.
Figure 3
Frequency spectrum
of light transmitted through an array with eight
beams, with alternating-width slits of 20 and 50 nm, with beam widths
ranging from 475 to 525 nm. The laser beam was defocused to a spot
size of ∼5 μm.
Frequency spectrum
of light transmitted through an array with eight
beams, with alternating-width slits of 20 and 50 nm, with beam widths
ranging from 475 to 525 nm. The laser beam was defocused to a spot
size of ∼5 μm.To further investigate the transduction of each beam by its
two
neighboring slits, we perform measurements in which both structures
were scanned through the focus of a laser beam (2.48 ± 0.06 μm
fwhm for the constant-width array, 2.84 ± 0.13 μm for the
alternating-width array), scanning orthogonal to the long axis of
the beams. Figure 4a and b show color plots
of the spectral density of transduced power as a function of the position
of the laser beam across the constant-gap-width and alternate-gap-width
arrays, respectively. Eight different curves are now clearly resolved
for both structures, each corresponding to the motion of an individual
nanobeam. Interestingly, as the laser beam is scanned across a single
nanobeam, the mechanical resonance wavelength decreases and increases.
This will be discussed further below.
Figure 4
Mechanical resonance intensities. (a) Line scan across
the center
of an array of eight nanobeams separated by a fixed width of 20 nm.
The peak resonance frequency is plotted on the horizontal axis, and
the resonance peak intensity is represented by the color scale. Dots
indicate Gaussian fits to peak frequencies as a function of the laser
focus position on the array. (b) Similar to (a), for an array with
beams alternately separated by 20 and 50 nm. (c) Transduction curves
extracted from (a): the resonance peak intensities are shown as a
function of laser spot position (red dots), along with the peak resonance
frequencies (blue line). A dashed line indicates that the signal was
too low to extract for use in fitting. The gray vertical lines indicate
the positions of the slits, with the solid lines indicating the slits
next to the beam for which the transduction is plotted. (d) Transduction
curves extracted from (b). The focal diameters, 2.48 ± 0.06 μm
fwhm for (a) and 2.84 ± 0.13 μm for (b), were determined
from the average width of the Gaussian fits. Laser power detected
was 11.5 μW (a, c) and 10.5 μW (b, d).
Another striking feature
in the transduction spectra in Figure 4a is
that the intensity shows clear dips close to
the center for all beams, except for the two outermost ones. The red
data points in the subpanels of Figure 4c show
the mechanical transduction power at resonance for each laser beam
position. Each subpanel shows data for a single beam. The transduction
curves clearly show dips in transduction for the six center beams
when the focal spot is close to the center of each beam, when , implying a vanishing transduction, and
showing that d̅ is very similar for the seven
center slits. If the slits were all exactly equal in width, the shape
of the dip should be proportional to the derivative of the spatial
intensity profile of the laser spot on the sample. However, due to
fabrication imperfections, the slits have slightly differing widths.
We also attribute the transduction visible in Figure 1c to this. The mechanical transduction for each beam in the
alternate-gap-width array is plotted in Figure 4d. The dips in the transduction are now much less pronounced compared
to those observed for the constant-width array shown in Figure 4a and c and are in fact absent in most cases, showing
that (dη/dx)(50 nm) ≠ (dη/dx)(20 nm).Mechanical resonance intensities. (a) Line scan across
the center
of an array of eight nanobeams separated by a fixed width of 20 nm.
The peak resonance frequency is plotted on the horizontal axis, and
the resonance peak intensity is represented by the color scale. Dots
indicate Gaussian fits to peak frequencies as a function of the laser
focus position on the array. (b) Similar to (a), for an array with
beams alternately separated by 20 and 50 nm. (c) Transduction curves
extracted from (a): the resonance peak intensities are shown as a
function of laser spot position (red dots), along with the peak resonance
frequencies (blue line). A dashed line indicates that the signal was
too low to extract for use in fitting. The gray vertical lines indicate
the positions of the slits, with the solid lines indicating the slits
next to the beam for which the transduction is plotted. (d) Transduction
curves extracted from (b). The focal diameters, 2.48 ± 0.06 μm
fwhm for (a) and 2.84 ± 0.13 μm for (b), were determined
from the average width of the Gaussian fits. Laser power detected
was 11.5 μW (a, c) and 10.5 μW (b, d).The measurements in Figures 3 and 4 provide direct proof that the transduction
through
the arrays is due to a plasmonic effect. If the transmission through
the slits was simply due to a geometric effect, i.e., a transmission
that is linearly proportional to the slit width, we would not observe
any transduction of motion: for in-plane motion, the total width of
the two slits surrounding a nanobeam is constant, and therefore no
transduction would be expected. However, the plasmonic resonance mediating
the transmission through the slit will lead to nonlinear dependence
of transmission on slit width (as shown in Figure 2e), allowing the alternate-slit-width structure to improve
transduction of the in-plane mechanical mode, and precludes the observed
effects being due to a purely geometric modulation of the transmitted
light by the beams’ motion.
