Composition and Explosibility of Gas Emissions from Lithium-Ion Batteries Undergoing Thermal Runaway

: Lithium-based batteries have the potential to undergo thermal runaway (TR), during which mixtures of gases are released. The purpose of this study was to assess the explosibility of the gaseous emission from LIBs of an NMC-based cathode during thermal runaway. In the current project, a series of pouch lithium-based battery cells was exposed to abuse conditions (thermal) to study the total amount of gases released and the composition of the gas mixture. First, the battery cells were placed in a closed vessel


Introduction
The safety of lithium-ion batteries (LIBs) is of major concern because of their high energy density. The primary safety hazards are the ignition of the cell due to thermal runaway and its accompanying gaseous emissions [1]. Heat transfer during thermal runaway can be induced by the decomposition of individual cell components or by interactive reactions between multiple components [2]. This results in heat generation and, in some circumstances, the release of harmful gases and fire.
Previous investigations have been conducted to quantify gaseous emissions and possible hazards, but most studies do not cover pouch lithium-ion batteries with NMC-based decomposition reactions can be enhanced by the temperature of the expelled gases [11]. This could result in a cascade thermal runaway of adjacent cells. The majority of thermal runaway reactions occur during or shortly after the Li-ion cell has reached 100% SOC [23]. From an energy perspective, the occurrence of a thermal runaway is less likely in LIBs with a low SOC [24].
Hollow-sphere glass granulate-like pyrobubbles have found effective applications in fire protection. Foam-like granules made from silicon dioxide with a diameter ranging from 0.5 to 5 mm have low thermal conduction, are not inflammable, are floatable, have outstanding asphyxiation, and have a high melting temperature (>1373 K) [25]. In this study, the effectiveness of pyrobubbles in removing the gas components in gas emission was investigated.
In summary, this work presents investigations of the emissions from NMC lithiumion batteries during thermal runaway at SOCs of around 0%, 30%, 50%, 80%, and 100%. The main focus of this investigation is the total amount of gases released, the gas composition, and the explosibility parameters of the emissions. The effectiveness of pyrobubbles in the removal of the gas emissions, namely CO, CO2, CH4, HCN, HF, C2H6, and C2H4, at different SOCs was evaluated.

Cells
In total, 34 pieces of lithium-ion cells with NMC-based cathode and graphite anode were used for the investigation. The electrolyte is composed of four different mixtures, namely ethylene carbonate (EC), ethyl methyl carbonate (EMC), dimethyl carbonate (DMC), and propylene carbonate (PC). Each cell used lithium hexafluorophosphate (LiPF6) as conducting salt. The batteries tested were pouch LIBs with nominal capacities, of 2.5 Ah (≈9.25 Wh), 10 Ah (37 Wh), and 32 Ah (≈118 Wh). The parameters of the studied cells are presented in Table 1. As depicted in Table 2, 31 tests were performed in three different test series. A battery stack consisting of two 10 Ah cells (double-cell) assembled together was also studied. As illustrated in Figure 1C, these cells were labeled as A and B.

Hollo-Sphere Glass Granulate Filter
A filter was used to treat the gases released during thermal runaway. The filter was made up of a stainless-steel container with hollow-sphere glass granulate (pyrobubbles) as the filter media. The properties of the pyrobubbles are shown in Table 3. The cylindrical container had an inner volume of 1.26 L (diameter, Ø = 100 mm; height, h = 160 mm). It had three openings, an inlet for off-gas inflow, an outlet for treated-gas outflow to the FTIR, and a vent. The cylindrical filter chamber was filled with 400 g of pyrobubbles.  Figure 2 shows the experimental setups for the thermal abuse. For test series 1 and 2, the thermal runaway was triggered inside an air-tight stainless-steel vessel with 10 L and 100 L inner volumes, respectively. A pyrobubble filter was incorporated into the experimental setup for test series 1. The cells used in test series 1 and 2 were forced into thermal runaway by local overheating using a glow plug and a heating plate, respectively. Overcharge experiments were performed in test series 3 in an enclosed explosion chamber with dimensions of 500 mm × 300 mm × 300 mm (height × length × width). The surface area of the glow plug for heating had a diameter of 5 mm and a height of 10 mm. Heat was supplied from the surface of the heating plate with dimensions 150 mm × 100 mm × 20 mm (height × length × width). To protect the heating plate from the direct impact of the thermal runaway, a stainless steel panel with a thickness of 2 mm was installed between the heating plate and the LIB, as shown in Figure 2. A transformer (TF) (Thalheimer LTS 606 Isolation Transformer, Jagst, Germany) was used to limit the power supply to the ignition sources to a maximum of 400 W.

