Kai Zhanga,
Yinan Hea,
Junwu Zhoua,
Xinyang Wanga,
Yong Li*b and
Fuqian Yang*c
aSchool of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092, China
bSchool of Intelligent Manufacturing and Control Engineering, Shanghai Polytechnic University, Shanghai 201209, China. E-mail: yongli@sspu.edu.cn
cMaterials Program, Department of Chemical and Materials Engineering, University of Kentucky, Lexington, Kentucky 40506, USA. E-mail: fuqian.yang@uky.edu
First published on 20th September 2024
Controlling the stress state of electrodes during electrochemical cycling can have a positive effect on the cycling performance of lithium-ion battery. In this work, we study the cycling performance of silicon-based lithium-ion half cells under the action of pressure in a range of 0.1 to 0.4 MPa. The cycling performance of the silicon-based lithium-ion half cells increases first with increasing the pressure to 0.2 MPa and then decreases with further increasing the pressure. The analysis of the surface morphologies of cycled electrodes reveals that applying a pressure of 0.2 MPa leads to the formation of fine electrode surface with the least surface cracks after the silicon-based lithium-ion half cells are cycled for 50 times, which supports the dependence of the cycling performance of the lithium-ion half cells on the pressure. The numerical results from the single particle model reveal that applying pressure can tune the stress state in a single electrode particle and reduce the tensile stress. However, the numerical results from the two-particle model point to that applying pressure can introduce tensile stress in the electrode particles due to contact deformation. Suitable pressure applied onto a lithium-ion battery is needed in order to improve the cycling performance of the lithium-ion battery without causing detrimental effects.
One of effective ways to control the internal deformation and stress in silicon is to optimize the silicon electrode structures through structural engineering,11 such as producing specific nanostructures like carbon-coated core–shell,12 yolk–shell13 structures, or porous structures,14 fabricating advanced binders15 or Si/C composite electrodes,16 incorporating self-healing polymers and advanced prelithiation techniques. These methods improve coulombic efficiency and reduce capacity loss, thereby enhancing the durability and performance of silicon anodes.
Progress has been made in achieving favorable outcomes for silicon electrode structures, while the technical thresholds and fabrication costs have limited their commercialization. Another approach is to use specific electrochemical or mechanical loadings, e.g., charging protocols and external stress to suppress the internal deformation and stress. Such an approach has also attracted much attention due to its feasibility.
Appling a partial lithiation charging protocol, Li et al.17 successfully controlled the volumetric swelling of silicon electrodes during cycling and enhanced the capacity retention of LIBs. Based on the evolution of stress in a silicon particle, Yang and co-workers proposed two stress-control charging protocols, i.e., the partial delithiation method18 and the multi-stage currents method.19 Their results highlight the effectiveness of the control of internal stress in improving the cyclic performance of Si-based LIBs. Cui et al.20 investigated the effects of external pressure on the electrochemical performance of Si electrodes. They suggested that applying pressure of ∼0.6 MPa likely can reduce internal resistance and improve the capacity of the Si-based LIBs. Zhang et al.21 examined the performance of lithium-ion pouch cells with silicon-composite electrodes under pressure. The experimental results showed that the capacity of the lithium-ion pouch cells underwent slow decline followed by rapid drop under constant pressure. They observed that this issue can be mitigated by applying multi-stage pressures. Li et al.22 reviewed the effects of both external pressure and internal stress on the performance and lifespan of LIBs. They suggested that the actual effects of external pressure on the performance of LIBs depend on specific type of LIBs. In general, it is challenging to determine the optimal pressure due to the complex nature of LIBs and their responses to external mechanical loadings.
Realizing the possible effects of mechanical loading on the performance of LIBS, we investigated the cycling performance of silicon-based LIBs under the action of pressure. An in situ loading system was constructed and allowed for the application of pressure to the silicon-based LIBs during electrochemical cycling. The optimal pressure was determined at which the performance of silicon-based LIBs was improved. Methods of applying distinct pressures during charging and discharging were proposed to control the stress states of silicon particles during electrochemical cycling and to improve the capacity retention.
