The mechanical properties of thin films can vary significantly due to variations in the deposition process. Monitoring these properties is essential when, e.g., engineering micro-mechanical devices. Established methods such as wafer bending and bulge testing provide only average values for the entire wafer or impose constraints on the sample fabrication process. Therefore, a method to efficiently characterize mechanical properties locally with simple sample fabrication is desirable. In this study, we determine the stress in direct-current magnetron-sputtered aluminum nitride films on prefabricated silicon nitride membranes by measuring the fundamental eigenfrequencies of the membranes and combining it with mechanical band structure simulations. We find that the stress, which is directly related to the strain, transitions from compressive to tensile as a function of the film thickness. Our simple and robust method allows in situ measurements that are compatible with existing nanofabrication techniques of, e.g., hybrid photonic circuits and can probe the stress locally over the chip.
Micromechanical membranes are an important platform for a wide range of electro- and optomechanical experiments. This goes all the way from applications like ultra-sensitive scanning force microscopy,1 radio frequency signal amplification,2 and microwave to optics conversion,3 to fundamental studies of cavity optomechanical backaction,4 exceptional points,5 and radiative heat transfer mediated via Casimir fluctuations.6 Their size in the 100-micrometer range allows the study of, e.g., mode-hybridization7 and the spatial structure of nonlinear dynamics.8,9 Another important aspect of these very thin membranes is that they allow to study the properties of materials placed on top.10 This provides an interesting route to measuring the mechanical properties of a variety of materials that can be deposited or grown on top of membranes.
Here, we employ high-stress silicon nitride (SiN) membranes to study the properties of aluminum nitride (AlN) grown on top of it. AlN is not only an important piezo-electric material for classical devices, but it is an emerging material for quantum technology11 with applications ranging from mechanical resonator–qubit coupling,12 microwave to optics conversion,13 on-chip isolation,14 photon-pair generation using spontaneous parametric downconversion,15 frequency shifting of single photons,16 to hybrid photonics.17 For many of the aforementioned applications, knowing the mechanical properties of the AlN is crucial.18,19 Furthermore, the mechanical and optical properties are sensitive to variations in the deposition conditions20,21 and are often correlated. The growth may also vary spatially22 and thus make it desirable to locally determine the mechanical properties in situ on the same chip without negatively impacting the intended application. We show that this is possible with bilayer membranes, which are readily fabricated, robust, and easy to measure. The stress in the AlN top layer can be determined as a function of the film thickness from the membrane's mechanical resonance frequency shift, in combination with mechanical band structure calculations.
Figure 1(a) shows optical micrographs of resulting membranes. The different colors result from the different AlN thicknesses, , which are determined using optical reflectometry.17 Each chip is glued onto a piezo-electric actuator and mounted in a vacuum chamber. The driven motion of its 120 membranes is detected optically in a scanning interferometric setup with a probe laser (wavelength 633 nm) as detailed in Refs. 7 and 25. A brief setup description can also be found in the supplementary material. Figure 1(b) shows the responses of a typical bilayer membrane and a SiN-only membrane. There, the fundamental (1,1) modes appear at different frequencies, showing the influence of AlN. Higher modes are also visible. Membranes dominated by bending rigidity will show different fundamental-to-higher-mode frequency ratios than tension-dominated membranes. In our case, the higher modes match with the calculated with Eq. (1) and the extracted , thus confirming that these membranes are indeed in the tension-dominated regime. Still, to avoid that bending rigidity (which becomes more important for smaller membranes and/or higher modes10) starts to influence the results,25 we limit the analysis to membranes with size , of which there are 53 on each chip. For all membranes, the exact resonance frequency and quality factor are obtained semi-automatically from detailed driven response measurements in the linear or weakly nonlinear regime.25 This is repeated for all chips with different AlN thicknesses. We observe that the more AlN is deposited, the lower the resonance frequency is. Figure 1(b) already showed that for the SiN-only membrane doped to when depositing 77 nm AlN. Such a comparison can be done for all 120 membranes on each chip. These differ in the numbers of holes as well as in lattice constant A and thus have different dimensions. Hence, varies strongly,25 making it difficult to see subtle trends when comparing frequencies directly. Equation (1) shows that by multiplying with twice the effective membrane size , the speed of sound c is obtained. Its value depends on the bilayer properties as outlined above, but—importantly—it should be size-independent. Given the close relation between the quantity and c, we will also call the former the speed of sound.25 Figure 1(c) shows that, although the frequencies from which c was extracted varied by more than a factor of 3, c is indeed independent of . Moreover, the decrease in c with increasing AlN thickness is now much more visible than when plotting directly.25 Table I shows that the change in c is not simply proportional to the AlN thickness; there is, e.g., a large decrease in c for the 45 nm layer, whereas the difference between the 77 and 140 nm films is quite small. The in-plane tensile stress of the AlN films clearly affects the tension of the membrane.
