Thin films of amorphous silicon (a-Si) coated on metals such as nickel (Ni) are one of the most promising anode architectures for high-energy-density lithium-ion (Li-ion) batteries. The performance and longevity of batteries with this type of electrode depend on the integrity of the Ni/a–Si interface. The integrity of the a-Si /Ni bonded interface during cycling is critical, but the experimental characterization of interfacial failure of this material system is highly challenging and there is a sparsity of interface strength data in the literature. Here, we describe a laser spallation (LS) technique to characterize the interfacial adhesion strength of Ni/a–Si multilayer films created by chemical vapor deposition (CVD). The LS technique enables the non-contact measurement of the tensile interfacial strength with high precision when compared to conventional methods for characterizing adhesion. Interferometric measurement combined with finite element analysis shows that the Ni/a–Si interface, created via the CVD of a-Si on Ni surfaces can withstand ≈46–72 MPa in tension before failure initiation. To ensure successful and precise characterization of interfacial adhesion strength using LS, we further develop a design criterion for multi-layer samples by analyzing the thin-film mechanics. Our study provides insights into the strength of the Ni/a–Si interface that governs the performance and durability of high-energy-density anodes and offers design guidelines for improving thin-film electrode integrity.

The increasing use of renewable energy sources has led to a pressing need for high-energy-density battery technologies. Lithium-ion (Li-ion) batteries have become the most widely used power source for portable electronic devices, electric vehicles (EVs), and stationary energy storage systems. However, it is widely acknowledged that current Li-ion technology will not meet future energy storage needs in terms of energy density, performance, durability, and longevity.1,2

The energy density of Li-ion batteries is primarily determined by the anode materials utilized. Anodes made of amorphous silicon (a-Si) increase the specific capacity by an order of magnitude compared to conventional carbon-based anodes, achieving a specific capacity of up to 4200 mA h g−1.3 A common feature in many a-Si anodes4–7 is the use of a-Si as the active material and a metal such as nickel (Ni) as the current collector. This configuration makes the Ni/a–Si interface a crucial component of the overall battery design. Failure at this interface, induced by the significant volumetric expansion of a-Si during charge–discharge cycling,3,8 can result in the loss of contact between a-Si and Ni and, thus, the degradation of battery capacity and performance.9 

Despite the crucial role of the Ni/a–Si interface, little work has been done in the battery community to study Ni/a–Si adhesion strength. Although a number of conventional adhesion test methods10 have been used to characterize the interfacial strength between the active materials and current collector, including peeling,11,12 pulling,13,14 bending,15,16 and cutting,17 and among others,18–21 these methods have significant limitations. The data interpretation is complicated by poorly defined stress states during the test, plastic deformation, unwanted damage of the film under investigation, or complicated sample preparation, which leads to inconsistency or inaccuracy in the measured adhesion strength.22 In contrast, laser spallation (LS)23–30 is a non-contact testing method that alleviates the intrinsic disadvantages of the aforementioned methods, by providing repeatable control over the stress state at the interface, access to high strain rates (∼107 s−1) with minimal inelastic deformation processes,29 for a range of film thicknesses.26 Due to these advantages, LS has been used on a wide range of film thicknesses, from nanometers to micrometers,25 for bimaterial systems such as ceramic/ceramic,31 metal/metal,32 metal/ceramic,25 and ceramic/polymer.33 

Here, we adapt LS induced delamination to make the first measurement of thin-film Ni/a–Si interfacial adhesion strength. The a-Si film is deposited via chemical vapor deposition (CVD) on an e-beam deposited Ni film to form the interface. By controlling the laser pulse fluence in combination with finite element analysis (FEA) simulations, the tensile adhesion strength of the Ni/a–Si interface is obtained. Additional experimental measurements further reveal design guidelines for the multilayer samples. The tensile LS test performed here provides a conservative baseline in system level design and provides an efficient and accurate method to simulate structured Ni/a–Si anodes.

