Open Access Article
Marwa Atwa
*a,
Sara Pedramb,
Shicheng Xuac,
Samuel Dulld,
Yunha Junge,
Takeharu Yoshii
f,
Ruohong Sui
g,
Rong Xue,
Robert Marriottg,
Hirotomo Nishihara
f,
Jonathan E. Mueller
h,
Marco Wiethoph,
Sebastian Kirschh,
Gerold Huebnerh,
Vedran Glavashi,
Jasna Jankovicb,
Thomas F. Jaramillo
*dj and
Fritz B. Prinz*acjk
aDepartment of Mechanical Engineering, Stanford University, Stanford, CA 94305, USA. E-mail: marwaatw@stanford.edu; fprinz@stanford.edu
bDepartment of Materials Science and Engineering, University of Connecticut, Storrs, CT 06269, USA
cJinetics Inc., 297 Bernardo Ave, Mountain View, CA 94043, USA
dDepartment of Chemical Engineering, Stanford University, Stanford, CA 94305, USA. E-mail: jaramillo@stanford.edu
eDepartment of Materials Science and Engineering, Stanford University, Stanford, CA 94305, USA
fAdvanced Institute for Materials Research (WPI-AIMR)/Institute of Multidisciplinary Research for Advanced Materials, Tohoku University, Sendai, 980-8577, Japan
gDepartment of Chemistry, University of Calgary, 2500 University Dr NW, Calgary, AB T2N 1N4, Canada
hVolkswagen AG, Berliner Ring 2, 38440 Wolfsburg, Germany
iDepartment of Mechanical Engineering, Mannheim Technical University of Applied, Mannheim, 68163, Germany
jSUNCAT Center for Interface Science and Catalysis, SLAC National Accelerator Laboratory, Menlo Park, CA 94025, USA
kDepartment of Mechanical and Industrial Engineering, Norwegian University of Science and Technology, Trondheim, 7491, Norway
First published on 23rd February 2026
Proton exchange membrane fuel cells (PEMFCs) have emerged as an efficient and clean energy conversion technology, utilizing platinum (Pt)-based catalysts to drive the electrochemical reactions that generate power, including nanoporous carbon-supported Pt nanoparticles. However, developing catalyst layers with exceptional stability has been a challenge, which is essential to achieving the 25
000-hour lifetime required for heavy-duty fuel cell applications. While Pt stability is critical, mitigating carbon support corrosion in the catalyst layer is equally important. Here, we show that tuning the properties of mesoporous carbon supports—specifically, pore size and the concentration of surface oxygen functional groups and H-terminated groups via high-temperature treatment—can overcome this challenge. Pore sizes of 8 nm or smaller are found to mitigate Pt dissolution and performance losses over 10
000–90
000 accelerated stress cycles. Additionally, high-temperature treatment at 2000 °C increased the carbon's crystallinity while retaining a BET surface area of 240 m2 g−1. This stability enabled the catalyst layer to maintain its initial performance after 40 hours of voltage hold at 1.2 V, demonstrating exceptional durability. These advancements are a critical step toward commercializing fuel cells for transportation applications and provide insights for advanced catalyst layer designs in clean energy conversion systems.
Broader contextProton exchange membrane fuel cells (PEMFCs) are among the most promising clean energy technologies, offering high efficiency and zero emissions through platinum (Pt)-based catalysts that drive hydrogen and oxygen conversion into electricity. However, achieving the durability needed for heavy-duty applications—up to 25 000 hours—remains a challenge due to catalyst degradation and carbon support corrosion. Tailoring mesoporous carbon supports by controlling pore size and crystallinity enhances durability, suppressing Pt nanoparticle dissolution and aggregation. Mesoporous carbons with sub-8 nm pores and high-temperature graphitization at 2000 °C maintain high surface area (240 m2 g−1) and resist oxidative corrosion, retaining catalytic activity after extensive durability tests. These corrosion-resistant, porous graphitic carbons are also ideal for water electrolyzers, CO2/CO electrolysis, and supercapacitors, serving as stable supports under harsh conditions. Advances in meso- and graphitic-carbon architectures thus offer a unifying strategy for scalable, long-lifetime electrochemical energy conversion and storage systems.