(a) Optical micrographs of the nominally same membrane on four different chips with the AlN thickness indicated. The support and membrane have different colors and the release holes are visible as dark dots. (b) Driven responses of membranes with 77 nm AlN (orange) and without AlN (gray). The dotted lines show and the other resonances calculated from Eq. (1). (c) Speed of sound vs the effective membrane size for different AlN thicknesses. The solid line shows the mean value (see also Table I).
(a) Optical micrographs of the nominally same membrane on four different chips with the AlN thickness indicated. The support and membrane have different colors and the release holes are visible as dark dots. (b) Driven responses of membranes with 77 nm AlN (orange) and without AlN (gray). The dotted lines show and the other resonances calculated from Eq. (1). (c) Speed of sound vs the effective membrane size for different AlN thicknesses. The solid line shows the mean value (see also Table I).
Overview of all 16 measured sets of membranes (four chips with different AlN thicknesses (color coded) and four different lattice constants A). The mean and standard deviation over the different sizes are stated for the measured speed of sound . The extracted stress is indicated in the last column.
. | . | . | . |
---|---|---|---|
0 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 | |||
45 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 | |||
77 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 | |||
140 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 |
. | . | . | . |
---|---|---|---|
0 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 | |||
45 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 | |||
77 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 | |||
140 | 14.56 | ||
12.56 | |||
10.56 | |||
8.56 |
The accuracy of the method also allows for the detection of small trends. Interestingly, Table I shows that c depends on the lattice constant A. This is not expected from the “ideal”-membrane model presented above. Looking back at the micrographs of Fig. 1(a) shows that the actual geometry is not a perfect rectangular membrane. First of all, the membranes are not continuous but have periodically arranged holes through which the buffered hydrofluoric acid (BHF) etches the oxide, forming cylindrical “drums” of suspended SiN. After 130 min, the undercut of is so large that fully suspended membranes are formed but with slightly “wavy” edges.29 The SiN is also partially etched. On the top, it thins uniformly, but at the bottom side, longer BHF exposure closer to the holes results in conical profiles.25,30 All these effects can be accounted for with computationally expensive three-dimensional finite element (FEM) simulations.25 However, since the entire structure is periodic, mechanical band structure simulations provide a good alternative as shown there. Figure 2(b) shows the calculated band structure of the unit cell shown in Fig. 2(a); the color indicates the polarization of the modes. In addition to the flexural modes, the longitudinal and transverse modes were also observed. Further details about the simulations can be found in the supplementary material. In the following, we will only consider the experimentally observable flexural modes.7 For small k, their frequency depends linearly on the wavenumber. For increasing k, a slightly higher slope (i.e., an increased group velocity) is observable; this is due to the bending stiffness. Furthermore, near the edges of the Brillouin zone gaps open, as visible in the zoom of the area near the X point. These effects become important for large , whereas we are interested in the opposite limit. Note that the wavevector is fixed by the membrane size and mode: and likewise for y. Since only the fundamental mode of large membranes is studied here, the band structure near the -point is the most relevant. There, is linear and the group velocity matches the speed of sound c. Modes propagating in different directions may have different speeds of sound,25 but for the lowest mode, c is independent of the direction of [cf. circular shape of Fig. 2(c)]. Therefore, the membrane can be treated as isotropic and just a single value needs to be simulated to obtain c for all combinations of and . With this simplification, one could think that the patterning has little impact, but this is not true, as the experimental values in Table I already showed. When a unit cell of an idealized membrane, i.e., one without release holes and with a uniform thickness , is simulated [Fig. 2(d)], the results match with Eq. (4). However, for the more realistic geometry with holes and partly etched SiN, simulations must be used to connect the speed of sound to the bilayer properties.25 We note that using a geometry close to the “ideal” membrane is also possible, e.g., by