The optical setup used for LS experiments is shown in Fig. 1.2 The laser used to induce stress waves was an Nd: YAG (New Wave Tempest 10 Hz) Q-switched pulsed laser with a wavelength of 1064 nm, a pulse width of 5 ns, and a nominal beam diameter of 5 mm. The laser pulse was focused through a 150 mm focal length lens (CVI Laser, BICX-50.8–153.4-C-1064) to a 2 mm-diameter spot on the sample. An attenuator was coupled to the Nd: YAG laser to tune the energy output in the range of 0–190 mJ, corresponding to a fluence of 0–55 mJ/mm2 as the attenuation factor decreases from 1000 to 0 (Fig. S1 in the supplementary material). The sample was held in a custom holder and was translatable on all three principal axes by micrometer screws. Prior to testing, the laser output power was calibrated using a Gentec power meter (QE25LP-H-MB). The Michaelson interferometer consisted of a 532 nm mode locked laser (Laser Quantum, Torus 532) that was first collimated and then focused through a 200 mm lens to bring the beam to a sharp point on the sample. After the focusing lens, the beam was passed through a non-polarizing beam splitting cube and split into two perpendicular beams. The first beam was directed toward the stationary reference mirror and the second beam toward the front face of the sample. The interferometric beam was carefully aligned to be colinear with the pulsed laser to ensure strong reading and accurate measurements. The high-speed photodetector used was an Electro-Optics Technology ET-2030. The voltage readings from the photodetector were collected using a LeCroy WaveRunner 640Zi oscilloscope with a sampling rate of 40 GHz. A built-in smoothing function was used to automatically smooth data in the oscilloscope. The smoothing function reduced noise but did not affect fringe maxima or periodicity and, thus, did not impede the accuracy of the test results.2 

FIG. 1.

Experimental setup used for laser spallation (LS) adhesion tests. (a) Schematic and (b) photograph of the LS system, consisting of an Nd: YAG laser coupled to an attenuator, a diagnosis laser with a Michelson interferometer, a photodetector coupled to an oscilloscope, and the test samples. The optical paths of the Nd: YAG and diagnosis laser are indicated by red and green dotted lines, respectively. The schematic in (a) is not to scale.

FIG. 1.

Experimental setup used for laser spallation (LS) adhesion tests. (a) Schematic and (b) photograph of the LS system, consisting of an Nd: YAG laser coupled to an attenuator, a diagnosis laser with a Michelson interferometer, a photodetector coupled to an oscilloscope, and the test samples. The optical paths of the Nd: YAG and diagnosis laser are indicated by red and green dotted lines, respectively. The schematic in (a) is not to scale.

Close modal

To enable the interfacial adhesion strength measurement, we designed and fabricated multi-layered samples for the LS test as shown in Fig. 2. The samples consist of a 1.6 mm-thick and 25.4 mm-diameter fused silica substrate (GM Associates, 7500–01), an energy-absorbing layer and a confining layer on the backside of the fused silica, a Ni layer, and an a-Si layer on the frontside [Fig. 2(a)]. Fused silica was used as the substrate due to its non-linear stress–strain relationship that shapes a Gaussian pulse into a wave with a linear ramp and large substrate compressive stress followed by a very sharp fall time.34,35 At 1.6 mm thickness, the fused silica substrate (GM Associates, 7500-01) generates a compressive stress with limited geometric attenuation while maintaining a planar one-dimensional (1D) wave propagation.25,36 A 400 nm-thick Al layer was deposited as the energy-absorbing layer via e-beam evaporation (Temescal FC-2000). The Al layer is much thicker than the critical penetration depth (∼10 nm) of the laser, allowing for the laser energy to be completely absorbed within the Al layer.25 Waterglass (sodium silicate, Fisher Scientific SS338-1) solution (1:1 by weight) was spin-coated (3000 rpm for 180 s) on the Al absorbing layer to form a 7 μm-thick solidified layer as a confining layer (thickness measured by stylus profilometry). On the front side, a 5 nm-thick chromium (Cr) adhesion-enhancing intermediate layer followed by a 50 nm-thick Ni layer was deposited via e-beam evaporation (Temescal FC-2000). The deposition of Ni on Cr was performed after the sample was naturally cooled down in the evaporator. The thickness of the Ni layer (50 nm) is close to the Ni thicknesses in a scaffold of a well-designed Si anode4 and is beyond the cut-off distance of molecular interactions (<10 nm) to represent an infinite body.37 The Ni layer is thin enough to reduce the substrate/Ni interfacial stress and allows for varying thicknesses of a-Si. Last, the a-Si layer with a thickness of 125–146 nm was deposited via static chemical vapor deposition (CVD) using a customized setup (Fig. S2 in the supplementary material).38 Air plasma cleaning (PDC001-HP, Harrick Plasma, medium power, 10–20 min) of the substrate was performed immediately before thin-film deposition to remove adventitious contamination (e.g., adsorbed volatile organic compounds or VOCs).39,40 The same plasma cleaning procedures were conducted whenever the surfaces were exposed to the atmosphere for 10 min or more, to minimize the effects of VOCs. During e-beam coating, a relatively low deposition rate (<0.15 nm/s) was adopted to limit thermal and growth stresses during the deposition of the thin films. In addition to the test samples, calibration samples were also fabricated following the same procedure, except for the absence of the a-Si layer on the front side. The exposed Ni layer acts as the reflective layer to enable reflection and interference of the diagnosis laser.