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The transition from light-duty to heavy-duty vehicle applications has shifted the focus of PEMFC research and development. While initial concerns centered on reducing capital costs, the emphasis has shifted towards improving durability and lowering operating costs over the lifetime of the fuel cell system.3,4
Different components of a single PEM fuel cell device can undergo various types of degradation, significantly impacting performance and longevity. Recent studies have provided valuable insights into these processes.5 For instance, the polymer electrolyte membrane (PEM), typically made of Nafion, can undergo chemical and mechanical degradation, leading to thinning and pinhole formation.6 Gas diffusion layers may experience changes in hydrophobicity and structure, affecting water management and gas transport.5,7 The catalyst layer, particularly on the cathode side, undergoes substantial degradation over the lifetime of a cell, with platinum nanoparticles experiencing dissolution, agglomeration, and detachment, leading to a reduction in the electrochemically active surface area.8–10 The carbon support in the catalyst layer may also corrode, especially under high potential conditions.11,12 Among these degradation pathways, catalyst layer stability, including catalyst and carbon support, remains one of the largest contributors that limits the longevity of PEMFCs.
Catalyst dissolution, particularly of platinum (Pt) and its alloys, remains a significant challenge in PEMFCs. Several mitigation strategies have been developed to address this issue. One approach involves alloying Pt with other transition metals like cobalt, nickel, or iron to enhance stability.13,14 Another method is the use of core–shell nanostructures, where a more stable metal core is coated with a thin Pt shell, reducing overall Pt content while maintaining catalytic activity.15,16 Surface modification techniques, such as the addition of atomic layers of stable metals or metal oxides, have also shown promise in improving durability.17–19 However, these methods often face limitations in long-term stability, especially under dynamic operating conditions. Some alloying elements may leach out over time, and core–shell structures can degrade in harsh electrochemical environments. Furthermore, the trade-off between enhancing stability and maintaining high catalytic activity remains a significant challenge in developing truly durable PEMFC catalysts.
In a recent study, Liu and co-workers20 designed a graphene-nanopocket-protected, pore-confined, Pt nanocatalyst supported on Ketjenblack carbon (KB), which was tested for heavy-duty fuel cell applications. The catalyst showed minimal performance loss of only 1.1% after 90
000 cycles of accelerated stress testing (AST), consisting of square-wave cycles between 0.6 V and 0.95 V with 3-second holds at each potential, which specifically probe for Pt dissolution. However, durability testing for carbon corrosion was not performed in this study.
While Pt dissolution dominates early degradation, carbon support corrosion becomes the limiting factor in long-term durability - a single start-up/shutdown event at 1.5 V can cause more carbon loss than 30
000 cycles below 1 V.12,21 The collapse of the catalyst layer architecture ultimately determines cell lifespan, making carbon corrosion mitigation equally critical to Pt stabilization. Therefore, researchers have developed several strategies to mitigate the corrosion of carbon supports of PEMFC cathodes. These include surface modification of carbon supports through graphitization and nitrogen doping, using alternative carbon structures like carbon nanotubes and graphene-based supports, and developing hybrid supports combining carbon with metal oxides or conductive polymers.22–24 However, there are often trade-offs between corrosion resistance and other aspects of fuel cell performance, such as catalytic activity or mass transport properties.25 Combining both catalyst and carbon stability in one PEMFC cathode without compromising performance and durability has not been achieved yet.
In the current study, atomic layer deposition (ALD) was used to deposit Pt onto a mesoporous carbon support. While prior studies—including our own—have applied ALD to porous carbon materials and composites to optimize Pt loading and nanoparticle size by controlling ALD cycle numbers, these works typically address only one or two of the three interrelated challenges in PEMFC catalyst layers: activity, performance, and stability.26–30 Furthermore, discussions of stability in the literature primarily focus on mitigating Pt dissolution, while carbon corrosion is often neglected.
In contrast, the present study demonstrates a cathode catalyst layer that simultaneously achieves high performance, high activity, and enhanced stability by addressing both Pt dissolution and carbon corrosion. This is accomplished by integrating Pt with highly graphitized, highly porous mesoporous carbon supports, enabling durable operation under demanding heavy-duty conditions.