Electrochemical cycling of the prepared CR2032 coin half cells on a battery testing system (CT-4008Tn, Neware). The cycling tests were conducted at a C-rate of 0.2 at room temperature. The voltage window was 10–1000 mV. Prior to the tests, 5 formation cycles were performed at a C-rate of 0.1C to establish a stable SEI. The battery testing system was placed in a loading system, which was used to apply compressive force, as shown in Fig. 2. The constant load mode was used during electrochemical cycling.
After electrochemical cycling for 50 cycles, the cycled CR2032 coin half cells were disassembled in the glove box. The silicon-based electrodes were cleaned with dimethyl carbonate (DMC, Tianci Material Technology Co.) to remove contaminants and naturally dried in a glovebox for 10 h. The surface morphologies of the working electrodes were imaged on a scanning electron microscope (SEM) (S-4800, Hitachi).
For the modeling schemes, see Appendix A.
Fig. 3a and b depicts the variation of the capacity retention with the cycle number under different pressures. For the same cycle number, the capacity retention increases first with increasing the of pressure, reaches maximum under the pressure of 0.2 MPa (Fig. 4a), and then decreases with increasing pressure (Fig. 4b). After the 50th cycle, the capacity retention is ∼70% under the pressure of 0.2 MPa more than ∼59% without pressure and ∼47% under the pressure of 0.4 MPa. Such a result suggests that the pressure of 0.2 MPa is likely the most suitable one applied onto the prepared silicon-based lithium-ion half cells, which does not cause detrimental effects to the lithium-ion half cells.
Fig. 3 Variation of the capacity retention with the cycle number under different pressures: (a) 0–0.2 MPa and (b) 0.2–0.4 MPa. |
Fig. 4 Variation of the capacity retention and coulombic efficiency with the cycle number for four different loading conditions. |
It is worth noting that changes in cycling performance resulting from external pressure can also be linked to the evolution of SEI layers under pressure. An increase in external pressure can promote the formation of a thin and dense SEI, enhancing the diffusivity and Young's modulus of the SEI.23 However, this can also lead to an increase in SEI structure delamination and a reduction in porosity.23 The synergistic effect of external pressure on the SEI results in a trend where the capacity retention of the battery initially increases and then decreases with the growth of external pressure, as shown in Fig. 3.
External pressure also influences the interactions among the components within the battery. Applying appropriate pressure can improve the effective contact between the battery electrode and the current collector, thereby reducing interfacial resistance and enhancing the conductivity and cycling stability. Additionally, proper pressure can strengthen the contact between the separator and electrode,24,25 reducing the overall internal resistance of the battery while maintaining a uniform distribution of the electrolyte within the porous electrode.26,27 This allows the electrolyte to fully permeate the porous structure, improving the transport efficiency of lithium ions and increasing the contact area between the active material and the electrolyte, thus enhancing the reaction efficiency of the active electrode. However, excessive pressure can damage the porous structure of the electrode material, reducing porosity, hindering lithium-ion transport, and potentially even causing the complete breakdown of the electrode structure. This explanation also aligns with the observations depicted in Fig. 3.
It has been reported that silicon electrodes can experience different stress states during lithiation and delithiation.28 This implies that applying different pressures during lithiation and delithiation stages likely introduces different stress states in the silicon particle during cycling. To investigate the effects of different stress states, two methods of applying pressures were used – the first one applied 0.2 MPa during lithiation and 0.3 MPa during delithiation (Method #1), and the second one applied 0.3 MPa during lithiation and 0.2 MPa during delithiation (Method #2).
Fig. 4 shows the variation of the capacity retention with the cycle number using the configurations of constant pressures of 0.2 and 0.3 MPa as well as the Method #1 and Method #2. It is evident that the silicon-based lithium-ion half cell with the configuration of Method #1 exhibited the best cycling performance for the first 10 cycles. After the first 10 cycles, the capacity retention of the lithium-ion half cells with the configuration of Method #1 decreases with increasing the cycle number and becomes comparable to the corresponding one for the lithium-ion half cells under 0.2 MPa pressure for the cycle number more than 30. The capacity retention of the lithium-ion half cells with the configuration of Method #2 experiences some fluctuations and eventually becomes slightly better than the corresponding one for the lithium-ion half cells under 0.3 MPa pressure, as evidenced by the higher capacity retention after the 50th cycle. In general, applying different pressures during lithiation and delithiation can slightly improve the cycling performance of the prepared silicon-based lithium-ion half cells. Note that there are nearly no differences in the coulombic efficiencies between the four different loading conditions.