FIG. 2.

Design of the thin-film interfacial adhesion test samples. (a) Exploded view and (b) cross-sectional schematic of the multi-layer test sample consisting of water glass (WG) as the confining layer, Al as the absorbing layer, fused silica as the substrate, Cr as the seed layer, and Ni and a-Si as the materials of interest. The deposition/coating sequence is indicated by numbers in (a). In (b), the pulse beam from the Nd: YAG laser is cast on the absorbing layer (Al) through the confining layer (WG), generating compressive stress within the fused silica substrate that propagates toward the Ni/a–Si interface of interest. The calibration samples have a similar surface configuration to the test samples, except for the absence of the a-Si layer on the front side. Figures are not drawn to scale.

FIG. 2.

Design of the thin-film interfacial adhesion test samples. (a) Exploded view and (b) cross-sectional schematic of the multi-layer test sample consisting of water glass (WG) as the confining layer, Al as the absorbing layer, fused silica as the substrate, Cr as the seed layer, and Ni and a-Si as the materials of interest. The deposition/coating sequence is indicated by numbers in (a). In (b), the pulse beam from the Nd: YAG laser is cast on the absorbing layer (Al) through the confining layer (WG), generating compressive stress within the fused silica substrate that propagates toward the Ni/a–Si interface of interest. The calibration samples have a similar surface configuration to the test samples, except for the absence of the a-Si layer on the front side. Figures are not drawn to scale.

Close modal

Laser spallation tests were performed by directing laser pulses of varying fluences (or extent of attenuation) to the backside of the as-fabricated samples. Upon laser ablation of the absorbing layer, the expansion was confined by the water glass (WG) to generate a compressive stress wave propagating through the fused silica substrate toward the Ni/a–Si interface [Fig. 2(b)]. The laser fluence was increased by tuning the attenuation factor (AT, ranging from 1000 to 0) to initiate a-Si film spallation. A large attenuation factor represents a lower laser energy fluence. After each laser shot, the sample was translated by 3 mm to align a new location for laser pulses. The 3 mm spacing was large enough to ensure planar 1D wave propagation36 for mechanics analysis. As shown in Fig. 3, spallation was first observed at a laser fluence of ψ = 15.87 mJ/mm2 (or attenuation factor AT = 850), as confirmed by the optical and digital microscope. A lower laser fluence (e.g., ψ = 11.96 mJ/mm2, or AT = 900) was not able to induce a-Si film failure, while larger scale delamination was observed at higher fluences (e.g., ψ = 19.52 mJ/mm2 or AT = 800). Under the digital microscope (Keyence VHX-5000), the a-Si surface appears green while the Ni surface looks pink, confirming the delamination of the upmost a-Si from the underlying Ni surface. To ensure the repeatability of the measurement, a minimum of three spallation tests were conducted at each fluence to obtain the critical laser fluence above which the a-Si film delaminated.

FIG. 3.

Optical microscope images of the interfacial failure from the Ni/a–Si interface for the test samples after laser spallation tests at varying laser attenuation. The critical attenuation (or laser fluence) at which the a-Si layer delaminates from Ni was determined to be AT = 850 (ψ = 15.87 mJ/mm2), and the high-magnification digital microscopy captured the initiation of a-Si film (green) spallation from the Ni film (white). The blue-shaded region highlights the contrast in appearance between Ni and a-Si surfaces under the optical microscope. See Fig. S1 in the supplementary material for the laser fluences as a function of attenuation factor. See Fig. 2 for the configuration of the test samples.