Experimental Setup
For the third test series (overcharging), the electrodes of the cell were connected to a current regulator MRGN-900 (E. T. T.-Trading GmbH, Braunschweig, Germany) to maintain the power supply to the electrodes and voltage measurement during the overcharging process. The thermal runaway was triggered by limiting the overcharge rate (Crate) to 2 C in test #30 and 4 C in test #31. Through the application of the high-speed camera (Photron Deutschland GmbH, Reutlingen, Germany), the thermal runaway was filmed at 250 fps. The data were recorded using Phototron Fastcam Viewer version 4.
To measure the temperature and pressure, K-type thermocouples (5 pieces maximum) and a pressure transducer (Kistler's Piezoresistive Amplifier 4603b, Kistler Group, Sindelfingen, Germany) were installed on the reaction vessels (i.e., test series 1 and 2). An exception was made in test series 3, for which only the local temperature on the cell surface was measured. The temperature and pressure were measured synchronously by the transducer and thermocouples with a sampling rate of 1 kHz and 0.1 kHz, respectively. Figure 1 illustrates the arrangement of thermocouples and the positioning of the ignition sources on the test cells. An electrical actuator (EA) and a gas accumulator (GA) were installed to ensure smooth flow of gas and prevent pressurization of the gas during the feeding of the sampling section. N2 gas was used for pressure regulation in the reaction vessels during operation and purging. Data were recorded using two types of data loggers. An Agilent Data Manager (DAQ: U2355A) (DL-1) (Agilent Technologies, Boeblingen, Germany) was used to acquire pressure and temperature readings, and a DL-2 (Gasmet FTIR analyser DX4000, Gasmet Technologies Oy, Helsinki, Finland) was used to record the readings from the FTIR with a P-Hot sampling system (Ansyco GmbH, Karlsruhe, Germany). In test series 3, data logger 3 (Voltsoft (Conrad Electronic International (HK) Limited, Tsuen Wan, Hong Kong) was used to record the voltage readings during the overcharging process.

Experimental Procedure
The experiments were conducted in three series, as listed in Table 2. In test series 1, 20 pieces of 2.5 Ah Li-ion cells were ignited by a glow plug. The glow plug was installed 20 mm from the top section of the LIBs to supply direct heat, as shown in Figure 1A. Triplicate analysis of single cells in dependence on their SOC levels (≈0%, 30%, 50%, 80%, and 100%) was carried out to study the gas emissions during thermal runaway. Subsequently, single runs were performed at the respective SOC levels to analyse the gas emission removal efficiency of pyrobubbles. Fresh pyrobubbles were used for each test. First, mean values of the triplicate analysis were used for the evaluation of pressures, temperatures, and gas concentrations.
In tests series 2 (tests #21 to #26), the gas emissions from 10 Ah (nominal capacity, ) NMC cells were investigated. For tests #27 to #29, 32 Ah NMC cells were used. All tests were performed with fully charged cells.
In test series 3, the combustibility of the released gases was closely studied with fully charged 2.5 Ah cells.
Prior to all tests, the cells were checked to confirm that they did not have any physical damage. The capacities of the cells were determined by three charging and discharging processes (CC-CV) at a C-rate of 0.5 using a Voltcraft multifunctional charger (V-Charge 100 Duo, Conrad Electronic International (HK) Limited, Hong Kong). In this way, the voltage limits, minimum voltage ( ≈0% SOC) and full charge voltage ( , 100% SOC) were also known, as shown in Figure 3. Each cell was then adjusted to its respective final SOC level ( ). A weighing balance (Kern & Sohn GmbH, Balingen-Frommern, Germany) was used to measure the weight of the prepared samples before and after the thermal runaway. The LIB was then placed into a sample container made of stainless steel to reduce and probably inhibit the distribution of particulate fragments in the respective reaction vessels used for test series 1 and 2 and the combustion chamber used for test series 3. All screws were fastened; valves were tightly closed; and the power supply, thermocouples, and pressure transducer were connected.
The pressure and temperature signals were recorded during the test. The total volume of gases released was calculated using the ideal gas law as described in detail in ref [26].
To measure the gas emissions produced during the thermal runaway, the FTIR analyzer was operated at the required temperature of 180 °C to avoid condensation of flue gas components with a high boiling point in the measuring line. It was calibrated manually using Calcmet Analysis STD Software, (Gasmet Technologies Oy, Helsinki, Finland) ahead of the flue gas analysis. In addition, a gas dilution system was installed to avoid extension of the measurement range of the FTIR, especially for CO, for which the upper limit without a dilution system is 2000 ppm. The dilution factor was 1:100 such that CO concentrations of as much as 20% in volume still could have been resolved.
The flue gas measurements were performed every 10 , consisting of 3 scans, enabling rapid real-time measurement. The mean values calculated from the 3 scans were used for all gas analysis measurements.