Fig. 5 Surface morphologies of the silicon-based electrodes, which experienced 50 lithiation–delithiation cycles, under different mechanical loadings. |
The diffusion-induced stress generated during cycling causes cracks to form on the surface of the silicon electrode, gradually breaking them down into powder. When the applied pressure increases to 0.1 MPa, the number of cracks on the silicon electrode significantly decreases, as the pressure enhances the contact between active material particles, promoting particle agglomeration. At a pressure of 0.2 MPa, the volume changes and pulverization of the silicon electrode are noticeably reduced, which decreases the separation of fractured silicon particles from the main body of the electrode. Additionally, the electrical contact between the active particles and adjacent units, the conductive network, and the current collector is improved, further reducing self-isolation and conductivity loss in the active material. However, when the load increases to 0.3 MPa and 0.4 MPa, particle agglomeration becomes more pronounced, but surface cracks increase, particularly for the pressure of 0.4 MPa. This is primarily because the continuously increasing external load excessively compresses the electrode structure, accelerating the fracture of silicon particles under pressure, leading to structural breakdown. As a result, more electrolyte is consumed during cycling, causing uneven SEI growth, which weakens the electrochemical reaction and accelerates capacity fading.
Fig. 6 shows the variation of hoop stress at the surface of the spherical electrode with SOC during a lithiation–delithiation cycle under the action of different compressions of 0, 0.1, 0.2, 0.3, and 0.4 MPa. It is evident that applying pressure causes the decrease of the hoop stress at the tensile state and the increase of the hoop stress at the compressive state for the same SOC. It is known that the hoop stress plays an important role in the nucleation and growth of surface cracks of electrodes during electrochemical cycling. The decrease in the tensile hoop stress will hinder the nucleation and growth of surface cracks and improve the structural stability of electrodes. Applying pressure might likely improve the structural stability of electrodes.
Fig. 7 shows the variations of hoop stress and radial stress at the center of the spherical electrode with SOC during a lithiation–delithiation cycle under the action of different compressions of 0, 0.1, 0.2, 0.3, and 0.4 MPa. The pink region corresponds to the tensile state, and the cyan region corresponds to the compressive state. The variations of hoop stress and radial stress at the surface of the spherical electrode with SOC exhibit similar trend to the hoop stress at the surface of the spherical electrode. Such a result also supports that applying pressure might likely improve the structural stability of electrodes.
According to the results shown in Fig. 6 and 7, it might be generally concluded that applying pressure to a battery system can likely improve the structural stability of the battery during electrochemical cycling. However, excessive pressure can lead to compressive failure of electrodes, as shown in Fig. 5. The magnitude of pressure applied to a battery system needs to be carefully controlled in order to avoid or limit the pressure-induced structural failure of electrodes and achieve a positive effect to the cycling performance of the battery system.
It should be pointed out that the stress analysis of a single electrode particle under pressure cannot provide stress state of electrodes, which consist of electrode particles, binders, and carbon blocks. A composite model needs to be developed to provide further information on the stress state of electrodes.
To understand if applying different pressures during lithiation and delithiation has any impacts on the stress state of the spherical electrode, we analyzed the stress evolution in the spherical electrode with the schemes of Method #1 and Method #2 in applying pressure. Fig. 8 shows the variations of hoop stress at the surface and center of the spherical electrode with SOC during a lithiation–delithiation cycle with the schemes of Method #1 and Method #2 in applying pressure. The Method #1 reduces the stress range of the surface of the spherical electrode and magnify the stress range of the center of the spherical electrode. The opposite trend is observed for the Method #2. The experimental results given by Liu et al.29 and the analysis by Yang30 suggest that cracks are more prone to initiate on the surface of a silicon particle. The analysis by Zhang et al.31 reveals that the stress range is closely related to the damage of electrodes and the cycling performance of lithium-ion battery. It can be inferred that the Method #1 may be more effective in improving the cycling performance, as supported by the experimental results shown in Fig. 4. Note that the increase in the stress range at the electrode center under the scheme of the Method #1 might lead to more structural degradation at the electrode center than the scheme of the Method #2 if the nucleation of structural degradation occurs at the electrode center.