FIG. 3.

Optical microscope images of the interfacial failure from the Ni/a–Si interface for the test samples after laser spallation tests at varying laser attenuation. The critical attenuation (or laser fluence) at which the a-Si layer delaminates from Ni was determined to be AT = 850 (ψ = 15.87 mJ/mm2), and the high-magnification digital microscopy captured the initiation of a-Si film (green) spallation from the Ni film (white). The blue-shaded region highlights the contrast in appearance between Ni and a-Si surfaces under the optical microscope. See Fig. S1 in the supplementary material for the laser fluences as a function of attenuation factor. See Fig. 2 for the configuration of the test samples.

Close modal
The calibration samples were then tested to obtain the fringe patterns for substrate stress calculations via Eqs. (1)–(3).24,26 First, the fringe count n ( t ) at time t is determined by the measured fringe intensity V ( t ) from interference theory,
(1)
where V max and V min are the maximum and minimum fringe values measured by the photodetector, respectively, and φ is the phase angle with respect to Michelson interferometry and is taken to be 0. Here, n ( t ) is determined by the optical path difference and is used to calculate the free surface displacements of the reflective film via the following equation:
(2)
The substrate stress σ sub ( t ) can be calculated using 1D stress wave propagation theory41 and is proportional to the velocity of the free surface (or derivative of u ( t )),
(3)
where ρ sub and c are the density and longitudinal wave speed of the substrate, respectively.

As shown in Fig. 4, a lower attenuation factor (or a higher laser fluence) results in a faster-oscillating fringe [Fig. 4(a)], indicating a larger displacement of the reflective film [Fig. 4(b)] and a larger maximum compressive stress within the substrate [Fig. 4(c)]. Consistent with previously reported stress wave profiles within fused silica when using a Gaussian laser pulse,25,30,34 the substrate stress shows a linear increase in the magnitude followed by a fast decompression, with the maximum substrate stress reaching −1.1 GPa for ψ = 19.52 mJ/mm2 (AT = 800) in Fig. 4(c). At all laser fluences tested, no delamination of the reflective Ni layer was observed. Note that the negative sign denotes compressive stress.

FIG. 4.

Laser spallation test results for the calibration sample. (a) Voltage fringe pattern measured by the photodetector at different laser fluences or attenuation (ψ = 19.52, 15.87, and 11.96 mJ/mm2, corresponding to AT = 800, 850, and 900, respectively). The fringes are used to analytically calculate the (b) surface displacement and (c) substrate stress as functions of time ( t ). The turning points, after which the film velocity changes the direction, are marked by arrows in (a). The peak substrate stress and interfacial stress occur near the turning point; thus, displacement and substrate stress after the turning point are not shown in (b) and (c). The calibration samples are the same as the surface configuration of the test samples (Fig. 2) but without a-Si layer on top of the Ni layer (50 nm in thickness). To prevent the overlapping of the displacement curves in (b), distinct origins were assigned to each of them.

FIG. 4.

Laser spallation test results for the calibration sample. (a) Voltage fringe pattern measured by the photodetector at different laser fluences or attenuation (ψ = 19.52, 15.87, and 11.96 mJ/mm2, corresponding to AT = 800, 850, and 900, respectively). The fringes are used to analytically calculate the (b) surface displacement and (c) substrate stress as functions of time ( t ). The turning points, after which the film velocity changes the direction, are marked by arrows in (a). The peak substrate stress and interfacial stress occur near the turning point; thus, displacement and substrate stress after the turning point are not shown in (b) and (c). The calibration samples are the same as the surface configuration of the test samples (Fig. 2) but without a-Si layer on top of the Ni layer (50 nm in thickness). To prevent the overlapping of the displacement curves in (b), distinct origins were assigned to each of them.