Results
Thermal abuse tests at various SOCs (0%, 30%, 50%, 80%, and 100%) were performed on 2.5 Ah, 10 Ah, and 32 Ah Li-cells of NMC chemistry in enclosed vessels. The surface temperature of the cells ( ), maximum pressure (absolute), and inside the reactor were monitored throughout each test conducted in series 1 and 2. The study showed that the thermal stability of lithium-ion pouch cells of NMC chemistry decreases at high SOC levels.

Thermal Runaway Behavior
As shown in Table 4, the increased with increasing SOC. The highest from test series 1 (3.2 ± 0.5 bar) was observed at 100% SOC, and the lowest value (1.2 ± 0.04 bar) was observed at 0% SOC. Low pressure spikes were detected at 0% SOC (test #01-#04). The low measured may be the result of gas (smoke) released from the cells into the environment. The maximum temperatures ( ) measured on the surface of the tested cells (374-402 K) was in the range of the thermal decomposition temperature of the SEI layer [24,27]. This suggests that gas release was only the result of the decomposition of the solid electrolyte interface (SEI) decomposition layer. Visual examination of the postfailure cells indicated that the thermal abuse resulted only in gas release. In addition to the aforementioned observation, the measured values of 1.3 ± 0.1 bar and 1.34 ± 0.15 bar from the triplicate analysis at 30% SOC (test #05-#07) and 50% SOC (test #09-#11) show that the gas may have been released simply due to the thermally driven decomposition of the solid electrolyte interphase (SEI) layer followed by a reaction between the graphite material with the electrolyte and binder inside the cell. At 80% SOC and 100%, the values of the cells were measured in ranges of 2.6 ± 0.9 bar and 3.2 ± 0.5 bar, respectively. An explanation of the higher values measured at an SOC level ≥ 80% could be due to the participation of lithium in the thermal runaway reaction. Further explanation is provided elsewhere [26]. The measured at thermal runaway (can be correlated to the sum of the thermal contribution from the decomposition of the SEI layer (Qs), electrolyte (Qe), anode (Qa), and cathode (Qc) in the cell. The initial heat generated from the decomposition of the SEI layer (Qs), which occurs between 363 K and 403 K, leads to the subsequent reaction between the intercalated anode and electrolyte in the temperature range of 373 473 K with the release of energy (Qa-e) [13]. Subsequently, the NMC cathode decomposes (~483 K), followed by an exothermic reaction between the NMC cathode and electrolyte (~503 K). Then, the electrolyte combusts (523-573 K), releasing additional heat energy inside the cell. [28,29]. The total heat generated (Qgen) from the reactions during the abuse test, as mentioned above, can be written as: According to the thermal conservation equation, the behavior of the cell during thermal abuse is expressed as [30]: where (kg /m 3 ) is the cell density, (J/ kg·K) is the specific heat capacity of the cell, T (K) is the temperature, t (s) is time, and k (W /m·K) is the thermal conductivity of the cell.
The total generated heat increases the rate of reaction in the cell, inducing thermal runaway. The occurrence of a series of thermal decompositions showing an SOC dependency is evident in Table 4, as indicated by the presented values. In this sense, it can be concluded that the characteristic thermal behavior of the Li cells at an SOC level ≤ 50% is mainly limited to the decomposition of the SEI layer and the reaction between the intercalated anode and electrolyte. The thermal runaway mechanism results in a higher temperature at SOC levels > 50% due to the thermal decomposition involving the cathode and electrolyte.
For cells at 0% (test #01-#03), the was measured in a range of 374-402 K. Wang et al. (2006) showed that such cell temperatures could result from the occurrence of a decomposition reaction involving the SEI layer, causing the intercalated lithium anode with electrolyte solvent to release heat [31]. Similarly, the observed at 50% SOC could largely be attributed to a successive degradation of the separator materials within the cells [32]. According to Feng et al., the separator material melts during the degradation process. During the phase transition (melting) process, the heat present in the cell is absorbed. This could lead to a small variation in temperature and pressure measurements in #01-#08 (SOC level ≤ 30%) compared to tests #09-#12 (SOC level =50%). It is worth mentioning that the pouch cells tested at SOC level ≤ 50% showed no sign of thermal explosion. However, cell swelling was observed.
At SOC values of approximately 80%, higher values were measured. The effects of the high and associated values lead to a thermal expansion and therefore rapture of the cells. However, thermal-runaway-induced explosion of the cells was evident at 100% SOC. It could be reasoned that the level of lithiation at the cathode has an inverse relationship with the thermal stability of the cells. A decrease in the lithiation level at the cathode of the cells as a result of extraction of lithium-ion reduces its thermal stability [33].