To examine the potential crack propagation of electrode particles under different pressure, we calculate the evolution of the J-integral at the crack tip. Fig. 9 shows the variation of J-integral at the crack tip with applying pressure for two different crack sizes and three different inclination angles. For the same inclination angle, the J-integral increases with increasing pressure, as expected. Applying appropriate pressure promotes close contact between particles, reducing contact resistance and thereby improving the cycling performance of LIBs. However, it does not lead to a significant increase in the J-integral. This explains why the cycling test results and surface morphology of the 0.2 MPa case outperform the others. Applying large pressure can cause the propagation of surface cracks. In particular, for pressures exceeding 0.2 MPa, there is a rapid increase in the J-integral, resulting in the degradation of silicon particles and ultimately leading to the capacity fade of the batteries. Under the action of the same pressure, the smaller the crack size, the larger the J-integral. This reveals the size dependence of the surface cracking. For the same crack size, the smaller the inclination angle, the larger the J-integral. This result is in accord with the contact-induced ring crack in a spherical particle.32,33
Fig. 9 Variations of J-integral at the crack tip with external pressure for two different crack sizes and three different inclination angles of (a) θ0 = 10°, (b) θ0 = 20° and (c) θ0 = 30°. |
From Fig. 9a, we note that there is a decrease in the increase rate of the J-integral with respect to applied pressure at p0 = ∼0.33 MPa for the crack with a0 = 10 nm and θ0 = 10°. This can be attributed to the fact that surface cracks under θ0 = 10° are located near the contact region. When the cracks are large, the contact status of the particles is greatly affected by the cracks, thus exerting a significant influence on the stress field at the crack tip and the J-integral. In more detail, the decrease in the increase rate of the J-integral is likely due to the dominance of viscoplastic flow, which consumes more mechanical work done by the applied stress. It should be pointed out that the close contact between electrode particles under pressure can reduce the contact resistance and thereby improve the cycling performance of LIBs.
The numerical results from the single particle model reveal that applying pressure can tune the stress state in a single electrode particle and reduce the tensile stress in the surface of the electrode particle. This can hinder the nucleation of surface cracking. However, the numerical results from the two-particle model point to that applying pressure can introduce tensile stress in the electrode particles due to contact deformation and the J-integral at the crack tip increases with increasing pressure. Applying large pressure can result in the propagation of surface cracks and lead to the capacity fading of lithium-ion battery. Thus, it requires suitable pressure to be applied onto a lithium-ion battery in order to improve the cycling performance of the lithium-ion battery without causing detrimental effects.
For the single particle model, we consider a spherical silicon particle with an initial radius of R0 in a reference coordinate system (R, Θ, Φ). The corresponding current coordinate system is (r, θ, φ). The cycling-induced deformation of the silicon particle is described by the deformation gradient tensor, F, as
F = FelFplFch, | (A.1) |
F = I + diag(∂uR/∂R, uR/R, uR/R), | (A.2) |
Fpl = diag(λpl, λpl−1/2, λpl−1/2), | (A.3) |
Fch = Λ1/3I, | (A.4) |
Fel = Λ−1/3diag〈(1 + ∂uR/∂R)λpl−1, (1 + μR/R)λpl−1/2, (1 + μR/R)λpl−1/2〉. | (A.5) |
The elastic strain tensor, i.e., the Green-Lagrange strain tensor, Eel, can be calculated as
Eel = diag(EelR, EelΘ, EelΦ) = [(Fel)TFel − I]/2, | (A.6) |
(A.7) |
E(C) = E0(1 − κC/Cmax), | (A.8) |
The first Piola–Kirchhoff stress tensor, P = diag(PKR, PKΘ, PKΦ), is calculated from P = ∂W/∂F as
(A.9) |
(A.10) |
The true stress tensor, σ = diag(σr, σθ, σφ), in the current configuration is obtained from the relation of σ = det(F)−1PFT. Without any body force, the mechanical equilibrium of the spherical particle is described as
