Raffael Rameshan1, Lukas Mayr2, Bernhard Klötzer2, Dominik Eder3, Axel Knop-Gericke4, Michael Hävecker4, Raoul Blume4, Robert Schlögl4, Dmitry Y Zemlyanov5, Simon Penner2. 1. Institute of Physical Chemistry, University of Innsbruck , Innrain 80-82, A-6020 Innsbruck, Austria ; Department of Inorganic Chemistry, Fritz-Haber-Institute of the Max-Planck-Society , Faradayweg 4-6, D-14195 Berlin, Germany. 2. Institute of Physical Chemistry, University of Innsbruck , Innrain 80-82, A-6020 Innsbruck, Austria. 3. Institute of Physical Chemistry, University of Münster , Corrensstrasse 28/30, D-48149 Münster, Germany. 4. Department of Inorganic Chemistry, Fritz-Haber-Institute of the Max-Planck-Society , Faradayweg 4-6, D-14195 Berlin, Germany. 5. Birck Nanotechnology Center, Purdue University , 1205 West State Street, West Lafayette, Indiana 47907-2057, United States.
Abstract
In order to simulate solid-oxide fuel cell (SOFC)-related coking mechanisms of Ni, methane-induced surface carbide and carbon growth was studied under close-to-real conditions by synchrotron-based near-ambient-pressure (NAP) X-ray photoelectron spectroscopy (XPS) in the temperature region between 250 and 600 °C. Two complementary polycrystalline Ni samples were used, namely, Ni foam-serving as a model structure for bulk Ni in cermet materials such as Ni/YSZ-and Ni foil. The growth mechanism of graphene/graphite species was found to be closely related to that previously described for ethylene-induced graphene growth on Ni(111). After a sufficiently long "incubation" period of the Ni foam in methane at 0.2 mbar and temperatures around 400 °C, cooling down to ∼250 °C, and keeping the sample at this temperature for 50-60 min, initial formation of a near-surface carbide phase was observed, which exhibited the same spectroscopic fingerprint as the C2H4 induced Ni2C phase on Ni(111). Only in the presence of this carbidic species, subsequent graphene/graphite nucleation and growth was observed. Vice versa, the absence of this species excluded further graphene/graphite formation. At temperatures above 400 °C, decomposition/bulk dissolution of the graphene/graphite phase was observed on the rather "open" surface of the Ni foam. In contrast, Ni foil showed-under otherwise identical conditions-predominant formation of unreactive amorphous carbon, which can only be removed at ≥500 °C by oxidative clean-off. Moreover, the complete suppression of carbide and subsequent graphene/graphite formation by Cu-alloying of the Ni foam and by addition of water to the methane atmosphere was verified.
In order to simulate solid-oxide fuel cell (SOFC)-related coking mechanisms of Ni, methane-induced surface carbide and carbon growth was studied under close-to-real conditions by synchrotron-based near-ambient-pressure (NAP) X-ray photoelectron spectroscopy (XPS) in the temperature region between 250 and 600 °C. Two complementary polycrystalline Ni samples were used, namely, Ni foam-serving as a model structure for bulk Ni in cermet materials such as Ni/YSZ-and Ni foil. The growth mechanism of graphene/graphite species was found to be closely related to that previously described for ethylene-induced graphene growth on Ni(111). After a sufficiently long "incubation" period of the Ni foam in methane at 0.2 mbar and temperatures around 400 °C, cooling down to ∼250 °C, and keeping the sample at this temperature for 50-60 min, initial formation of a near-surface carbide phase was observed, which exhibited the same spectroscopic fingerprint as the C2H4 induced Ni2C phase on Ni(111). Only in the presence of this carbidic species, subsequent graphene/graphite nucleation and growth was observed. Vice versa, the absence of this species excluded further graphene/graphite formation. At temperatures above 400 °C, decomposition/bulk dissolution of the graphene/graphite phase was observed on the rather "open" surface of the Ni foam. In contrast, Ni foil showed-under otherwise identical conditions-predominant formation of unreactive amorphous carbon, which can only be removed at ≥500 °C by oxidative clean-off. Moreover, the complete suppression of carbide and subsequent graphene/graphite formation by Cu-alloying of the Ni foam and by addition of water to the methane atmosphere was verified.