In this work, we optimize a mesoporous carbon, including its surface properties, including pore size and crystallinity, to serve as a durable carbon support in a PEMFC cathode that meets and exceeds the activity, performance, and stability requirements (both catalyst dissolution and carbon corrosion) for heavy-duty applications. This represents a rare combination of these critical characteristics in a single catalyst layer electrode setup. The durability metrics of these cathodes meet the requirements of hydrogen fuel cells for heavy-duty vehicles, i.e. >1.07 A cm−2 at 0.7 V after 90
000 cycles of AST for Pt dissolution and performance retention after 40 hours of potential hold at 1.2 V as AST for carbon corrosion.
Nitrogen gas sorption analysis was used to analyze porous structure, including pore size distribution, pore volume, and extraction of the Brunauer–Emmett–Teller (BET) surface area.31 Fig. 1a shows the nitrogen adsorption and desorption isotherms of MCP8 and MCP12. According to IUPAC classifications, the isotherms for MCP8 and MCP12 powders are Type IV with H2 hysteresis, indicating uniform pore sizes and strong pore interconnectivity. These results also suggest that narrow pore necks and limited cross-sectional surface areas constrain N2 gas adsorption and desorption within the MCP porous structure.32 To reveal the pore and pore neck size distribution, the Barrett, Joyner, and Halenda (BJH) method33 was used for both MCP8 and MCP12, as shown in Fig. 1b. Both MCP8 and MCP12 have similar pore neck sizes of ∼ 4.6 nm, with an average pore size of 6.4 nm and 8.8 nm, respectively. The pore size of MCP12 is 1.3 times larger than that of MCP8, with MCP12 having a broader pore size distribution (2–15 nm) than MCP8 (2–8 nm). The specific surface area (SBET) of the MCPs was extracted from the nitrogen isotherm using the BET method (Table S1). The micropore surface area (Smicro) was calculated using the t-plot method reported by Lippens and De Boer.34 The total pore volume was estimated at a relative pressure of 0.98. The specific surface area and total pore volume (VNSI) of the MCP12 are lower than those of the MCP8, which is attributed to the increase in pore size, as shown in Table S1. Based on previous studies, differences in pore size and pore volume between MCP8 and MCP12 could potentially affect both the mass activity and stability of the Pt/MCP catalyst layer (CL).29,30,35–37
For further investigation of the microstructure, including surface chemistry, X-ray photoelectron spectroscopy (XPS) and high-resolution transmission electron microscopy (HR-TEM) were used. No significant differences have been observed in the surface carbon species and morphology of MCP8 and MCP12, as shown in Fig. 1c and d, respectively. The C 1s XPS spectra for MCP8 and MCP12 revealed the coexistence of hydrogen-terminated, hydroxide, carbonyl, and acetate surface functional groups (Fig. 1c). HR-TEM images also showed ordered, porous, spherical structures for MCP8 and MCP12, consistent with the silica templates used to prepare these mesoporous carbon powders (Fig. 1d).
We also compared electrochemical results for Pt/MCP-based GDEs with those of the commercial KB nanoporous carbon, which was sprayed onto MPL/GDL and used as a substrate for Pt ALD (prepared using the same procedure as for the Pt-MCP samples). Three sets of samples were tested: Pt/MCP8, Pt/MCP12, and Pt/KB GDEs. All three electrodes have the same Pt mass loading (0.1 mgPt cm−2) and an I/C ratio of 4.
Fig. 3a shows that Pt/MCP8 and Pt/MCP12 have higher mass activities compared to Pt/KB. The high mass activity of Pt/MCP GDEs (ca. 0.5 A mgPt−1), which is almost twice the mass activity of Pt/KB (ca. 0.3 A mgPt−1), can be attributed to the screening effect of ionomer poisoning as MCP pore size is big enough to host Pt NPs inside, but small enough to prevent infiltrate ionomer leaving it mostly outside the pores (Fig. 3a).35 For reference, most of the pores in KB are micropores, which are less than 2 nm in diameter (according to IUPAC, pores with <2 nm are micropores).32,42 Due to the microporous nature of KB, Pt grows outside the primary pores, and is therefore poisoned by Nafion, leading to a loss in activity and performance compared to Pt/MCP-based GDEs.
