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. 2016 Aug 9:7:12496.
doi: 10.1038/ncomms12496.

Force sensitivity of multilayer graphene optomechanical devices

Affiliations

Force sensitivity of multilayer graphene optomechanical devices

P Weber et al. Nat Commun. .

Abstract

Mechanical resonators based on low-dimensional materials are promising for force and mass sensing experiments. The force sensitivity in these ultra-light resonators is often limited by the imprecision in the measurement of the vibrations, the fluctuations of the mechanical resonant frequency and the heating induced by the measurement. Here, we strongly couple multilayer graphene resonators to superconducting cavities in order to achieve a displacement sensitivity of 1.3 fm Hz(-1/2). This coupling also allows us to damp the resonator to an average phonon occupation of 7.2. Our best force sensitivity, 390 zN Hz(-1/2) with a bandwidth of 200 Hz, is achieved by balancing measurement imprecision, optomechanical damping, and measurement-induced heating. Our results hold promise for studying the quantum capacitance of graphene, its magnetization, and the electron and nuclear spins of molecules adsorbed on its surface.

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Figures

Figure 1
Figure 1. Mechanical displacement and force sensitivity.
(a) Mechanical displacement spectrum Sz close to the mechanical resonance frequency ωm/2π. The total displacement spectral density formula image at ωm is the sum of the displacement noise formula image and the displacement imprecision formula image. (b) Corresponding force sensitivity formula image (dark grey). The individual components are the thermal force noise formula image (dark yellow) and the imprecision force noise formula image (turquoise), given by equations (1) and (2), respectively. The quantum back-action noise is neglected for simplicity. For the plots most of the parameters are those of device B, but we estimate the mass assuming that the graphene flake is a single layer. Further we choose nadd=0.5, Tbath=0.015 K, and np=2·105 in a (see text).
Figure 2
Figure 2. Device and characterization.
(a) False-colour image of the device. The cavity is coloured in dark yellow. The graphene flake is clamped in between niobium support electrodes (grey) and cross-linked poly(methyl metracylate) (turquoise). The scale bar is 5 μm. (b) Schematic cross-section of the graphene resonator along the white dashed dotted line in a. (c) Schematic of the measurement circuit. The graphene mechanical resonator is coupled to the superconducting LC cavity through the capacitance Cm. The separation d between the suspended graphene flake and the cavity counter electrode is controlled by the constant voltage Vg. The cavity is pumped with a pump tone at ωp and the output signal is amplified at 3 K. (d) Reflection coefficient |S11|2 and (e) reflected phase Δφ11 of the superconducting cavity of device A at Vg=3.002 V. The dark yellow lines are fits to the data using κint/2π=950 kHz and κext/2π=850 kHz using equation (7) (see Methods). (f) Driven vibration amplitude of the graphene resonator of device A as a function of drive frequency. The driving voltage is 22 nV and Vg=3.002 V. The dark yellow line is a lorentzian fit to the data. (g) Resonant frequency ωc/2π of the superconducting cavity as a function of Vg. (h) Resonant frequency ωm/2π of the graphene resonator as a function of Vg. The black line is the Vg dependence of ωm expected from electrostatic softening (see Supplementary Note 1).
Figure 3
Figure 3. Effective mechanical energy decay rates extracted from ring-down measurements.
Mechanical dissipation rate formula image measured on device A with the ring-down technique as a function of the number np of pump photons in the cavity at Vg=0 V and Vg=3.002 V, where np is proportional to the microwave power Pin applied at the input of the cryostat (see Supplementary Note 3). Red and blue data points correspond to red and blue detuned pumping, respectively. The measurements are well described by formula image (red and blue lines) using g0/2π=9.7 Hz in a and g0/2π=42.6 Hz in b. The inset in b shows a ring-down measurement for np=1.4·106. We plot the normalized vibration amplitude as a function of time t. The resonator is driven with a capacitive driving force for t<t0. At t0 the drive is switched off and the vibration amplitude decays freely (t>t0). We fit the data with an exponential decay (black line) using formula image with a decay rate formula image. The vibration amplitude in ring-down measurements is larger than that in undriven displacement spectra, so that the motion in ring-down measurements can be resolved with lower np.
Figure 4
Figure 4. Thermal calibration and sideband cooling of fundamental mechanical mode with red-detuned pumping.
(a) Selected thermo-mechanical noise spectra for different temperatures and np=6·104. (b) Plot of the measured mechanical mode temperature of device A, expressed in phonon occupation nm, as a function of cryostat temperature at Vg=3.002 V where ωm/2π=53.7 MHz and np=6·104. On the right y-axis, we display the variance of the vibration amplitude 〈z2〉, which is obtained by integrating the thermal resonance, as is shown in a. The phonon occupation is quantified with formula image (see Supplementary Note 3). The error bars are given by the standard deviation of 5 spectral measurements. (c) Mechanical displacement spectral density Sz measured for different pump photon number. The cryostat temperature is 15 mK. Note that the curves are not offset. (d) Displacement imprecision as a function of cavity pump photon population. The line is a fit of equation (3) with nadd=32. (e) Average phonon number nm as a function of np. The error bars are given by the standard deviation of five spectral measurements.
Figure 5
Figure 5. Characterization of the force sensitivity.
(a) Force sensitivity formula image as a function of cavity pump photon population measured when pumping the cavity on the red sideband. (b) Imprecision force noise formula image (turquoise) and thermal force noise formula image (dark yellow) versus np. The data in a,b are fitted to equations (2), (6). (c) Product of the bath temperature Tbath and the intrinsic mechanical decay rate formula image as a function of cavity pump photon occupation. The line is a fit to the data. (d) Effective spectral mechanical line width formula image and energy decay formula image as a function of np. The data are fitted to formula image with δΓnoise/2π=8.7 kHz (red line). (eh) Equivalent to (ad) but for device B. The lowest value for the force sensitivity in e is formula image. In e and f the data are fitted with nadd=22 and in h we use g0/2π=7.3 Hz, κ/2π=2.5 MHz and δΓnoise/2π=0.145 kHz. All the measurements on device A are performed at Vg=3.002 V and on device B at Vg=0 V. The cryostat temperature is 15 mK.

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