The initial test cycle, conducted at 0.2 C, 0.5 C, and 1.0 C, revealed the reference battery's capacity to be 162.8 mAh, 157.5 mAh, and 151.2 mAh, respectively. The cell subjected to cycling exhibited capacities of 155.0 mAh, 150.2 mAh, and 144.2 mAh, respectively (Fig. 4C). Subsequently, the experiment subjected the battery to 100 cycles of 1C load. Until cycle 42, the capacity demonstrated a gradual decline at a rate of approximately 0.15% per cycle. At this point, a more rapid capacity decline of about 0.6% per cycle became evident (see Fig. 4A, 4B). Furthermore, a decline in Coulombic efficiency was observed in this phase. Ultimately, the battery reached the end of its cycle life after 59 cycles, accompanied by a 20% capacity loss. After completing 100 cycles, the total capacity loss reached 40%, to a final capacity of 86.5 mAh (compared to 144.2 mAh at the start of cycling). Finally, post-cycling test cycles performed at 0.2 C, 0.5 C, and 1.0 C revealed a capacity of 90.0 mAh, 68.9 mAh, and 45.8 mAh, respectively (Fig. 4C). This decrease in capacity was also accompanied by a significant drop in the discharge plateau. Notably, these test cycles were performed subsequently to the CT scan of cycled battery rather than immediately following the completion of the cycling process. Therefore, we assume that, meanwhile, in the cycled battery cell, a continuous degradation process took place. After the test was completed, a third cell from the same production series was subjected to the identical electrochemical testing. The result of this cycling was similar and rapid capacity degradation is therefore not a random event.
Figure 4D showcases the Nyquist diagram of the electrochemical impedance spectroscopy (EIS) data obtained before and after cycling, including the corresponding equivalent circuit model. The curves clearly show the significant changes that occurred because of cycling. The series electrochemical resistance (ESR) value, which initially measured 81 mΩ, increased to 167 mΩ after cycling. This change is associated with electrolyte decomposition, as was evident in the CT analysis of the battery swelling. Furthermore, this change is due to the increase in the solid electrolyte interphase (SEI) layer and along with the likely deposition of lithium on the electrode surface and the structural damage to the graphite in the anode layer, as evidenced by the combined changes in RSEI and the constant phase element CPE1. Before cycling, the RSEI value measured 19 mΩ, which subsequently increased to 442 mΩ post cycling. Simultaneously, there was an increase in the charge transfer resistance (RCT), which increased from 393 mΩ to 549 mΩ. This increase is related to the electrode corrugation, resulting in localized loss of contact and an overloading of the cathode material in the contact area, as revealed by the CT analysis.
Utilization of space-filling helical trajectory enabled scanning of the cell on the whole cell level with sufficient resolution to distinguish components of the inner structure. Figure 5 presents a CT scan image of the cell before electrochemical cycling, depicting its internal structure. The cell comprises 12 anode and 13 cathode layers distinguished by the folds. The first outer active layer encountered is the anode marked as (1), followed by a single-coated cathode layer (2) positioned on the outer side, enveloping the anode. The second cathode layer commences in position (3), 8 mm below the initial beginning of the anode layer (1).
Consequently, this 8 mm section of the anode layer remains inactive. A notable gap can be observed within the cell's central region, resulting in a significant void. The electrodes tend to bend, creating two distinctive undulations or "waves" during cycling.
Following a series of 100 cycles, the battery experienced inflation by 29%. Comparing the tomographic cross-section of the cycled cell with the new cell (Fig. 6), it is evident that the bulged regions exhibit increased spatial separation. This bending induced by deformations has led to the emergence of new bulged regions situated at the lower side of the tomographic cross-section of the cell. Furthermore, the inter-electrode space reveals the presence of discernible material filling this void (Fig. 11).
During the cycling process, a fully charged reference cell was disassembled, and an optical inspection (Fig. 7) revealed a uniform lithiation pattern on the anode, indicated by its golden colour. However, the ends of the anode, where the cathode material is absent on the cathode side, remained black. Furthermore, slight discolouration of the separator is evident in the active regions, and the cathode material adhered to the separator in the bends of the cell edges. SEM analysis of the cathode cross-sections prepared using BIB revealed that the active material consisted of spherical particles with sizes up to 20 µm. The thickness of this active layer ranged from 45 to 60 µm, while the current collector is measured at approximately 12 µm. The overall thickness of the cathode measured 120 µm. In the case of the anode, the particles exhibited an oval shape in size up to 45 µm. The thickness of the active layer in the anode ranged from 55 to 65 µm, and the current collector was approximately 7.5 µm. The total thickness of the anode was 130 µm. Notably, the electrodes did not contain a surface layer, such as alumina).