using commercial membranes.31 It is the convenient combination of our in situ measurement, front-side-only processing, and easy interferometric detection that results in this geometry, which requires this modest computational step. This approach is illustrated in Fig. 2(e), where we plot the dependence of the speed of sound on the stress in the AlN film for the four different thicknesses studied in the experiment. For zero stress in the AlN layer, c decreases with increasing , due to the increased mass . For (right side), the speed of sound converges to a single value as also predicted by the simple model of Eqs. (2)–(4). Note that in the stress-dominated regime, bending rigidity is unimportant, but this may no longer be the case for very thick membranes. This will then be signaled by a nonlinear dependence in the simulations or dependence in the experiments. Returning to the experimental data, the sample without AlN is considered first. Here, the simulations are fitted to the experimental values for c by varying the SiN film stress.32, Table I shows the value that is obtained using this method. In contrast to the simple model of Eq. (4), this now yields a consistent for all lattice constants, despite the observed variation of c with A. This shows that the mechanical band structure calculations are essential for quantitatively understanding the membranes. Combining all SiN-only data gives a weighted mean value for the tensile in-plane stress, which is used for the subsequent simulations of bilayer membranes. By adjusting the stress in the AlN film, these simulations are fitted to the experimental c. The resulting for every set of A and is listed in Table I, whereas the combined (i.e., with all A for a given ) fits are shown in Fig. 3(a). The FEM model again reproduces the upward trends with increasing lattice constant, although experimentally, the dependence is a bit flatter than in the simulations. The stress values obtained by fitting the data are shown in Fig. 3(b), with negative stress values for the 45 nm and the 77 nm thick film. This indicates a compressive strain in the AlN, translating into a reduced in-plane stress component of the bilayer membrane. For the thickest AlN film, the strong reduction in c with increasing thickness has halted and the 140 nm thick AlN film has a tensile stress. Such a transition has also been observed in other AlN thin films.27,33,34 The increased tension from the strained AlN film outweighs the additional increase in mass. These measurements thus show the feasibility of using micromechanical membranes to determine the stress (and with the elastic constants also the strain) in the top layer. The method is nondestructive, easy to use, and unlike wafer-bending22,27,33–35 and bulge-test22,36 techniques, it is fully compatible with pre-patterned samples like our hybrid AlN-on-SiN photonic integrated circuits17 and will also work with samples where the second film is not continuous.37 Furthermore, every membrane probes the local material properties and the uniformity can be studied over a chip or wafer. To demonstrate this, the spatial dependence is studied in Fig. 4. Panel (a) shows the speed of sound. The colorscale shows that c decreases with the vertical position on the chip. This is, however, mainly due to variation of A in the chip design [cf. Fig. 3(a)]. Still, devices on the right-hand side of the chip appear to have slightly higher c than the left side. To make this more apparent, is determined for every membrane individually and plotted in Fig. 4(b). To avoid any residual systematic trends with the lattice constant, the average value over all membranes with the same A is subtracted. This map clearly shows the gradient of the stress over the chip. The variations are only about a few percent of the stress in the SiN membrane, highlighting the sensitivity. Further improvements will focus on reducing the variations and fit uncertainty and also on extracting the elastic moduli, e.g., by probing different modes and/or smaller membranes, and the dissipation.10
Band structure simulations. (a) Rendering of a simulated unit cell with SiN in gray and AlN in blue. The lattice constant is and the AlN thickness is 140 nm. The z direction has been magnified by 10× for better visibility. (b) Band structure for the geometry in (a) with a zoom near the X-point. The colors indicate the polarization of the modes. Inset: first Brillouin zone (blue) and special -points. (c) Dependence of the speed of sound of the lowest flexural mode on the direction of for . (d) Comparison of Eq. (4) (black line) to the simulated c of an “idealized” membrane, i.e., without any removal of SiN or release holes (open), and a realistic geometry as depicted in (a) where all these effects are included (filled symbols). (e) Speed of sound vs for different thicknesses. In all other panels, .