The confinement of ionomer to the surface of the Pt/MCP agglomerates has been confirmed by the EDS mapping of the cross-section of the electrodes (represented by the Fluorine EDS map) in Fig. S3–S5. Almost no ionomer exists inside the agglomerate, where most Pt nanoparticles are located. This confirms that the MCP8 porous structure allows for the uniform distribution of Pt nanoparticles inside and outside the carbon agglomerates while allowing Nafion to infiltrate only on the outside surface of the carbon agglomerate. The same Pt and Nafion distribution is observed in the Pt/MCP12 GDE. Thus, the performance and activity of Pt/MCP12 is expected to be similar to that of Pt/MCP8.
The electrochemical active surface area (ECSA) was obtained from the hydrogen under potential deposition (HUPD) in the cyclic voltammetry in H2/Ar at 80 °C for all three GDEs. Based on the cyclic voltammograms collected and shown in Fig. 3b, Pt/KB has the highest ECSA value (64.7 m2 gPt−1) compared with Pt/MCP12 (38.8 m2 gPt−1) and Pt/MCP8 (49.1 m2 gPt−1). Furthermore, both Pt/MCP8 and Pt/MCP12 showed similar beginning-of-life (BoL) performance and activity that is significantly higher than Pt/KB (Fig. 3a and c). Based on our previous studies, mesoporous carbon materials allow uniform Pt deposition via ALD.29,30 However, pore size would be small enough not to allow Nafion to penetrate the pores, preventing the poisoning of Pt nanoparticles.
000 voltage cycles of accelerated stress test (AST; voltage cycling between 0.6 V and 0.9 V, with holds of 3 s at each voltage) compared to Pt/KB. The results in Fig. 3c reveal the high stability of the Pt/MCP8 catalyst layer, where the performance is almost fully retained after 10
000 cycles (with no current density decrease at 0.7 V). In comparison, a loss of 20% and 22% in the performance of Pt/KB and Pt/MCP12, respectively, has been observed in Fig. 3c.Furthermore, we conducted over 30
000 cycles with Pt/MCP8, featuring a higher Pt mass loading (0.3 mgPt cm−2), to evaluate its suitability for heavy-duty applications. The results, shown in Fig. 3d, revealed performance losses after 30
000 cycles of Pt dissolution. The electrochemically active surface area of this sample remained unchanged up to 10
000 cycles, followed by a 34% decrease after 20
000 cycles and an additional 8% decrease after 30
000 cycles, amounting to a total 42% reduction in ECSA. This suggests that the most significant changes occurred after 20
000 cycles. Nevertheless, the reduction in ECSA does not necessarily translate into performance losses, a finding consistent with previous studies.37
In the Pt/MCP8 MEA, a similar Pt NP size (ca. 1.5 nm) in both the inner and outer surfaces (Fig. 4a) was observed at BoL (Table S2). However, at the EoL (after 10
000 cycles), an observed difference in the Pt NP size between the inner and outer surface of the carbon agglomerate of the Pt/MCP8 catalyst layer (CL) is detected (Fig. 4b and Table S2). There is a significant increase in the Pt NP size of the outer surface (4.3 nm) versus the inner surface (2.6 nm), shown in Fig. 4c. This indicates that Pt dissolution and growth within the pores may be limited by mass transport of dissolved Pt ions through the pores and thus exhibit a strong dependence on the primary porosity. Pt NPs on the outer surface are not subject to the same transport limitations and are thus more susceptible to agglomeration and Ostwald ripening.43 This decrease in Pt dissolution results from the pore confinement effect,25,43 which explains the stable performance of Pt/MCP8 (Fig. 3c and d).