The maximum pressure peaks obtained from test series 2 showed distinctive behavior. The measured from tests #22, #24, and #25 ranged from 1.83 bar to 2.7 bar. The measured is comparable to measured values obtained from test series 1. In tests #21, #22, #25, #26, and #27-#29, the range was approximately 4 bar to 7 bar. These high pressure measurements were a resultant of a possible subsequent gas explosion of the gas mixture released into the reaction chamber. Here, the temperatures measured on the cell surface reached the minimum ignition temperature of the ejected gas mixture and therefore caused ignition. For instance, the concentration of CO, CH4, and C2H4 gases measured from tests #27-#29 were within their corresponding explosible range. The gases could have ignited because measured cell surface temperatures exceeded their respective minimum ignition temperatures (CO = 878 K; CH4 = 868 K; C2H4 = 713 K) [34,35].
In test #30 (test series 3), there was no observed ignition of the gas mixture injected into the test chamber. The ignition of the succeeding project from the Li cell was evident in test #31 (Figure 4). Some of the flammable gas emissions were within their explosible range, and the ambient temperature inside the test chamber exceeded the minimum ignition temperature of the emerging gas mixture. The high value measured in test #30 = 750 K, and that measure in test #31 = 978 K, indicating that the gas emission from the cell probably underwent an ignition with a higher . Based on tests #21-#29, a > 750 K could provide the necessary condition for the ignition of the ejected gas mixture.
It could be deduced from the test series that the ignition source seems to have an influence on the thermal runaway behavior.
On the one hand, the measured values from test series 3 (test #30: = 750 K at C-rate = 2 and test #31: = 978 K at C-rate = 4) are higher than those measured in test series 1 (tests #17-#20: ≤ 529 K). One explanation is that the overcharge procedure (test series 3) introduced additional electrical energy into the cell before the thermal runaway was triggered. SOC values of 194% (test #30) and 180% (test #31) were measured prior to thermal runaway ( Figure 5). At this point, the amounts of electrical energy inside the cells were 4.85 Ah (test #30) and 4.5 Ah (test #31), resulting in the release of higher energy at a high temperature compared to test series 1 (test #17-#20). On the other hand, higher values of (780-1240 K) were measured in test series 2 compared to both test series 1 and test series 3. The reported correlation between and the stored electrical energy of the cell confirms that assumption. In test series 2, the electrical energies stored in the tested cells were 10 Ah (test #21-#23), 20 Ah i.e., 2 × 10 Ah (test #24-#26), and 32 Ah (test #27-#29); therefore, thermal runaway from the test would definitely lead to the measurement of a comparably high . In test series 3, the thermal runaway occurred in tests #30 and #31 in about 1640 s and 720 s, respectively. This indicates that the onset of thermal runaway is dependent on the overcharge rate (C rate). At a high C rate, a greater amount of energy is introduced into the cell per unit time. The onset of thermal runaway in test #30 (at C rate = 2) was approximately 2 times that of test #31 (at C rate = 4). The results indicate that the onset of thermal runaway has an inverse relationship with the overcharge rate.
Upon overcharge, lithium that has not moved to occupy the intercalation site in the anode is deposited on the surface of the anode [36]. This formation is termed lithium plating. According to Lin et. al, lithium plating forms lithium dendrite, which penetrates the separator and causes an internal short circuit [37]. In a study by Juarez-Robles et al., lithium plating and electrolyte decomposition were observed when the voltage in a cell exceeded 4.5 V [38]. As shown in Figure 5, 4.5 V was exceeded earlier in test #31 (C rate = 4) than in test #30 (C-rate = 2). The probable early occurrence of lithium plating during overcharge at a high C rate could have contributed to the earlier onset time of thermal runaway.
It is established that lithium-ion battery degradation is enhanced at a higher C rate. According to the literature, the formation of some combustible gases, namely H2, CH4, CO, C2H6, and C2H4, attributed to the decomposition of the electrolyte was significant at a high C rate [39,40]. The presence of combustible gases in significant amounts (thus, at a high C rate) at an elevated temperature could result in early occurrence of thermal runaway. This was evident in test series 3, for which runaway occurred at a higher SOC (194%) in test #30 compared to test #31 (SOC = 180%).