Carbon
surface and interface chemistry represents one of the fastest
evolving and expanding research areas, primarily due to the extraordinary
physicochemical properties of its nanomodifications, especially of
graphene and carbon nanotube materials.[1] Equally important is the function of carbon in heterogeneous catalysis,
where it can be used as tailor-made support with distinct morphological
and surface-chemical properties.[2] A particularly
important topic regarding the role of carbon in catalysis is connected
with metal–carbon interaction, which has been shown to influence
the catalytic activity and selectivity of the catalytic entity, as
shown, e.g., for vinyl acetate synthesis.[3] This necessarily also includes studies on carbon adsorption, (bulk)
migration, metal–carbon compound formation, and carbon dissolution
in metals. It has, for example, been shown how dissolved carbon controls
the initial stages of nanocarbon growth[4] or how a complex surface–bulk diffusional equilibrium affects
the structural and electronic properties of the near-surface regions
of Pdmetal and, in turn, the adsorption and dehydrogenation of ethene.[5] Particularly well-studied is the interaction
of different carbon species with various Ni surfaces in reforming
processes. With respect to the carbon source, in most cases, this
includes the use of methane, as methane dissociation is an important
reaction step in the chemical industry. The steam-reforming process
transforms methane to synthesis gas (CO and H2), which
is of paramount importance for the further reaction to various chemical
products. As this is usually performed over supported Ni catalysts,
knowledge about the elementary reaction steps of methane dissociation,
adsorption/deposition as different (near)-surface species, and finally
the specific reactivities of the latter is imperative. Methane chemisorption
has been studied on a number of metal surfaces and also different
crystal facets of Ni, and data on the thermal and molecular beam deduced
sticking coefficients are readily available.[6,7] The
most interesting feature, which has so far only been studied on well-defined
Ni single-crystalline samples using ethylene or acetylene as a carbon
source, refers to the preferential growth of carbidic and grapheneC species after dissociative hydrocarbon adsorption.[8] Usually performed at high temperatures (400–650
°C), the corresponding hydrocarbon species is decomposed and
atomic carbon diffuses into the Ni surface. Upon reaching a carbon
content of ∼0.45 ML, the Ni surface reconstructs and forms
a surface carbide of composition Ni2C.[9] The formation, stability, and reactivity of this phase
are of particular importance for the subsequent formation of the recently
well-studied graphene/graphite layers. The formation mechanism of
the latter in the presence (or in expense) of the carbide, and the
particular structural role of the carbide for graphene growth, is
controversially discussed.[10−12] Patera et al.[11] discuss a temperature-dependent graphene growth mechanism
in ethylene, switching from in-plane single layer (previously introduced
by[12]) or two-layer carbide conversion below
∼500 °C to a direct conversion mechanism without intermediate
carbide above 500 °C. Whereas at T < 500
°C only epitaxial unrotated graphene directly attached to bulk
Ni(111) was observed after conversion, both rotated and unrotated
graphene domains were observed above 500 °C. Alternatively, simultaneous
presence of Ni2C and rotated graphene domains as a layered
structure, resulting from toluene decomposition, has been reported,
identifying Ni2C as a source of graphenegrain rotation.[13]The limited applicability of these studies
to real (electrode)
catalytic processes arises from the fact that they are exclusively
performed on highly ordered, single crystalline model systems with
particularily “sticky” hydrocarbon molecules such as
ethene. Related experiments on realistic systems with more “open”,
structurally imperfect, and thus more “bulk diffusion friendly”
surfaces appear to be still scarce. Also, the use of technologically
more relevant carbon source molecules, especially of methane, is interesting.Hence, our primary aim is to present a thorough study of methane
dissociation and carbon growth, suppression and dissolution on a porous
Ni foam sample and polycrystalline Ni foil. Since C deposition and
whisker growth is a serious issue also on Ni/YSZ cermet anodes of
SOFCs,[14] the Ni foam sample is also regarded
as a model system for the interconnected bulk Ni network of the commercial
Ni/YSZ cermet materials, exhibiting mesoscopic porosity and a high
fraction of curved surface area. A major problem of Ni/YSZ cermet
anodes, especially upon “dry” admission of the hydrocarbon
fuel to the cell at typical operation temperatures above 600 °C,
is the ability of Ni to incorporate and resegregate large amounts
of carbon into/out of its structure, eventually inducing the growth
of carbon filaments and in turn causing electrode failure by anode
fracture and short-circuiting of the entire cell.[14]To overcome the much lower sticking probability of
methane (as
compared to ethene, etc.), near ambient pressure XPS spectroscopy
(NAP-XPS) is the appropriate technique, since methane pressures up
to 1 mbar can be used and the growth process can be studied under
close-to-real conditions in situ. Ni-coking is more an issue, the
slower the deposited carbon is reacted
off the Ni surface either by direct electrooxidation at the three-phase
boundary or by internal reforming of methane with water toward CO/H2. Hence, particular emphasis will also be given to eventual
and substantial suppression of carbon growth by directional surface
doping and chemical modification. In the present contribution, these
will include doping of the Ni surface with Cu and adding steam to
the reaction mixture. The Ni foil was used as a reference sample covering
the “materials” gap between Ni single crystals and the
foam.