Thermal Tuning of Eigenfrequencies
Figure 4 shows that the mechanical eigenfrequencies
of the beams depend strongly on their position relative to the laser
spot. We ascribe this to a photothermal effect: heating-induced expansion
of the tensile-stressed beams causes a reduction in the axial stress,
leading to reduced resonance frequencies. The maximum frequency shift
is observed when the laser beam is centered on a nanobeam, where heating
is maximum. We perform Gaussian fits to the (thermally shifted) resonance
frequency as a function of laser focus position for each beam. The
blue lines in the subpanels of Figure 4c and
d show the thermally tuned frequency shift Δf = (ftuned – f0)/f0. Frequency shifts as
high as 5% (150 kHz) are observed.To further investigate this
effect, we calculate the relative frequency
shift as a function of absorbed power using a simple thermal model.[18,19,20,21] We calculate the eigenfrequencies as a function of stress in the
nitride layer of the beams:with L the length of the
beam, w the width, h the thickness,
and I the geometrical moment of inertia, and using
geometric averaging to calculate the effective stress σe, Young’s modulus Ee, and
density ρe for the Au/Si3N4 bilayer beams.[28,29] This geometric averaging is valid
when most of the forces are along the length of the beams, implying
that the system is far from buckling due to thermal stresses. As we
are measuring the fundamental mode, we use β = 4.730 04.[30] Note that all equations are also valid for single-layer
beams.To fit the model to the data, we first extract the nonthermally
shifted eigenfrequencies f from the Gaussian fits in Figure 4a,b
and plot these as a function of beam width in Figure 5a. We then fit eq 2 to the data using
the effective Young’s modulus Ee and stress σe as free parameters, using length
and height as determined from SEM images and using literature values
for the mass densities of gold and silicon nitride. Figure 5a shows good agreement between model and data for
an effective Young’s modulus of Ee = 75.2 GPa, between the value of that for gold and silicon nitride.
We will assume the Young’s moduli are independent of temperature.[31,32] The fitted effective stress (in the low-power limit) is 36.5 MPa.
Assuming the manufacturer’s specification of σe = 250 MPa, this implies that there is a compressive stress of σAu = −60 MPa in the gold layer.
Figure 5
(a) Nonthermally shifted
eigenfrequencies for constant-width array
(blue data points derived from Figure 4a,c)
and alternate-width array (red dots, derived from Figure 4b,d) and model, fitting effective Young’s
modulus Ee and in-plane stress σe. (b) Measured thermally induced maximum frequency shifts
from Figure 4 for constant-width (blue) and
alternating-width (red) arrays as a function of beam width. The drawn
lines are fits using eq 6, with the fraction
of absorbed power γ as a free parameter. (c) Calculated frequency
shift in %/mW of absorbed power for a gold-coated silicon nitride
beam, plotted as a function of beam width. The purple line is for
the alternating-width array; the blue line, for the constant-width
array.