Figure 7 presents different contrast exhibited by individual grains of the anode's active material. The EDS analysis shows the material is the same material – graphite. This difference may arise from varying degrees of lithiation, as the low-energy electron in-lens detectors are sensitive to conductivity. However, this assumption cannot be confirmed through EDS analysis. The cathode analysis confirmed the presence of NMC 532 as the electroactive material. Both electrodes also contained traces of fluorine, phosphorus and residual sulphur.
After analyzing the disassembled fully charged cell after cycling (Fig. 8), a noticeable observation is the incomplete lithiation of the anode in the cycled cell. The anode shows a lack of golden-coloured areas, indicating insufficient lithiation. However, dark regions can be identified, surrounded by bright, metallic shiny formations. The separator displays a more yellow-brown compared to its original appearance. At first view, there are no visually observable changes on the cathode. Furthermore, reduced delamination and adhesion to the separator are observed, indicating improved integrity.
A detailed CT scan shows material in the cavities (Fig. 9a, b). Optical inspection revealed this result from the lithium plating process (bright formations) taking place at the interface of the inactive region indicated by dark colour and the active region of the electrode (Fig. 9c, d). The inactive regions recorded by the optical microscope correlate to the cavities visible in the tomographic cross-section of the CT scan. The individual locations of these inactive regions can be correlated to the measured distances in the CT model. A BIB cross-section was prepared from the area on the active/inactive region boundary (Fig. 9e, Fig. 10).
The BIB cross-section SEM analysis of the anode exhibited over-lithiated surface graphite particles (Fig. 10). The individual layers within the anode are tearing and separating apart due to the lithium growth. Some graphite layers lost contact with the grains, rendering them inactive. The height of the lithium layer on the surface reached up to 30 µm, causing a potential risk of short-circuiting. Considering the thickness of the separator is approximately 20 µm, this elevated lithium dendrite height increases the likelihood of puncturing the separator. Comparatively, the SEM/EDS analysis of the cathode cross-section indicated no notable changes in the internal structure composition or significant grain cracking. However, the active regions were coated with a thick Cathode Electrolyte Interface (CEI) layer on the surface.
Furthermore, the anode and cathode surfaces were examined to assess their composition and structure across different regions. Figure 11 exhibits SEM images of the anode surface of the reference and aged cells in both the inactive and active areas within Region 4A. Subsequently, Fig. 12 presents a corresponding analysis for the cathode in region 6A. EDS analysis was conducted in all the areas mentioned above, and the results are summarized in Table 2 for the anode and Table 3 for the cathode.
Table 2
Results of EDS analysis of anode surfaces, region 4A
Anode | Atomic % |
Element | Reference | Aged inactive | Aged active |
C | 76.4 | 77.4 | 21.8 |
O | 9.1 | 16.5 | 36.1 |
F | 13.3 | 5 | 35.5 |
P | 0.5 | 0.4 | 5.5 |
S | 0.2 | 0.2 | 0.6 |
Table 3
Results of EDS analysis of cathode surfaces, region 6A
Cathode | Atomic % |
Element | Reference | Aged inactive | Aged active |
Ni | 10.0 | 9.2 | 8.3 |
Mn | 6.9 | 6.4 | 5.4 |
Co | 4.2 | 3.8 | 3.5 |
O | 33.8 | 34.9 | 34.6 |
C | 27.2 | 30.3 | 25.1 |
F | 17.3 | 14.8 | 21.8 |
P | 0.4 | 0.3 | 0.9 |
S | 0.1 | 0.1 | 0.3 |
The SEM images reveal the surface structure of the reference electrode, which closely resembles the inactive region of the cycled cell. However, EDS analysis exhibits changes in composition, specifically a decrease in fluorine and phosphorus content. In contrast, the active region shows a thick surface layer that overlaps over the active material grains, accompanied by a significant increase in fluorine and phosphorous content. Although EDS analysis does not directly detect lithium, elevated fluorine and phosphorus concentrations indicate its presence as intense electrolyte decomposition occurs. Trace amounts of sulfur were detected, with the concentration being up to three times higher in the active region. This further confirms the presence of lithium metal since sulfur tends to precipitate onto it.