Released Gases
The total volume of released gas was calculated by considering the change in pressure in each test and the ideal gas law. Under the assumption that the gas inside the reaction vessel has cooled down to ambient temperature after sufficient time, the change in the number of moles in the gas phase can be calculated according to Equation (3).
where V is the free inner volume of the reactor, R is the universal gas constant, T is the initial (and final) gas temperature, and Δ is the difference between the final pressure ( ) and initial pressure ( ), as illustrated in Figure 6. In some experiments, the gas release was followed by an immediate ignition of the gases. Then, the maximum pressure inside the reaction vessel reached a level comparable to that of closed-vessel gas explosions [41,42]. Such a case is depicted in Figure 6.
In test series 1, an insignificant amount of gas emission (⪅1 L) was released at SOC levels ≤ 30%, while the highest amount of gas (6.5 ± 0.4 L) was measured at 100% SOC. The gas release at 100% SOC is in agreement with the findings of Golubkov et al. (2014). At SOC levels ≥ 80%, a comparably significant amount of gas (4.8 ± 0.6 L) was released at thermal runaway. The volume of gas produced at 100% SOC was more than three times larger than the release at 50% SOC (i.e., 1.9 L).
The normalized volumes of gas emission at 30% SOC and 50% SOC were 1.2 ± 0.2 L/Ah and 1.2 ± 0.3 L/Ah, respectively. The values obtained (at an SOC level ≤ 50%) demonstrated that the gas release occurs with less influence of the SOC.
The normalized volumes of gas released at 80% and 100% SOC were 2.4 ± 0.3 L/Ah and 2.6 ±0.2 L/Ah, respectively. This provides a clear indication that the maximum gas release is likely to occur at SOC levels ≥ 80%. In addition, the literature shows that the normalized volume of gas relative to the capacity proportion of NMC cells is in the range of 1.2-2.5 L/Ah [13,43]. The measured values fit into the data reported in literature.
In test series 2, the highest level of gas release (102 ± 4 L) was generated from tests #27-#29 (32 Ah NMC cells), with a normalized gas volume of 3.2 ± 0.1 L/Ah. In three tests (#21, #22, and #23) with 10 Ah single cells, the amount of gas released from tests #21 and #22 was 16.5 ± 1.5 L (1.65 ± 0.15 L/Ah), while a higher volume of up to 42 L (4.2 L/Ah) was produced in test #23. Likewise, tests #24 and #25 (double cells) produced 42 ± 1 L of gas, corresponding to a normalized value of 2.15 ± 0.05 L/Ah. The characteristic emission of the abovementioned double cells was smaller than that obtain in test #26 (71 L; 3.6 L/Ah). The divergence of the observation cannot be explained by the increase in the number of moles added to the gas phase due to gas emission. Figure 7 shows that the thermal runaway in test #26 generated a of 2.96 bar, followed by a succeeding high-pressure peak ( = 7.28 bar) within 35 ms. Although the minimum ignition temperatures and lower explosion limits of the gas mixtures released during thermal runaway are the subject of a succeeding project, it can be stated that the composition of the gas mixture inside the RV could have reached the explosible range and that the surface temperatures of the cells during runaway exceeded the minimum ignition temperature of the emerging gas mixtures in these tests.