(a) Nonthermally shifted
eigenfrequencies for constant-width array
(blue data points derived from Figure 4a,c)
and alternate-width array (red dots, derived from Figure 4b,d) and model, fitting effective Young’s
modulus Ee and in-plane stress σe. (b) Measured thermally induced maximum frequency shifts
from Figure 4 for constant-width (blue) and
alternating-width (red) arrays as a function of beam width. The drawn
lines are fits using eq 6, with the fraction
of absorbed power γ as a free parameter. (c) Calculated frequency
shift in %/mW of absorbed power for a gold-coated silicon nitride
beam, plotted as a function of beam width. The purple line is for
the alternating-width array; the blue line, for the constant-width
array.Next, we investigate the effect
of heating of the nanobeams as
they absorb light, changing the stress in the nanobeam through the
thermal expansion coefficient:where σ is the original stress
determined above, σt is
the thermal stress, ΔT is the average temperature
increase of the nanobeam, and αe is the effective
thermal expansion coefficient αe = (αSiASi + αAuAAu)/(ASi + AAu),where A = w × h is the cross-sectional area
of layer i. For this formulation for σe to be valid, we assume the end points of the beam do not
move. We can then calculate the relative frequency change due to heating,
using eq 2:where ft is the
thermally tuned frequency (eq 2 with σ
from eq 3), f is the prestressed frequency without heating (eq 2 with σe = σ), and f0 is the eigenfrequency
for a beam with no added stress (σe = 0).We
use a one-dimensional heating model, in which the beam is heated
by a power Pabs applied evenly across
the cross section of the beam at x0, while
the ends of the beam are kept at ambient temperature (T(0) = T(L) = 298 K). In the stationary
case, the absorbed power equals the outgoing fluxes:with κ the heat conductivity,
so that
ΔT = PabsL/8κA. Using eqs 3–5, we findThe untuned
frequencies f0 and f are
extracted from the Gaussian fits to the thermal tuning as shown in
Figures 4 and 5a. Effective
parameters for α and κ are derived from the weighted averages
using αSi = 1.23 ×
10–6 K–1, αAu = 14 × 10–6 K–1, κSi = 2.5 W m–1 K–1, and κAu = 320 W m–1 K–1.[20] That leaves
the absorbed power Pabs to be directly
determined from δf using eq 6.Assuming the laser focus has a 2D Gaussian shape,
the power density
absorbed on one beam, with width w, can be expressed
as a function of the incident power Pin and a parameter γ describing the fraction of incident power
that is absorbed in the beam:For example, for the constant-width array,
a 500-nm-wide beam has 18% of the total optical power incident upon
it, given the laser spot size. For the alternating-width array, the
slightly larger focal width leads to a 500-nm-wide beam having 16%
of the total power incident upon it. Figure 5b shows the measured maximum thermally induced frequency shift from
Figure 4 as a function of beam width for the
constant-width and alternating-width arrays. The frequency shift is
stronger for narrower beams, as these have a lower heat capacity.
The drawn lines are fits of eq 6 to the data,
taking into account the width dependence of the incident power on
the area of the beam (eq 7) and assuming a fixed
fraction γ of the power incident on the beam to be absorbed
in the beam. We find the data can be fitted well with this model for
both constant- and alternating-width arrays and find that for a 500-nm-wide
beam Pabs = 611 μW for the constant-width
array and Pabs = 396 μW for the
alternating-width array.Using the thermal frequency shift model,
we find that for both
the constant-width and alternating-width arrays, the sensitivity of
frequency to absorbed power is, for a 500-nm-wide beam, δf/Pabs = 6%/mW. This is shown
in Figure 5c, dividing out the focal width
and power in Figure 5b. Because the heat capacity
of a narrow beam scales with its width, the narrower beams are more
sensitive to Pabs. We find that the sensitivity
to absorbed power is the same for both structures, as would be expected.
Parametric
Oscillation of Nanobeams
We have also studied the out-of-plane
mechanical mode under high
illumination power; Figure 6 shows the mechanical
resonance spectrum for an array of eight beams under 10 mW irradiation.
The mechanical transduction amplitude exceeds the noise by 50 dB and
is much more than in Figure 3. Also, the effective
quality factor of the resonance increases to Qm > 50.000; this is a lower limit determined by thermal
fluctuations
that shift the resonance during the measurement averaging time. Figure 6 shows several harmonics at a frequency spacing
exactly equal to the fundamental frequency of 2.21 MHz. The appearance
of these higher order sidebands is intrinsic to the large modulation
amplitude (up to 10% of the dc transmitted power). At these modulation
amplitudes, power is transferred not only to the first sideband but
also to higher order sidebands.[33] Spectra
such as that shown in Figure 6 are observed
for laser powers > 8 mW, with the exact threshold depending on
the
laser focusing condition.
Figure 6
Mechanical response of a beam undergoing thermally
induced parametric
amplification, showing greatly increased response amplitude, high
effective Q-factor, and higher order sidebands of
the fundamental out-of-plane mode at 2.21 MHz.