Band structure simulations. (a) Rendering of a simulated unit cell with SiN in gray and AlN in blue. The lattice constant is and the AlN thickness is 140 nm. The z direction has been magnified by 10× for better visibility. (b) Band structure for the geometry in (a) with a zoom near the X-point. The colors indicate the polarization of the modes. Inset: first Brillouin zone (blue) and special -points. (c) Dependence of the speed of sound of the lowest flexural mode on the direction of for . (d) Comparison of Eq. (4) (black line) to the simulated c of an “idealized” membrane, i.e., without any removal of SiN or release holes (open), and a realistic geometry as depicted in (a) where all these effects are included (filled symbols). (e) Speed of sound vs for different thicknesses. In all other panels, .
(a) Experimental (symbols) speed of sound, fitted with the FEM simulations (lines). (b) Extracted stress for every individual data point (bars, see Table I) and the value obtained from the fits in (a). Without AlN, the plot shows , whereas for nonzero AlN thickness it is . The error bars indicate the fit uncertainty.
(a) Experimental (symbols) speed of sound, fitted with the FEM simulations (lines). (b) Extracted stress for every individual data point (bars, see Table I) and the value obtained from the fits in (a). Without AlN, the plot shows , whereas for nonzero AlN thickness it is . The error bars indicate the fit uncertainty.
(a) Map of the speed of sound for the chip with 77 nm AlN. The size of the marker indicates (not to scale). (b) Map of the fitted AlN stress values with the average over each block (i.e., set of three rows) subtracted. The chip size is and has a 1 mm wide border without any patterning, leaving a device area with 12 rows. Every block has the same value of A, ranging from 14.56 (top) to (bottom). Some membranes were broken or damaged and are omitted.
(a) Map of the speed of sound for the chip with 77 nm AlN. The size of the marker indicates (not to scale). (b) Map of the fitted AlN stress values with the average over each block (i.e., set of three rows) subtracted. The chip size is and has a 1 mm wide border without any patterning, leaving a device area with 12 rows. Every block has the same value of A, ranging from 14.56 (top) to (bottom). Some membranes were broken or damaged and are omitted.
In summary, we demonstrated the use of micromechanical membranes to probe the mechanical properties of thin films, specifically the stress in AlN on SiN. Additionally, we showed that the speed of sound can vary depending on the geometry of the release holes. Finally, we presented the use of these membranes as local probes to examine the mechanical properties across a centimeter-large sample.
SUPPLEMENTARY MATERIAL
See the supplementary material for details on the fabrication of silicon nitride membranes, optical detection, and simulations.
We thank P. Soubelet for discussions, J. Röwe for initial measurements, D. Hoch and N. Mange for assistance with nanofabrication, and M. Müller for growth of the AlN. This work is funded by the German Research Foundation (DFG) under Germany's Excellence Strategy (EXC-2111-390814868) and received the support of the Technical University of Munich – Institute for Advanced Study, funded by the German Excellence Initiative and the European Union Seventh Framework Programme under Grant Agreement No. 291763.
AUTHOR DECLARATIONS
Conflict of Interest
The authors have no conflicts to disclose.
Author Contributions
Timo Sommer: Resources (equal); Supervision (supporting); Writing – original draft (supporting); Writing – review & editing (equal). Aditya: Formal analysis (equal); Investigation (equal); Writing – review & editing (equal). Rudolf Gross: Funding acquisition (equal); Writing – review & editing (equal). Matthias Althammer: Funding acquisition (equal); Resources (equal); Writing – review & editing (equal). Menno Poot: Conceptualization (equal); Funding acquisition (equal); Software (equal); Supervision (lead); Writing – original draft (lead); Writing – review & editing (equal).
DATA AVAILABILITY
The data that support the findings of this study are available from the corresponding author upon reasonable request.