Moreover, we investigated the change in the Pt NP size in the MEA with the larger pore-size carbon support (MCP12). At BoL, the TEM of Pt/MCP12 presents Pt NP size (∼1.5 nm) located in the inner and outer surfaces of the carbon agglomerate, similar to what has been observed in the Pt/MCP8 GDE (Fig. 4a and d). However, at EoL (after 10
000 cycles), Pt growth of both inner and outer Pt particles is more significant than in Pt/MCP8, Fig. 4e and f and Table S2, with the average inner Pt NP size of 4.8 nm, and average outer Pt NP size of 6.8 nm. This dramatic increase in the Pt NP size in Pt/MCP12 may be attributed to the presumably low mass transport resistance of dissolved Pt ions, which is likely due to the larger pore size and could explain the significant loss in the performance of Pt/MCP12 after 10
000 cycles (Fig. 3c).
In Fig. 5c and d, the HR-TEM images of MCP8 and MCP8-2000 and the corresponding FFT patterns reveal an interlayer spacing of 0.397 and 0.350 nm, respectively, which is larger than that of pure graphite (0.335 nm).44 While both carbons (MCP8 and MCP-2000) show higher interlayer distance than pure graphitic carbon, MCP8-2000 shows values significantly closer to graphitic carbon. The interlayer distance of 0.350 nm in MCP8-2000 suggests the presence of structural disorder caused by defects, functionalization, or incomplete graphitization. The arrangement of disordered graphene layers and the enlarged interlayer distance indicate abundant porosity and structural versatility. These findings suggest that high-temperature treatment induces long-range graphene orientation while retaining defects that are essential for efficient Pt deposition on the carbon surface via ALD. Nevertheless, Fig. S10 shows the N2 gas sorption and pore size distribution of MCP8 after the 2000 °C treatment and Table 1 presents the BET and microporous surface areas of both carbons, showing a 40% decrease in surface area after heat treatment while retaining the original pore size, which is crucial for preventing Pt dissolution.
| Sample | BET surface area (m2 g−1) | Microporous surface area (m2 g−1) | Pore size (nm) | Pore neck size (nm) |
|---|---|---|---|---|
| MCP8 | 412.5 | 59.1 | 6.4 | 4.8 |
| MCP8-2000 | 241.5 | 17.6 | 6.4 | 4.2 |
Interestingly, the BoL performance in H2/air of Pt/MCP8 and Pt/MCP8-2000 is similar (Fig. 5e), suggesting that the high-temperature treatment has no drastic effect on the overall performance in H2/Air. However, it is worth noting that the BoL performance at low current density is slightly higher in Pt/MCP8 compared with Pt/MCP8-2000 and is comparable with the lower mass activity observed in pure O2 (Fig. S11). This decrease in mass activity is due to the larger Pt NPs (3.25 ± 0.81 nm) that have been observed on MCP8-2000 compared with MCP8 (1.73 ± 0.66 nm), shown in Fig. S12. This is consistent with what has been observed in the literature when Pt is deposited on graphitic, hydrophobic, defect-free, or crystalline carbons, larger nanoparticles are observed.45
To investigate the effect of the high-temperature heat treatment (2000 °C) on overcoming carbon corrosion in Pt/MCP8 MEAs at high potentials, we held the potential at 1.2 V for 40 h under an H2/Ar atmosphere (Fig. 5e). When subjected to this carbon corrosion protocol, the Pt/MCP8-2000 showed no significant performance loss, while a drastic loss in the performance of Pt/MCP8 was observed. This difference could be attributed to that the large number of defect sites in the MCP8, which are susceptible to carbon corrosion and oxidation.46 These processes lead to oxidation to carbon dioxide or surface oxidation (forming oxygen-functional groups) of MCP8, making it more hydrophilic, leading to flooding and loss in the high current density region. In contrast, in the heat-treated, partially graphitized MCP8-2000, there a much fewer defect sites. These defects and edge sites