Mechanical response of a beam undergoing thermally
induced parametric
amplification, showing greatly increased response amplitude, high
effective Q-factor, and higher order sidebands of
the fundamental out-of-plane mode at 2.21 MHz.We attribute this behavior to parametric oscillations[17,21] that occur due to a driving force that is bolometric in nature:[25,34] for the out-of-plane mode, power absorbed in the beams causes an
out-of-plane bending stress, due to the bilayer geometry of the beams
and the differing thermal expansion coefficients αSi and αAu of silicon nitride
and gold, which, if this stress is modulated at twice the mechanical
frequency, can lead to parametric oscillations. When the out-of-plane
displacement of one of the beams increases, the incoupling into the
plasmonic resonance is reduced, reducing the heating and allowing
the beam to cool off, with a certain time delay controlled by the
heat capacity, restoring the equilibrium position. Then, light can
be coupled back into the cavity, once again increasing absorption,
driving the beams to greater and greater displacement. This process
is eventually limited by coupling of mechanical energy into the higher
harmonics of the system.
Avoided Crossings in Arrays of Beams
Multiple mechanical oscillators can not only be used for parallelization
of measurements. If the mechanical modes are coupled, a range of different
effects can be observed and exploited, for instance using localized
modes[35] to improve sensitivity[36] or using coupled resonances to create mechanical
RF filters,[37,38] to enable single-input single-output
mass sensing[39] or to observe synchronization.[40]If two resonators are coupled and then
are tuned to make their
eigenfrequencies match, their eigenfrequencies as a function of coupling
will show an avoided crossing, as shown earlier for nanomechanical
systems.[41,42] Figure 7b shows a
FEM simulation of the in-plane eigenmode of the fourth beam, showing
that the neighboring beams also contribute to the eigenmode. To study
the coupling between the beams, we fabricated an array of eight beams
with beam widths leading to in-plane eigenfrequencies such that they
could be thermally tuned to match. This was achieved by fabricating
an array of eight beams with widths of 425, 450, 459, 480, 500, 525,
545, and 570 nm, where the second and third beams have nearly identical
widths. The gap widths were fabricated to be alternating between 20
and 40 nm.
Figure 7
(a) Mechanical
transduction spectrum of an array of eight microbeams,
engineered to show avoided crossings in the thermally tuned eigenfrequencies
of the microbeams. The widths of the beams were chosen such that one
pair of neighboring beams would have similar eigenfrequencies. The
dashed outlines indicate avoided crossings. The solid outline indicates
a nonavoided crossing. (b) Simulated array of beams of increasing
widths showing the shape of the fourth in-plane eigenmode, showing
that the neighboring beams are also in motion due to the coupling
at the anchoring points of the beams. Displacements are greatly exaggerated
for clarity.
Figure 7a shows the measured
mechanical
transduction as a function of frequency and of the position of the
focused laser beam in the array. The thermal tuning behavior observed
in Figure 4 is clearly observed for four beams.
Two avoided crossings are observed, indicated by the dashed outlines.(a) Mechanical
transduction spectrum of an array of eight microbeams,
engineered to show avoided crossings in the thermally tuned eigenfrequencies
of the microbeams. The widths of the beams were chosen such that one
pair of neighboring beams would have similar eigenfrequencies. The
dashed outlines indicate avoided crossings. The solid outline indicates
a nonavoided crossing. (b) Simulated array of beams of increasing
widths showing the shape of the fourth in-plane eigenmode, showing
that the neighboring beams are also in motion due to the coupling
at the anchoring points of the beams. Displacements are greatly exaggerated
for clarity.We also observe a nonavoided
crossing, suggesting these mechanical
modes are related to nonadjacent beams. For nonadjacent beams, we
expect very low mechanical coupling between these beams and, therefore,
do not expect to see a splitting in the crossing.
Conclusion
We demonstrate parallel transduction of the thermally driven mechanical
motion of an array of nanobeams using a simple free-space technique.
The motion of each beam is transduced by the adjacent plasmonic slits.
When these are identical, the transduction of in-plane motion can
cancel, due to antisymmetric transduction by the slits. By tuning
the gap width, the plasmonic resonances are tuned, allowing simultaneous
parallel transduction of the mechanical modes of all beams.The thermal tuning due to optical power absorption leads to resonance
frequency shifts as large as 6%/mW of power absorbed in the beam.
At powers above 8 mW parametric oscillations are observed due to a
bolometric driving force. We find that neighboring beams are mechanically
coupled through the membrane in which they are suspended. When thermally
tuning such an array to make the eigenfrequencies of two neighboring
beams match, the coupling between these beams creates an avoided crossing
in the transduced mechanical modes of these two beams. The photothermoelastic
effect observed in this work could therefore find application in tuning
and actuating plasmonic micro- and nanomechanical resonators.The principle of parallel plasmonic mechanical transduction could
be used in a variety of sensor array applications, due to its simple
free-space readout and scalability to include many more resonators
than shown here.