1. Introduction
At the end of 2023, global proven natural gas reserves have risen to an estimated 212.54 trillion cubic meters [
1], which takes no account of those trapped in gas hydrates at the continental slopes of oceans and in permafrost areas; it was estimated that the amount of natural gas stored in global recoverable natural gas hydrates is between 25.55 and 84.36 trillion cubic meters [
2]. Additionally, biogas is being considered a renewable natural gas that is generated from the thermochemical conversion or anaerobic digestion of crops, residues, and waste. Currently, a major portion of natural gas in the world is directly burned to produce energy for heating and power generation, which has high exergy losses and CO
2 emission.
Compared with combustion, the transformation of the predominant component of natural gas, methane (CH
4), into chemicals or liquid fuels is more economically viable [
3]. Methane can be converted to syngas, a mixture of hydrogen (H
2), carbon monoxide (CO), and some carbon dioxide (CO
2) by reforming [
4]. Subsequently, syngas is used to produce high-value products, such as liquid fuels, waxes, or light alkenes. There are two main conventional reforming technologies: steam methane reforming (SMR) and dry reforming of methane (DRM) [
5,
6]. The former is being widely used in the chemical industry to produce hydrogen, whereas the latter has not yet reached full technological maturity, although it has environmental and economic advantages. CH
4 has a symmetrical tetrahedral configuration with four equivalent C−H bonds, which makes it very difficult to activate methane. Thus, the reforming reactions are always carried out at high temperatures in the presence of supported metal catalysts. One of the thorny issues associated with thermal catalytic reforming at high temperatures and pressures is coking, which results from both methane thermolysis and CO disproportionation reactions. To address that, one can optimize the operating conditions and/or design novel catalysts [
7,
8]. Alternatively, coking is inherently circumvented in chemical looping reforming (CLR) processes [
9,
10,
11], which can be driven by solar energy.
A typical chemical looping scheme involves two steps: a redox material (usually a metal oxide) is first reduced by methane (MeO
x + δCH
4 → MeO
x-δ + 2δH
2 + δCO), and then the reduced metal oxide is re-oxidized (or regenerated) by putting it in contact with steam or CO
2 to replenish its lattice oxygen, producing hydrogen or carbon monoxide (MeO
x-δ + δH
2O/CO
2 → MeO
x + δH
2/CO). Generally, coking may occur in the reduction step, but the solid carbon is completely gasified (C(s) + CO
2 → 2CO, C(s) + H
2O → H
2 + CO) in the oxidation step. Another two obvious advantages of CLR over conventional reforming are: the syngas ratio (nH
2:nCO ≈ 2:1) of the reduction step is very suitable for most downstream processes such as Fischer-Tropsch synthesis and direct methanol synthesis. A pure CO stream is obtained in the oxidation step if CO
2 is used to replenish the lattice oxygen, which could be directly used as the feed for the production of phosgene as an intermediate for polycarbonate production [
12]. Additionally, if steam is used to replenish the lattice oxygen, then a hydrogen-rich or even pure hydrogen stream will be produced in the oxidation step. The high concentration of hydrogen reduces the specific requirements of utilities and offers substantial advantages in the selection of purification technologies.
In the reduction step (with respect to the redox material), two main side reactions have to be inhibited: one is the complete oxidation of methane (combustion), and the other is methane pyrolysis. The former reduces carbon efficiency, whereas the latter results in coke. In typical operating conditions, gas-phase methane pyrolysis is always negligible, and catalytic pyrolysis over metal particles plays a key role in coking. Therefore, any strategies that can tune the geometric and electronic structure of the metal particles could suppress coking, e.g., designing the redox materials (also known as oxygen carriers) with confined microenvironments. On the one hand, considerable effort in recent years has been devoted to the development of high-performance perovskite-typed OCs. Li et al. reported perovskite nanocomposites where SrFeO
3-δ is dispersed into a matrix of mixed metal oxides and exhibit excellent redox performance toward the chemical looping and reforming of methane [
13]. Shen et al. found that A and B co-doping of LaMnO
3-δ shows satisfactory performance and good stability in chemical looping steam methane reforming [
14]. Our group investigated the effect of nickel and cobalt doping on the redox performance of SrFeO
3-δ toward chemical looping dry reforming of methane [
15]. Zhou et al. prepared high-performance Sr
0.98Fe
0.7Co
0.3O
3-δ perovskites by combining A-site defects and B-site doping of SrFeO
3-δ [
16]. On the other hand, the mechanism of methane oxidation by perovskite-typed OCs remains elusive. Methane combustion is always attributed to adsorbed oxygen species on the surface of oxygen carriers (OCs) [
14,
17,
18]. However, adsorbed oxygen species can enter the lattice structure, and oxygen species can leave the lattice structure after migrating to the surface. There is also evidence that surface species and lattice species can both be active in the same reaction, and the surface species operate on shorter time scales (<10 ms) [
19]. Therefore, it is worthwhile to investigate the oxygen species that are involved in the deep oxidation of methane in detail. In this context, we investigated methane oxidation by SrFeO
3-δ, a perovskite-typed OC, at 900 °C and 1 atm in a pulse mode. The OC was synthesized by a Pechini-type polymerizable complex method, and the carrier gas was pure argon or an argon and hydrogen mixture. At a pulse interval of 10 min, the amount of CO
2 produced in the absence of hydrogen is one order of magnitude greater than that in the presence of hydrogen. In the former case, the amount of CO
2 produced dramatically decreases first and then gradually approaches a constant, and the oxygen species involved in methane combustion can be partially replenished by extending the pulse interval. Our findings suggest that most oxygen species that perform methane combustion reside in the surface layer, and a large portion of this kind of oxygen species can be eliminated by hydrogen. These findings further our understanding of e methane combustion in the reduction step of chemical looping reforming.