have been reported to be the sites for corrosion.46 These edge sites are composed of oxygen functional groups (also seen in the analysis of XPS, C 1s, Fig. 1c) and hydrogen-terminated edge sites that, when exposed to high potentials, leave the surface as a combination of CO, CO2, H2, and H2O gases (Fig. S13 and Table S3). Hence, the total gas evolved during the temperature-programmed desorption (TPD) can be used as a direct quantification of oxygen functional groups and hydrogen-terminated edge sites. Using this technique, we compared the total gas evolved for the two catalysts, revealing that MCP8-2000 evolved ∼3.5 times less total gas than MCP8, indicating that edge sites in MCP8-2000 are much lower, decreasing the susceptibility to corrosion (Table S3). The total gas evolved (reflecting total oxygen and H-terminated functional groups) from MCP8-2000 is similar to what has been reported for highly oriented pyrolytic graphite (HOPG), suggesting the presence of graphene sheets in the MCP8-2000 (as proven in Fig. 5d).45
000 voltage cycles between 0.6 V and 0.9 V, with holds of 3 s at each voltage) of Pt/MCP8-2000 GDEs with Pt mass loading of 0.3 mg cm−2 were measured. Furthermore, commercial carbon catalyst-coated membranes (Pt/C) with Pt mass loadings of 0.4 mg cm−2 were also tested for both carbon corrosion and Pt dissolution under identical conditions (Fig. 6). The BoL performance of the Pt/MCP8-2000 is as high as that of commercial catalyst-coated membranes (CCM), despite the lower Pt loading of the Pt/MCP8-2000 GDEs (see Fig. 6a and b). The Pt/MCP8-2000 showed 3–7 times lower potential losses (depending on the current density value) compared with commercial CCM due to Pt dissolution after 10
000 cycles (see Fig. 6a–c). The commercial CCM and Pt/MCP8-2000 showed minimal performance loss after 40 hours at 1.2 V (carbon corrosion), while Pt/MCP8 exhibited significant performance loss due to carbon degradation, attributed to its less graphitic structure and higher density of defects and functional groups, which are more susceptible to degradation (see Fig. 6b). Among the three catalysts, MCP8-2000 offers minimal performance losses after Pt dissolution and carbon corrosion, compared with the Pt/MCP8 GDE and commercial CCM (see Fig. 6c and d). Most of the voltage loss in the Pt/MCP8-2000 CL is at low current density and might be attributed to agglomeration and a decrease in mass activity after 10
000 cycles of Pt dissolution (see Fig. 5c). TEM images were obtained to investigate the change in Pt NPs in Pt/MCP8-2000 after Pt dissolution (10
000 cycles) and carbon corrosion (40 hours at 1.2 V) tests. The TEM images show a 30% increase in particle size, with the average particle growing from 3.25 ± 0.81 nm to 4.26 ± 1.15 nm, as shown in Fig. S14. Moreover, the Pt particle size increases by the same percentage when carbon corrosion and Pt dissolution protocols are applied.
000 cycles of Pt dissolution, which the United States Department of Energy (DOE) requires for high-duty vehicle applications.4 To complement the comparison with the commercial CCM shown in Fig. 6, Fig. 7a benchmarks the Pt/MCP8-2000 catalyst against representative Pt and Pt-alloy catalysts reported in the literature,4 especially at low current density. For example, Liu et al.20 reported minimal performance loss at 1.5 A cm−2 after 90
000 AST cycles due to Pt dissolution, their study does not address degradation from carbon corrosion—a key factor in catalyst layer stability and device lifetime. Additionally, their H2/air performance (∼1.8 A cm−2@0.6 V) was achieved at 94 °C, 250 kPaabs, and 100% RH. In contrast, our study achieved higher performance (∼2.4 A cm−2@0.6 V) at lower temperature (80 °C) and pressure (150 kPaabs), demonstrating a rare combination of high performance, Pt dissolution resistance, and carbon corrosion durability in a purely Pt-based catalyst layer.