(A.11) |
For the viscoplastic problem, we have the rate of the plastic deformation, Dpl, as
Dpl = Ḟpl(Fpl)−1 = pl/λpldiag(1, −1/2, −1/2). | (A.12) |
The rate of the plastic deformation can be calculated by a plastic flow potential, Gpl, as
Dpl = ∂Gpl/∂τ, | (A.13) |
(A.14) |
pl/λpl = sgn(σr − σθ)ḋ0(σeff/σY − 1)mH(σeff/σY − 1). | (A.15) |
The deformation of the pristine silicon particle has initial conditions as
uR(R,0) = 0,λpl(R,0) = 1. | (A.16) |
uR(0,t) = 0,PKR(R0,t) = p0. | (A.17) |
With the spherical-symmetrical characteristics of the problem, there is only non-zero radial flux for mass transport, which is calculated by the spatial gradient of the chemical potential, μ, as
(A.18) |
μ = μ0 + RgTlnc − Ω1σm + Ω2w, | (A.19) |
(A.20) |
The mass conservation in the spherical particle in the reference configuration yields
(A.21) |
The initial condition for the pristine unlithiated silicon is
C(R,0) = 0. | (A.22) |
To mimic the experimental conditions, we adopt galvanostatic operation in the modeling analysis and have the influx to the spherical particle as
(A.23) |
(A.24) |
Fig. 10 Two-particle model: (a) schematic of the axisymmetric model with geometric parameters, and (b) the mesh refinement near the crack tip. |
The compression of the two particles can cause the propagation of the pre-existing cracks, resulting in adverse effects on lithium-ion batteries, including the formation of new SEI and the capacity fading. To track the potential crack growth, we evaluate the variation of the J-integral around the crack tip with increasing external force. Note that the J-integral is not valid for the deformation with eigen strains, such as diffusion-induced strain. Here, we examine the fracture behavior of the spherical particles at the un-lithiated state. The rate-dependent viscoplastic behavior with power-law hardening was used, which is the same as the viscoplastic flow used in the single particle model of eqn (A.15). Note that for the material with a power-law flow law of eqn (A.15), one needs to consider the singularity of ρ−m(m−1+1) at the crack tip with ρ as the distance from the crack tip. The ρ−m(m−1+1) singularity cannot be created using commercial finite element method code, but the combination of ρ−1 and ρ−1/2 singularities can provide a reasonable approximation for ρ−m(m−1+1).38 Therefore, the finite elements with ρ−1/2 + ρ−1 singularity were constructed at the crack tip, as shown in Fig. 10b. Quadratic axisymmetric elements with reduced integration were used in the finite element analysis. The singularity at the crack tip was achieved by collapsing the elements.
The two-particle contact model was constructed using the commercial finite element code ABAQUS. Quadratic axisymmetric elements with reduced integration (CAX8R) were used. The contact interfaces were assumed to be frictionless. For each crack tip, 3 contour integrals of J-integral were collected to verify the path independence.
The material properties of silicon for both the single particle model and the two-particle model are assumed to be the same. The material properties and parameters used in the analysis are listed in Table 1.
Property/Parameter | Symbol | Value |
---|---|---|
Elastic modulus of pristine Si | E0 | 80 GPa (ref. 40) |
Poisson's ratio | ν | 0.29 (ref. 41) |
Volumetric strain per unit mole fraction of Li | Ω1 | 8.18 × 10−6 m3 mol−1 (ref. 42) |
Partial molar volume | Ω2 | 8.18 × 10−6 m3 mol−1 (ref. 42) |
Yield strength | σY | 2.6 × 106 Pa (ref. 43) |
Characteristic strain rate | ḋ0 | 0.001 (ref. 35) |
Stress exponent | m | 4 (ref. 35) |
Lithiation-induced softening coefficient | κ | 0.375 (ref. 40) |
Diffusivity | D | 1 × 10−16 m2 s−1 (ref. 37) |
Stoichiometric maximum concentration | Cmax | 3.67 × 105 mol m−3 (ref. 37) |
Gas constant | Rg | 8.3145 J K−1 mol−1 |
Absolute temperature | T | 296 K |
Initial radius | R0 | 50 nm |
Fig. 13 shows the distributions of hydrostatic stress in the middle surface of the electrode under different compressions. The numerical results indicate that external loads do introduce hydrostatic stress in most regions of the electrode, i.e., mechanical load is indeed transmitted to the electrode.
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