Composition of Released Gases
The average concentrations of the most relevant analyzed gas components are presented in Table 5. In test series 1, the prevailing gas components, i.e., CO2 (≈48 ± 1 vol%), C2H4 (≈8.1 ± 2.3 vol%), CO (≈6.8 ± 0.9 vol%), and CH4 (≈4.3 ± 0.9 vol%), were measured at 100% SOC. No CO2 was detected at SOC levels of 0% (tests #01-#04) and 30% (#05-#08), which means that the reaction is less complete during thermal abuse. The production of CO2, CO, CH4, C2H6, and C2H4 was promoted at high SOC levels, indicating that the conversion of the organic content of the cells into the gas phase is highly dependent on the SOC. Notably, a large fraction of the organic compounds was converted to CO2 at a higher SOC. Additionally, the high measured volume of CO is evidence that the gases are released as a result of incomplete combustion. The measured concentration of HF from the untreated gas emission is ranges from 8.5 ppm to 22 ppm. A clear trend for HF production could not be established. However, the highest HF (22 ppm) was produced at 100% SOC. The range of HF values is consistent with that reported by Larsson et al. (2016) [44]. In test series 2, none of the measured gas mixtures contained HF gas in a substantial concentration. A possible reason could be the test setup (difference in the volume of the reactor vessel). In test series 1, the HF was injected into a 10-L reactor, whereas the gas component was injected a 100-L reactor in test series 2. Therefore, it can be concluded that the ambient air in the void volume of the reactor and further dilution have influence HF detection.
Furthermore, if the HF had been released in low concentrations, the dilution factor of 1:100 might have led to HF concentrations below the limit of detection (LOD, 1 ppm).
The concentration of HCN from the untreated gas mixture was identified to be between 34 ppm and 200 ppm and was clearly higher at high SOC levels. The laminated aluminum film used in the case of pouch cells contains polyamide [45]. In the event of thermal decomposition of the polyamide, ammonia (NH3) could be produced [46]. The resulting reaction of NH3 could possibly be promoted by the presence of CH4 and CO to produce HCN: CH4 + NH3 → HCN + 3 H2 CH4 + NH3 + 1.5 O2 → HCN + 3 H2O Generally, test series 2 shows that the relative concentration of CO increased with higher cell capacity. Higher concentrations of CO release were observed in tests #26 and #27-#29. The measured concentration of CO emission in test #26 (168,500 ppm; 16.85 vol%) was the highest, with lowest emission (29,220 ppm; 2.92 vol%) measured in test #22. The CO emission in test #26 was about 2.5 times higher than that of tests #24-#25 (10 Ah double-cells). Additionally, test #26 produced approximately 4-6 times more CO compared to test #21-#23.
The amount of CH4 released was between 8040 ppm and 76,050 ppm. The concentration of CH4 increased with increasing cell capacity. Using test #21 (in which the least amount of CH4 was measured among the series) as a basis, the generated concentration of CH4 increased by a factor of 9.5 with respect to test #29.
Among the ejected gases, HCN was released in the lowest concentrations. HCN emission was measured to be between 80 ppm and 380 ppm. Unlike tests #23 and #27-#29, the concentration of HCN emission in test #26 (80 ppm) did not differ considerably compared to tests #21-#22 (105 ± 5 ppm). The autoignition temperature is known to be 811 K [47]. Such high temperatures were recorded in LIBs with high SOC values and capacities, meaning that HCN could have also autoignited to form other products at temperatures above this set value.
Compared to the other hydrocarbons considered in both test series, the concentration of generated C2H6 was low. The concentrations of C2H6 released from the cells was the lowest compared to the other analyzed hydrocarbons (CH4 and C2H4).
Similarly to CH4, the release of C2H4 showed an increase with regards to cell capacity. A low amount of C2H4 was measured in test #26 compared to the other double cells (tests #24-#25). The reason for this observation might be the decomposition of C2H4 to form other components, as the autoignition temperature of 723 K was exceeded.