Close modal

The interfacial adhesion strength is determined using finite element analysis (FEA) and the stress profiles measured for the calibration samples. Specifically, a one-dimensional FEA was developed to study the wave propagation in the multilayer thin-film specimens and analyze the stresses developed at each interface. The non-linear fused silica substrate was not explicitly included in the analysis. Instead, we imposed the substrate stress history measured directly from calibration experiments at the same fluence, i.e., the substrate stress profile [Eq. (3)] obtained from the calibration samples at the critical laser fluence (ψ= 15.87 mJ/mm2 or AT = 850) in Fig. 4(c), to calculate the stress at the Ni/a–Si interface, σ Ni / Si ( t ). The top and bottom surfaces of the multilayer film stack were assumed in plane strain with traction free boundary conditions. The specimen geometry was meshed using the elements of size Δ h / 30, where Δ h is the thinnest layer dimension. This element size was chosen based on a convergence study. An explicit direct integration scheme with a forward difference time step was applied for transient analysis. The simulations were performed using a time step Δ t / 5, where Δ t is the minimum of wave travel time in the elements of considered layers. Details on FEA can be found in previous studies.42 The peak value of the simulated σ Ni / Si ( t ) represents the interfacial adhesions strength σ Ni / Si . To check the accuracy of the FEA, we compared the interferometric measurements of the film surface displacements to the FEA-calculated displacements. The simulated peak displacements averaged less than 0.5% deviation for all shots, validating the use of continuum 1D wave mechanics in our simulations (Fig. S3 in the supplementary material).

Alternatively, σ Ni / Si ( t ) can also be determined from the planar 1D wave propagation mechanics,25 
(4)
where 2 u / t 2 is the acceleration of the film and can be numerically determined by the second derivative of the measured displacements u ( t ). However, the experimentally determined second derivative is noisy and unreliable. FEA allows for the calculation of reliable interface stress values for any laser fluence given the calibration substrate stress. A further benefit of incorporating FEA is the ability to predict the stresses generated for varying combinations of materials, multilayers, and film thicknesses prior to testing, which facilitates the design of the multilayer samples as will be demonstrated in the subsequent section. We further note that the calibration samples allow for a higher signal-to-noise ratio of the fringe intensity due to better reflectivity of the calibration samples, while the Ni/a–Si test samples cannot produce accurate data on shots where the interface and reflective surface fail. Therefore, FEA based on calibration sample compressive stress input was used to determine interfacial stress in the present study.

The thickness measurement of the a-Si film is critical for accurate calculation of σ Ni / Si ( t ). Figure 5(a) shows laser scanning microscopy (Keyence VK-X1000) and a cross-sectional profile of the spallation spot obtained at ψ= 46.18 mJ/mm2 (AT = 400, inset in Fig. 3). Surface-averaging measurements indicate an a-Si thickness of Δ h Si = 125 nm (Fig. S4 in the supplementary material). Although the laser scanning microscope has a relatively low height resolution (20 nm), it provides a large field of view for baseline benchmarking. Atomic force microscopy (AFM, Asylum Research Cypher S) with a higher vertical resolution (∼ 0.1 nm) confirms our measurement consistency [ Δ h Si = 142 nm, Fig. 5(b)].

FIG. 5.

Interfacial adhesion strength analysis. (a) Digital microscopy showing spallation of the a-Si film, corresponding to the blue-shaded region in Fig. 3 at ψ= 46.18 mJ/mm2 (AT = 400). (b) Atomic force microscopy (AFM) of the spallation spot. The bottom panels show the cross-sectional profile, i.e., the height (Z) along the dotted line (X), from which the thickness (ΔhSi) of the a-Si film is determined. See Fig. S3 in the supplementary material for a more detailed measurement of the a-Si thickness using an area-averaging scanning measurement. (c) Interfacial stress obtained via FEA using the critical substrate stress at ψ= 15.87 mJ/mm2 (AT = 850) in Fig. 4(c) and a-Si thickness ΔhSi as the input. The Ni/a–Si interfacial adhesion strength was determined to be σNi/Si=68.0MPa. (d) Determination of the Ni/a–Si interfacial adhesion strength incorporating the uncertainty of the a-Si thickness (ΔhSi<ΔhSi<ΔhSi+) and critical laser fluences (ψ= 11.96 and 15.87 mJ/mm2, or AT = 900 and 850). The Ni/a–Si interfacial adhesion strength is bounded within σNi/Si=45.7MPa,σNi/Si+=72.1MPa, indicated by the red dots). See Fig. S3 in the supplementary material for more details on data analysis.