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| Fig. 7 A single PEMFC performance and key performance indicators (KPIs) comparison with previously reported studies and 2025 DOE targets. (a) H2/air performance (non-IR-corrected) of MEAs of this work (Pt/MCP8-2000; Pt mass loading 0.3 mgPt cm−2) and previously reported Pt/C and PtCo/C (Pt mass loading 0.25 mgPt cm−2)47 at 100% RH, 150 kPaabs, and 80 °C. (b) KPIs of this work compared to the 2025 DOE targets. | ||
We investigated the change in the electrochemical surface area (ECSA) as a function of platinum (Pt) dissolution cycles (Fig. S15). After 90
000 cycles, the ECSA decreased by half. This decrease can be attributed to Pt nanoparticle (NP) agglomeration, with the size of Pt NPs increasing from 2.22 ± 0.66 nm to 4.93 ± 2.02 nm as shown in Fig. S16. The ECSA values exhibit a linear relationship with the number of cycles. This linear trend suggests that the degradation mechanisms remain consistent throughout the cycling process and that degradation likely occurs at a constant rate. Furthermore, it implies that catastrophic secondary mechanisms, such as carbon support collapse, may not be triggered under the given AST conditions, thereby avoiding accelerated degradation.
TEM images and EDS analysis of the cross-section of BoL and EoL Pt/MCP8-2000 GDEs reveal distinct changes, as shown in Fig. S17. At BoL, the cross-section shows a uniform distribution of Pt and Nafion (concentrated on the outside surface of the carbon agglomerate) across the thickness of the catalyst layer. After 90
000 cycles, the Pt band is observed near the membrane and cathode interface, revealing Pt dissolution and diffusion to the membrane (see Fig. S18), contributing to ECSA and the performance losses shown in Fig. 7a. However, no significant Pt agglomeration in the layer is observed, indicating that the performance degradation is mainly caused by the loss of Pt to the membrane. This indicates that the Pt/MCP8-2000 can withstand at least 90
000 cycles before noticeable effects occur. This stability could be for two reasons: (1) the pore confinement effect hinders the Pt agglomeration from the MCP8-2000, and (2) the carbon support itself after 2000 °C heat treatment becomes more graphitic with fewer defect sites (Fig. S13 and S19) and provides Pt with a robust environment that is less susceptible to corrosion.
Finally, we compared the key performance indicators (KPIs) of the Pt/MCP8-2000 GDE with the 2025 DOE targets for heavy-duty applications. MCP8-2000 GDE nearly meets, and even surpasses, some KPIs, such as the DOE targets in efficiency, power density, utilization, and lifetime (see Fig. 7b). The Pt mass loading used in Pt/MCP8-2000 GDE is 0.3 mgPt cm−2 (cathode), and that used in anodic coated membrane (ACM) is 0.1 mgPt cm−2 (anode), giving a total of 0.4 mgPt cm−2. The target for the DOE is 0.3 mgPt cm−2 for both anode and cathode. We used a slightly higher loading (0.3 vs. 0.25 mg cm−2) in the cathode, and used a high anode loading to eliminate any losses that might come from the anode side so that we could closely study the performance and the durability that results from the cathode side.
000 stress cycles. These results exceed the DOE 2025 targets, demonstrating the potential of Pt/MCP8-2000 GDEs to advance the commercialization of PEMFCs for heavy-duty applications. Finally, the effect of pore size and graphitization of the carbon support on mitigating Pt migration and dissolution can be explored in future studies using operando and in situ advanced X-ray synchrotron techniques, such as X-ray fluorescence and X-ray absorption spectroscopy.
To quantify the electrochemical surface area (ECSA), a cyclic voltammogram (CV) between 0.06 and 0.6 V (50 mV s−1) was measured after purging the cathode with Ar. The average current in the capacitive region provided the parasitic H2 crossover current used for background correction. All subsequent electrochemical measurements were carried out at 80 °C, 100% R.H., and 1.5 bar absolute pressure.
Air–H2 polarization curves were measured in 5000 sccm house air with 3 min current holds (U.S. DOE protocol). Throughout the entire testing sequence, 500 sccm H2 (99.999%, Praxair) was flown through the anode at 100% relative humidity. To break in the MEA, a cathode recovery protocol was performed by maintaining a 0.1 V bias for 4 h in air (1000 sccm) at 40 °C and 150% relative humidity (RH).48
The accelerated stress test (square-wave cycles between 0.6 V and 0.95 V with 3 s holds at each potential), was carried out in 1000 sccm H2 and 5000 sccm Ar at 80 °C, 100% RH, and 150 kPa absolute backpressure. For support stability, the cell was held at 1.2 V for 40 hours in H2/Ar at 80 °C and 100% RH. The gas flow was kept at 1000 sccm at anode and cathode and 1.5 bar absolute back pressure.