3. Results and Discussion
The compound SrFeO
3-δ belongs to the class of non-stoichiometric compounds in which the oxygen non-stoichiometry (δ) is variable [
20,
21,
22]. This compound, δ can continuously vary in the range of 0 to 0.5. Extensive studies on this compound have shown that there exist four phases of ideal composition in the range 0 ≤ δ ≤ 0.5 [
18,
19], these are: cubic SrFeO
3 (δ = 0), tetragonal SrFeO
2.875 (δ = 0.125; or equivalently Sr
8Fe
8O
23), orthorhombic SrFeO
2.75 (δ = 0.25; or equivalently Sr
4Fe
4O
11), and brownmillerite SrFeO
2.5 (δ = 0.5; or equivalently Sr
2Fe
2O
5). For all the others, the composition is a mixture of the two nearest ideal phases. On the other hand, the ranges of δ in which a single phase exists at room temperature differ from one study to another and can be roughly estimated to be 0 ≤ δ ≤ 0.08 for cubic, 0.125 ≤ δ ≤ 0.17 for tetragonal, and 0.25 ≤ δ ≤ 0.32 for orthorhombic phase. For the as-prepared SrFeO
3-δ at ambient conditions, its diffraction patterns well match those of SrFeO
2.86 (
Figure 1), suggesting that δ is equal to 0.14. From the above description, it can be said that the as-prepared SrFeO
3-δ has a tetragonal structure and it may contain a minor amount of orthorhombic phase.
For SrFeO
3-δ, the oxygen non-stoichiometry depends on both temperature and oxygen pressure and the relationship can be described by the following equations [
20,
21,
22],
where T is temperature (K), P
O2 is oxygen pressure (atm). According to the specification provided by the vendor, the oxygen content in the pure argon is less than 1 ppmv but the measured one is 2 ppmv. In this case, the variation of the oxygen non-stoichiometry with temperature is illustrated in
Figure 2. As can be seen, δ approaches 0.5 as the temperature increases to 900 °C, suggesting that the tetragonal structure will change to brownmillerite phase when SrFeO
3-δ is treated in pure argon at 900 °C.
Before pulsing methane to the OC bed, as-prepared SrFeO
3-δ particles were heated in pure argon to the targeted temperature. As
Figure 3 shows, oxygen release was observed at a temperature range of 300 to 800 °C. The release of oxygen can be divided into two steps, one at temperatures between 300 and 500 °C and the other at temperatures between 500 and 800 °C. At ramping rates of 2.5 and 5 °C/min, there exist doublet peaks in the low-temperature region that merge into a single peak when the ramping rate was 10 °C, but no trend can be observed. Therefore, this might come from the fluctuation in the flowrate of argon. Another observation is that the amount of oxygen released in the low-temperature region is less than that in the high-temperature one. Specifically, the area of the high-temperature peak is 2.5 times as much as that of the low-temperature one at a ramping rate of 2.5 °C/min.
Based on the above description, SrFeO
2.86 first transforms into SrFeO
2.75 at low temperatures and then into SrFeO
2.5 at high temperatures as the perovskite is heated up from 100 to 900 °C. As a result, the amount of oxygen released in the high-temperature region is 2.3 times as much as that in the low-temperature region. Upon combination of this value and the measured one, we can conclude that the as-prepared sample undergoes two consecutive phase transitions in the pretreatment, i.e., tetragonal SrFeO
2.86 to orthorhombic SrFeO
2.75 (T→O transition) and then to brownmillerite SrFeO
2.5 (O→BM transition). Furthermore, the activation energy of these two transformations can be evaluated using the Kissinger method [
23,
24], which is generally performed considering that
where
β is the ramping rate (°C/min),
A is the pre-exponential factor,
R is the gas constant;
E is the activation energy (kJ/mol),
Tm is the temperature at which the reaction rate is maximum (K). The plots of ln[
β/
Tm2] vs. 1/
Tm are presented in
Figure 4, from which the values of activation energy for T→O and O→BM transitions are obtained from the slope of straight lines; they are 294 and 177 kJ/mol, respectively.