FIG. 5.

Interfacial adhesion strength analysis. (a) Digital microscopy showing spallation of the a-Si film, corresponding to the blue-shaded region in Fig. 3 at ψ= 46.18 mJ/mm2 (AT = 400). (b) Atomic force microscopy (AFM) of the spallation spot. The bottom panels show the cross-sectional profile, i.e., the height (Z) along the dotted line (X), from which the thickness (ΔhSi) of the a-Si film is determined. See Fig. S3 in the supplementary material for a more detailed measurement of the a-Si thickness using an area-averaging scanning measurement. (c) Interfacial stress obtained via FEA using the critical substrate stress at ψ= 15.87 mJ/mm2 (AT = 850) in Fig. 4(c) and a-Si thickness ΔhSi as the input. The Ni/a–Si interfacial adhesion strength was determined to be σNi/Si=68.0MPa. (d) Determination of the Ni/a–Si interfacial adhesion strength incorporating the uncertainty of the a-Si thickness (ΔhSi<ΔhSi<ΔhSi+) and critical laser fluences (ψ= 11.96 and 15.87 mJ/mm2, or AT = 900 and 850). The Ni/a–Si interfacial adhesion strength is bounded within σNi/Si=45.7MPa,σNi/Si+=72.1MPa, indicated by the red dots). See Fig. S3 in the supplementary material for more details on data analysis.

Close modal

Using the known a-Si thickness, the interfacial stress at the critical laser fluence (ψ= 15.87 mJ/mm2 or AT = 850) was calculated to be σ Ni / Si = 68 MPa [Fig. 5(c)]. To account for the uncertainty of interfacial adhesion strength, we incorporated the uncertainty of thin-film thickness and critical substrate stress into the FEA simulation by considering the lower and upper boundaries of a-Si thicknesses and substrate stresses. Given that the thicknesses of Cr and Ni layers do not directly contribute to the Ni/a–Si interfacial stress [Eq. (4)], we only considered the lower and upper boundaries of the a-Si layer ( Δ h Si < Δ h Si < Δ h Si + ). To facilitate the analysis, Δ h Si and Δ h Si + are obtained from thickness measurements by laser scanning microscopy ( Δ h Si = 125 nm ) and AFM ( Δ h Si + = 146 mm ) . The boundaries of the critical interfacial stress ( σ Ni / Si < σ Ni / Si < σ Ni / Si + ) are calculated from the FEA using the substrate stress profiles at critical laser fluences near spallation initiation (ψ= 11.96 and 15.87 mJ/mm2, corresponding to AT = 900 and 850, respectively). Figure 5(d) shows the Ni/a–Si interfacial stress as a function of a-Si thickness for varying laser fluences. It is worth noting that the FEA-calculated interfacial stress is proportional to the a-Si thickness for a given substrate stress, consistent with the theoretical analysis [Eq. (4)]. The lower boundary of the Ni/a–Si interfacial adhesion strength ( σ Ni / Si ) is obtained at a lower substrate stress (ψ= 11.96 mJ/mm2 or AT = 900) and a thinner a-Si thickness Δ h Si = 125 nm , while the upper boundary exists at a higher substrate stress (ψ= 15.87 mJ/mm2 or AT = 850) and a larger a-Si thickness ( Δ h Si + = 146 mm ), i.e., σ Ni / Si = σ Ni / Si (AT = 900, Δ h Si ) and σ Ni / Si + = σ Ni / Si (AT = 850, Δ h Si +). From Fig. 5(d), we obtain σ Ni / Si [ 45.7 MPa , 72.1 MPa ].