We estimated the fuel cell lifetime following the study by Peng et al.49 The department of energy (DOE) defines fuel cell lifetime as the operational duration until a 10% reduction in cell voltage at the rated power is observed. To analyze voltage loss, we selected a current density of 1.5 A cm−2, corresponding to the current density at which the targeted rated power is delivered at a rated voltage of 0.67 V. The lifetime of the tested MEA is estimated using the ratio of 10% of the initial voltage (Vinitial) at 1.5 A cm−2 to the voltage loss rate at the same current density, as expressed in the equation below.49 An acceleration factor of 100 (in terms of time) relative to the drive cycle is applied, consistent with prior studies.50 Each complete square-wave cycle spans 6 seconds (3 seconds at 0.60 V and 3 seconds at 0.95 V)
High-temperature programmed desorption (TPD) was performed using an in-house high vacuum apparatus, allowing quantitative detection of gases evolved during the heating of samples to 1800 °C at 10 °C min−1. At these high temperatures, most of the carbon edge sites terminated by H or O were decomposed, forming H2, H2O, CO, and CO2, thus allowing the number of edge sites to be estimated.
X-ray photoelectron spectroscopy (XPS) was conducted using the PHI Versaprobe 4 at Stanford nano shared facility (SNSF) with Al Kα radiation. The PHI instrument-specific relativity sensitivity factors were used and all XPS spectra were obtained from the bare surfaces, without the use of monoatomic argon sputtering. In addition, all XPS spectrums were calibrated employing the adventitious carbon peak at 248.8 eV.
For nitrogen gas sorption, a 3Flex Version 3.01 gas sorption instrument (Canadian foundation for innovation (CFI)) was used to run nitrogen gas sorption analysis and determine the specific surface area and porosity of the carbon samples. 100 mg of carbon powders were used in each measurement. Data were collected at 77 K with prior degassing in N2 at 150 °C for 4 h and then degassing at a pressure lower than 10–3 Torr before the measurements. The specific surface area of the MCP in m2 g−1 was obtained using the Brunauer–Emmett–Teller (BET) plot in the range of 0.05 < P/P0 < 0.3, where P is the N2 partial pressure and P0 is the N2 vapor pressure. The total pore volume was calculated at P/P0 = 0.98, and the pore size distributions were obtained from the adsorption and desorption branches, measured using the Barrett–Joyner–Halenda (BJH) method with Faas correction based on Carbon Black materials.
Transmission electron microscope (TEM) samples were prepared as follows: CCM samples, a 0.5 cm × 0.5 cm portion of the CCMs was cut with scissors Then, the GDL was carefully removed from each MEA using tweezers. A small section of each CCM was embedded in a mixture of resin and hardener in equal parts (obtained from Sigma-Aldrich, USA) and left to solidify overnight, allowing the sample to be prepared for ultramicrotomy. Thin 100 nm sections were sliced using a Leica UCT ultramicrotome setup (Germany) equipped with an Ultra 45°DiATOME knife (USA). These sections were then mounted on multiple 200 mesh Cu/Pd grids.
For imaging of the samples, a Talos F200X STEM (Thermo Fisher Scientific, USA) with a 200 kV electron accelerating voltage and super-X four silicon drift detectors of energy dispersive X-ray spectrometry (Super-X SDD EDXS, Bruker, USA) was utilized. To analyze the catalyst particles, TEM images were captured at 190 k× using the bright field detector. Fiji ImageJ software was used to extract the particle size distribution (PSD), measuring a minimum of 200 platinum particles. EDS maps were obtained on at least 5 different randomly selected regions. STEM-EDS maps of the catalyst layers were collected at 5 k× and 79 k× magnification. The EDS maps were acquired with an electron dose of 2.34 × 104 e-nm−2 and processed using ESPIRIT 1.9 (Bruker, USA) software.
Supplementary information (SI) is available. See DOI: https://doi.org/10.1039/d6ey00019c.
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