2012
DOI: 10.1016/j.jpowsour.2012.06.015
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Comparative DEMS study on the electrochemical oxidation of carbon blacks

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Cited by 58 publications
(62 citation statements)
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“…Figure 4D) from a BOL value of ≈38 μm/(mg Pt cm −2 ) (or ≈33 μm/(mg C cm −2 ), which agrees with the 28 ± 2 μm/(mg C cm −2 ) reported in literature) 36 to ≈23 μm/(mg Pt cm −2 ) and points to a collapse of the CL structure which can inhibit effective mass transport of reactants and that is supported by the drastic performance decline in the H 2 /air I/E curves in Figure 2A. The CL collapse can be attributed to carbon support corrosion in the applied potential regimes [20][21][22]37,38 and the resulting CL porosity decrease has been demonstrated by Schulenburg et al 39 in a FIB-SEM tomography study. On the other hand, representative cross section images before/after the load-cycle AST (Figures 3D/3F) do not indicate significant morphology/porosity changes concomitant with the negligible decrease in thickness to ≈34 μm/(mg Pt cm −2 ) discernable from Figure 4B.…”
Section: Resultssupporting
confidence: 90%
“…Figure 4D) from a BOL value of ≈38 μm/(mg Pt cm −2 ) (or ≈33 μm/(mg C cm −2 ), which agrees with the 28 ± 2 μm/(mg C cm −2 ) reported in literature) 36 to ≈23 μm/(mg Pt cm −2 ) and points to a collapse of the CL structure which can inhibit effective mass transport of reactants and that is supported by the drastic performance decline in the H 2 /air I/E curves in Figure 2A. The CL collapse can be attributed to carbon support corrosion in the applied potential regimes [20][21][22]37,38 and the resulting CL porosity decrease has been demonstrated by Schulenburg et al 39 in a FIB-SEM tomography study. On the other hand, representative cross section images before/after the load-cycle AST (Figures 3D/3F) do not indicate significant morphology/porosity changes concomitant with the negligible decrease in thickness to ≈34 μm/(mg Pt cm −2 ) discernable from Figure 4B.…”
Section: Resultssupporting
confidence: 90%
“…Interestingly decreasing the LPL even further (to 0.05 V RHE ), the CO 2 signal increases dramatically and a significant, almost constant CO 2 signal is observed even at the end of the test cycle. A similar effect was observed independently by Ashton et al 32 and Linse et al 37 Linse et al suggested that below 0.6 V RHE the changes in carbon corrosion behavior cannot be attributed to the catalytic effect of Pt, which is already reduced. Both authors agree that it can originate from modifications in carbon surface oxide composition.…”
Section: Resultssupporting
confidence: 78%
“…The fact that for a MEA with Pt black electrode and gold mesh contacting practically no CO 2 release was observed also is a strong indication that the start-stop cycle ADT does not significantly stress the ionomer neither in the membrane nor the electrode, A surprising result was the finding that the start-stop cycle ADT caused a destabilization of the carbon support, which lead to an increase of the carbon mass loss rates on subsequent operation even if no stress potentials were applied. This can go along with the finding by Ashton and Arenz 9,10 who found that transferring their carbon electrode to low potentials after excursion to high potential caused the formation of reduced oxygenated carbon surface groups which are easier to oxidize than the carbon itself. However, the potentials for which CO 2 release is observed in this work are even lower.…”
Section: Discussionsupporting
confidence: 77%
“…Ashton and Arenz reported on detailed studies of the carbon corrosion of high surface area carbon supports with and without graphitization treatments using DEMS. 9,10 They found that in particular for the non-graphitized support not the entire observed faradaic current caused the release of either CO 2 or O 2 . They therefore postulated that also a partial oxidation of the carbon surface can occur causing either the release of CO or the formation of oxygenated carbon groups at the carbon surface.…”
mentioning
confidence: 99%