The key to successful measurement of interfacial adhesion strength is the design of the multi-layer test sample. The properties and constitutive relationship of the substrate play a critical role in the development of a stress wave and must be well characterized. In contrast to fused silica substrates, metal plates (Al or Cu) show slower fall and rise in the compressive stress profile that leads to lower peak compressive stress and weaker interfacial stress (Fig. S5 in the supplementary material), making interfacial failure difficult. The use of Si wafers sees damage due to cleavage under the action of the tensile wave at high laser energy fluences.25 

In addition to the rational selection of the substrate, the orientation of the thin films needs to be designed to ensure spallation at the interfaces of interest.2 In the current surface configuration, two heterogeneous interfaces exist: the substrate/Ni and Ni/a–Si interfaces. The delamination of the Ni/a–Si interface needs to be initiated prior to the failure of the substrate/Ni interface, or σ sub / Ni > σ Ni / Si , where σ sub / Ni and σ Ni / Si are the maximum interfacial stresses at the substrate/Ni and Ni/a–Si interfaces, respectively. The intermediate Cr layer enhances the substrate/Ni adhesion strength from <100 MPa to σ sub / Ni 233 MPa (Fig. S6 in the supplementary material), thus allowing for a similar interfacial adhesion strength of Ni/a–Si to be measured.

The Ni and a-Si thicknesses can be estimated using experimentally obtained σ sub / Ni and an empirical value for σ ~ Ni / Si . Assuming planar 1D wave propagation, the interface stress is directly proportional to the film density, thickness, and acceleration [Eq. (4)], i.e., σ Ni / Si = ρ Si a Δ h Si, and σ sub / Ni = ( ρ Ni Δ h Ni + ρ Si Δ h Si ) a, where a = 2 u / t 2 is the acceleration of the film and can be determined by the stress profile within the substrate. Here, ρ Si and ρ Ni are the densities of a-Si and Ni, respectively, and Δ h Ni is the thickness of the Ni film. For a given Δ h Ni, the range of Δ h Si within which the aforementioned delamination sequence criteria are met can be solved from Eq. (4) by equating σ Ni / Si = σ ~ Ni / Si and σ sub / Ni = σ sub / Ni ,
(5)

As plotted in Fig. 6, σ sub / Ni and σ Ni / Si are the linear functions of Δ h Si, with the same slope [ ρ Si a in Eq. (5)] determined by the stress profile. For Δ h Ni = 50 nm and ψ= 15.87 mJ/mm2 (AT = 850), we obtained Δ h Si ranging from Δ h Si = 90 nm to Δ h Si + = 340 nm, corresponding to known values of σ ~ Ni / Si = 50 MPa and σ sub / Ni = 233 MPa (Fig. 6). Similar calculation procedures can be used to optimize the design a multi-layer sample for laser spallation tests. Equation (5) reveals that a thick Ni layer ( Δ h Ni ) reduces the upper boundary of a-Si thickness ( Δ h Si + ), and in the limiting cases where Δ h Si + drops below Δ h Si , substrate/Ni interface failure becomes a critical issue preventing the precise characterization of Ni/a–Si interfacial adhesion strength.

FIG. 6.

Maximum stress at the substrate/Ni ( σ sub / Ni ) and Ni/a–Si ( σ Ni / Si ) interfaces as a function of a-Si thickness. The slope is determined by the substrate stress profile for ψ= 15.87 mJ/mm2 (AT = 850). The lower ( Δ h Si ) and upper ( Δ h Si + ) boundaries of a-Si thickness were determined by the guess value of Ni/a–Si interfacial adhesion strength σ ~ Ni / Si = 50 MPa and experimentally obtained substrate/Ni interfacial adhesion strength σ sub / Ni = 233 MPa. Red dots mark the intersection of interfacial adhesion strengths (horizontal dotted lines) and the maximum interfacial stress (solid lines). The shaded region indicates where the Ni/a–Si delaminates and the substrate/Ni remains intact.

FIG. 6.

Maximum stress at the substrate/Ni ( σ sub / Ni ) and Ni/a–Si ( σ Ni / Si ) interfaces as a function of a-Si thickness. The slope is determined by the substrate stress profile for ψ= 15.87 mJ/mm2 (AT = 850). The lower ( Δ h Si ) and upper ( Δ h Si + ) boundaries of a-Si thickness were determined by the guess value of Ni/a–Si interfacial adhesion strength σ ~ Ni / Si = 50 MPa and experimentally obtained substrate/Ni interfacial adhesion strength σ sub / Ni = 233 MPa. Red dots mark the intersection of interfacial adhesion strengths (horizontal dotted lines) and the maximum interfacial stress (solid lines). The shaded region indicates where the Ni/a–Si delaminates and the substrate/Ni remains intact.