Previous studies have shown that SrFeO
3-δ can be reduced to SrO and metallic iron, which are subsequently oxidized back to SrFeO
3-δ at high temperatures in a redox mode [
13,
18]. As previously stated, brownmillerite SrFeO
2.5 is the stable phase at 900 °C in pure argon. Thus, the following equation can be written for the redox reaction,
The standard Gibbs-energy changes of the above reaction and methane oxidation as a function of temperature are given in
Figure 5. According to the standard Gibbs-energy change in reactions, the reduction of SrFeO
2.5 by methane can be divided into three regions: neither methane combustion nor partial oxidation of methane is thermodynamically favorable at temperatures below 770 °C, only partial oxidation of methane is thermodynamically favorable at temperatures between 770 and 1110 °C, and both are thermodynamically favorable at temperatures above 1110 °C. Therefore, chemical looping reforming of methane should be operated in the second region. At 900 °C and 1 atm, the partial pressure of oxygen is 4.2 × 10
−20 atm at equilibrium; thus, the equilibrium ratio of
PCO to
PCO2 is about 37.4. It is worth noting that the lower the oxygen pressure, the higher the selectivity toward partial oxidation, and the lower the conversion in the second region.
When pure argon was used as the carrier gas, both partial and complete oxidation of methane were observed after pulsing methane to the OC bed at 900 °C and 1 atm (
Figure 6). In the seven consecutive pulses with an interval of 10 min, both the conversion of methane and the amount of CO
2 produced dramatically decrease in the first four pulses and then gradually approach constants in the last three pulses. On the other hand, the amount of hydrogen produced follows an opposite trend. Specifically, methane conversions are 28%, 13%, and 12% in the first, fourth, and seventh pulses, respectively. The amount of CO
2 produced in the first pulse is 3.5 times as much as that in the fourth pulse, and the amount of hydrogen produced in the fourth pulse is 6 times as much as that in the first pulse; the former decreases by 1.2 times and latter increases by 1.1 times in the last three pulses.
As
Figure 6d shows, the selectivity of CO
2 is as high as 71% in the first two pulses and higher than 32% in the following five pulses. According to the above discussion, the partial oxidation of methane is favorable over methane combustion when it contacts SrFeO
2.5 at 900 °C. These observations clearly indicate that most oxygen species involved in methane combustion are not the lattice oxygen of bulk SrFeO
2.5. On the other hand, if only the surface oxygen species account for methane combustion, they will be quickly consumed because these species operate within a time scale of less than 10 ms. Therefore, we surmise that other oxygen species that perform combustion are located in the surface layer.
For the as-prepared SrFeO
3-δ, the amount of available lattice oxygen species that perform partial oxidation at 900 °C is 7.93 mmol/g
OC; thus, the total amount of this type of lattice oxygen in the fixed-bed reactor is about 2.75 mmol. For each pulse, the amount of methane injected into the reactor is around 0.0557 mmol. Because the maximum methane conversion is 28%, it is reasonable to assume that the structure of SrFeO
2.5 remains intact in the pulse run. Between two pulses, the total amount of molecular oxygen fed to the OC is 8.9 × 10
−2 μmol in 10 min, which is only 2 percent of minimum amount of oxygen species that participate in methane combustion. Thus, the replenishment of consumed oxygen species by gaseous oxygen can be ignored between pulses. The oxygen species that are located in the surface layer can replenish those involved in methane combustion, which predominantly occurs on the surface of SrFeO
2.5. If the pulse interval increases, there are more oxygen species that perform methane combustion. As expected, more CO
2 is produced as the interval changes from 10 to 20 min (
Figure 6a). A very interesting observation is that the relationship between the amount of CO
2 produced and the interval in the last four pulses (t
interval = 10, 20, 30, 60 min) is linear (inset in
Figure 6c), which may imply that not the diffusion but other factors such as the activation of adsorbed molecular oxygen control the evolution of oxygen species. More studies are required to clarify the evolution mechanism in the future.
When introducing hydrogen into the carrier gas, nine consecutive pulses with an interval of 10 min were carried out, and the results are illustrated in
Figure 7. As can be seen, both the conversion of methane and the amount of hydrogen produced monotonically increase with pulse number. On the other hand, the amount of CO
2 produced increases in the first seven pulses and then decreases in the last three pulses. A close examination of
Figure 7d reveals the variation of the amount of hydrogen produced with pulse number is linear and includes two segments; the slope of the second segment (6–9 pulse) is almost 3 times that of the first segment (1–6 pulse). At this moment, both where this linear relationship comes from and what causes the change in the slope remain elusive. The amount of CO
2 produced with hydrogen in the carrier gas is much less than that without hydrogen in the carrier gas, decreasing by more than one order of magnitude. Specifically, a decrease by a factor of 50 was observed in the first pulse. Assuming that only methane oxidation occurs after injecting it into the OC bed, then the average mole ratio of CO produced to CO
2 generated in the first 8 pulses falls between 14 and 19, but it becomes 32 in the ninth pulse. The latter is very close to the one (37.4) predicted by the thermodynamic analysis. These observations unambiguously confirm the above assumption that some oxygen species that perform combustion are located in the surface layer. Furthermore, the combustion of methane by these oxygen species may follow the bulk nucleation-growth model, which is frequently used to describe methane partial oxidization by bulk lattice oxygen [
25,
26,
27].