Explosibility of Released Gases
Five combustible gases, namely CO, HCN, CH4, C2H4, and C2H6, were studied using their respective explosible ranges [48][49][50]. The measured ranges of the gas components of the untreated gas mixture from test series 1 and 2 (tests #17-#29) at 100% SOC are presented in Table 6.  Table 6 shows that the concentrations of gases released during the aforementioned tests reached the explosible range. Applying Le Chatelier's law based on the lowest values measured for the individual components (see Table 6) yields a lower explosion limit (LEL) of 7% in the volume fraction for the gas mixture and an upper explosion limit (UEL) of 31% in volume.
H2O and CO2 are known to be effective inhibitors of fires and explosions; however, the free volume of the reactor vessel contains sufficient oxygen to support a secondary explosion.
As presented in Tables 5 and 6, two (HCN, C2H6) out of the five analyzed flammable gases had concentrations below that of the explosible range. CO, CH4, and C2H4 were detected at levels within their corresponding limits. Therefore, the risk of further combustion could be supported by these explosible compounds in the presence of an ignition source and substantial amount of air. The 32 Ah lithium-ion cells (test #27-#29) released CO, CH4, and C2H4 in concentrations of approximately 13.61 ± 1.2 vol%, 6.08 ± 1.5 vol%, and 7.10 ± 0.8 vol%, respectively, all of which are above the LEL. Similar observations were made in test #26, in which the concentration of released CO was 16.85 vol%; tests #17-#19 (8.12 ± 2.32 vol%); test #24 (3.51 vol%); and test #25 (3.77 vol%), in which the measured C2H4 exceeded the LEL.

Gas Treatment with a Pyrobubble Filter
A filter comprising hollow sphere glass granulate (so-called pyrobubble) was used for the removal of the studied gas components released during the thermal abuse. The values obtained from the test with the filter were used to calculate the removal efficiency based on the gas component emission from the triplicate tests conducted in test series 1 according to eq. 2.
Here, the removal of gas component ( ) was: where is the average concentration of gas component without the pyrobubble filter, while is the concentration of gas component in a test with the pyrobubble filter. Figure 8 shows gas component removal at various SOC states. According to the gas emission data presented in Table 5, up to 48 vol% of CO2 was detected (see tests #17-#19). The total amount of CO2 released at the respective SOC levels was reduced to an insignificant level (99.96-100% removal), irrespective of the high concentrations detected. The removal of CO ranged between 26 and 95%. A clear relation was not established for CO removal. However, at high SOC values, the removal of CO was less effective. A similar observation was made for C2H6, with a lower percentage of removal at high SOC states. The removal of C2H6 was observed to be lower at high SOC value, although a linear trend could not be established. Additionally, 86%-92% removal was achieved for C2H6 at SOC levels ≤ 30%. The ineffectiveness of the pyrobubbles at high SOC value may be related to the amount of CO2 released, as elaborated in the following paragraph.
The retention of HF and HCN by the pyrobubble bed did not follow a particular pattern. However, the respective removal ranges of 7-54% and 62-94% cannot be neglected. The removal efficiency of the pyrobubble filter may be influenced by the available active sites. In the case of the gas components such as CH4, C2H4, and C2H6, the removal rate was generally lower at a high-SOC states. After the near-complete removal of highly concentrated CO2, there were likely fewer active sites available for component removal, resulting in the observed outcome.
Although the diffusion of the gas component through the pores of the pyrobubbles was not studied, we can deduce that retention of high-concentration gas components such as CO2 resulted in the saturation of the pyrobubbles. At this point, gas component reduction cannot be controlled by diffusion, and it is possible for some gas components to pass through the pyrobubble bed without being adsorbed.

Conclusions
This study revealed that the concentrations of gaseous emissions consisting of CO, CH4, C2H4, C2H6, and HCN are likely to exceed the LEL of the gas mixture. Among the analyzed gases, CO and CH4, together with C2H4, were detected in levels within their corresponding individual flammability ranges. The inhibiting effect of inert gases such as CO2 and water vapor does not reliably prevent ignition of the gas mixture ejected from batteries. In the presented test series, a secondary explosion occurred in one test, leading to a maximum pressure of about 7 bars in the 100 L-reactor. Presumable ignition sources were either the hot gases themselves or hot metal parts of the battery. A test performed in an enclosed vessel showed an ignition of the hot gas ejected into the environment. This observation confirmed that hazards associated with the occurrence of secondary explosion cannot be neglected.
It could be deduced from the test series that the ignition source seems to have an influence on the thermal runaway behavior. For cells triggered by the overcharge procedure, the addition electrical energy introduced into the cell resulted in the release of higher energy at a higher temperature compared to cells triggered by overheating. The results indicate that the onset of thermal runaway has an inverse relationship with the overcharge rate. Therefore, lithium-ion battery degradation is enhanced at higher C rates.
Overall, the test series revealed that treatment with hollow-sphere glass granulate can be used to lower the concentration of the gas components released during thermal runaway. The drop in the concentration of the gas components minimizes the risk of occurrence of a secondary explosion.  Data Availability Statement: All the data are included in the paper.

Conflicts of Interest:
The authors declare no conflict of interest.