Close modal

The measured Ni/a–Si interfacial adhesion strength ( σ Ni / Si [ 45.7 MPa , 72.1 MPa ] ) is similar to Al/Si (∼60 MPa),25 but smaller than that of polyimide/Si or Si3N4 (>140 MPa),42 epoxy/fused silica (>120 MPa),43 and diamond/polycrystalline alumina (>140 MPa)44 interfaces, as well as the Ni/fused silica interfaces with an intermediate Cr layer reported here ( σ sub / Ni > 200 MPa ). The relatively weak adhesion strength may result from the fabrication processes of the Ni and a-Si films. Future work is needed to provide a further understanding of the Ni/a–Si system by investigating the effects of intermediate layers, surface roughness, annealing, residual stresses, impurities, and native oxides, all of which have the potential to change the interface strength.45,46 Furthermore, with Ni underneath the Si layer, the current surface configuration enables electrodeposition of Si to Ni in addition to CVD presented here, allowing one to explore the role of Si deposition methodology in interfacial strength. The measured Ni/a–Si interfacial strength, which has not been reported in the literature, could be employed for failure modeling47 and to investigate the changes in electrode configuration19 in future studies.

Laser spallation (LS) coupled with finite element analysis (FEA) was used to probe the interfacial adhesion strength of the nickel and amorphous silicon (Ni/a–Si) interface. Multilayer samples were designed to enable the LS test by enabling high tensile interfacial stress and promoting delamination of the interface of interest. For a-Si fabricated via CVD, the Ni/a–Si adhesion strength was measured to be ≈46–72 MPa. Furthermore, design guidelines for multi-layer samples for LS tests were developed based on a thin-film mechanics analysis. Our results provide insight into the strength of the Ni/a–Si interface and serve as an important metric for the material design of high-energy-density anodes. The heterogeneous adhesion strength characterization procedures presented here also provide valuable methods for the design and understanding of thin films and coatings for energy,4 thermal,48–50 optical,51 chemical,52 and microelectromechanical applications.16,53

See the supplementary material for information about laser energy fluence as a function of attenuation factor (Fig. S1), CVD setup and procedures for a-Si deposition (Fig. S2), analysis of interfacial stress (Fig. S3), surface-averaging measurement of the a-Si thickness (Fig. S4), compressive stress profile of Al, Cu, and Si substrates (Fig. S5), and measurement of the substrate/Ni adhesion strength (Fig. S6).

N.S., P.B., X.Y. and J.M.D. acknowledge the funding support by the U.S. Army CERL under Grant No. W9132T-19-2-0008. X.Y. and N.M. acknowledge the funding support by the Office of Naval Research (ONR) under Grant No. N00014-16-1-2625. N.M. also acknowledges the funding support from the International Institute for Carbon Neutral Energy Research (No. WPI-I2CNER), sponsored by the Japanese Ministry of Education, Culture, Sports, Science and Technology. X.Y. also acknowledges support from the Innovative research group project of National Natural Science Foundation of China (No. 52021004) during writing of the manuscript. This work was carried out, in part, at the Materials Research Laboratory Central Research Facilities, University of Illinois.

The authors have no conflicts to disclose.

X.Y. and J.M.D. contributed equally to this work.

Xiao Yan: Data curation (equal); Formal analysis (equal); Investigation (equal); Writing – original draft (lead); Writing – review & editing (equal). Jacob M. Diamond: Data curation (equal); Formal analysis (equal); Investigation (equal); Writing – original draft (equal); Writing – review & editing (equal). Nathan J. Fritz: Data curation (equal); Formal analysis (equal); Writing – original draft (supporting). Satoshi Matsuo: Data curation (supporting); Writing – original draft (supporting). Kazi F. Rabbi: Data curation (supporting); Writing – original draft (supporting). Ishrat Zarin: Data curation (supporting); Writing – original draft (supporting). Nenad Miljkovic: Project administration (equal); Supervision (equal); Writing – review & editing (equal). Paul V. Braun: Funding acquisition (equal); Project administration (equal); Supervision (equal); Writing – review & editing (equal). Nancy R. Sottos: Conceptualization (lead); Funding acquisition (lead); Project administration (lead); Writing – original draft (equal); Writing – review & editing (equal).

The data that support the findings of this study are available within the article and its supplementary material.

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Supplementary Material