Experimental Section
The in situ NAP-XPS
system[15] at the
beamline ISISS-PGM of BESSY II allowed us to perform in situ photoelectron
spectroscopy up to 1 mbar total reactant pressure. It is equipped
with differentially pumped electrostatic lenses and a SPECS hemispherical
analyzer. The sample is positioned inside the near ambient-pressure
chamber 2 mm away from a 1 mm aperture, which is the entrance to the
lens system separating gas molecules from photoelectrons. Binding
energies (BEs) were generally referred to the Fermi edge recorded
after each core level measurement. In general, equal photoelectron
kinetic energy and thus information depth for the different XPS signals
was realized by tuning the photon energy (monochromator) to the respective
value. The respective photon energy dependent XPS cross sections were
derived from ref (16).Samples were mounted on a transferable sapphire holder. The
temperature
was measured by a K-type chromel/alumel thermocouple spot-welded to
the side of the sample, and temperature-programmed heating was ensured
by an IR laser from the rear. In the case that the Ni-foam was investigated,
it was heated indirectly from the back via a Ni foil support, making
sure that the latter was geometrically “invisible” for
the spectrometer. The initial sample cleaning procedure consisted
of repeated cycles of Ar+ sputtering for 15 min at room
temperature, exposure to 0.2 mbar O2 at 500 °C, followed
by exposure to 0.2 mbar H2 at 500 °C, and in some
cases an additional flash anneal cycle to ∼650 °C in a
vacuum. After this treatment, cleanliness was checked by XPS. In order
to induce carbon growth at the surface, the sample was then exposed
to 0.2 mbar methane within ∼15 min at 400 °C. The temperature
was thereafter lowered to and kept at 250 °C (still at 0.2 mbar)
for 30 min. Eventually the methane pressure was decreased to 0.02
mbar in order to follow the carbon growth kinetics with sufficient
time resolution.In order to prepare a Ni:Cu = 1:1 near surface
alloy, 5 ML of Cu
were thermally evaporated by means of an electron beam PVD source.
Stepwise annealing up to 400 °C in UHV allowed an ∼1:1
atomic Ni:Cu ratio to be attained within the near-surface layers,
as derived from the ratio of the cross-section-corrected Ni 2p and
Cu 2p areas.
Results
Growth
of Distinct Carbonaceous Species on
Ni Foam and Ni Foil in Clean CH4
As already outlined
in the Introduction section and will be further
discussed below, the role of the surface carbide for the subsequent
growth of the graphene/graphite layers was not fully understood. On
this basis and to induce the relevant surface species under question,
dedicated pretreatments in methane with respect to sample temperature
and methane partial pressure were chosen. After the cleaning procedure,
the carbon supersaturation of the near-surface regions, being inevitable
to induce the subsequent growth of both carbidic and graphene carbon
species, was provided. The respective detailed experimental procedure
is described in the preceding Experimental Section.Figure shows
the XPS spectra of methane-induced carbon growth on the Ni foam at
0.02 mbar in the temperature range around 250 °C after the above-described
pretreatment. As can be deduced from the translational/rotational
and surface temperature resolved molecular beam adsorption study on
Ni(100) by Chorkendorff et al.,[7] under
the experimental conditions presented in this work, a lower limit
of the thermal sticking coefficient stherm of methane between 10–7 and 10–8 can be estimated for exposures around 250 °C, whereas, for
the pretreatment at 400 °C, stherm is estimated to be ∼10–6. Likely, the structural
“openness” of the foam surface and the simultaneous
influence of the intense X-ray beam favor a higher sticking probability.
At a pressure of 0.2 mbar/20 Pa, the impingement rate of CH4 amounts to ∼7 × 1019 cm–2 s–1 at ∼100 °C estimated gas temperature
between nozzle and sample surface. With an assumed sticking probability stherm around 10–6 at 400 °C
and 10–7 at 250 °C, this corresponds to a carbon
deposition rate of ∼7 × 1014 and ∼7
× 1013 C atoms cm–2 s–1, respectively. Assuming a mean number density of ∼2 ×
1015 Ni atoms/cm2, this yields ∼0.35
ML s–1 carbon for 15 min at 400 °C and ∼0.035
ML s–1 for 30 min at 250 °C. In total, the
sample was already exposed to ∼380 ML carbon before reducing
the methane pressure to 0.02 mbar, which is regarded as an important
prerequisite for sufficient supersaturation of the near-surface regions
with dissolved C. In comparison, Patera et al.[11] used ∼5 × 10–7 mbar ethylene
as a carbon source on Ni(111) at 400 °C and observed almost immediate
formation of the Ni2C surface carbide. However, in order
to induce the onset of graphene growth, a further 14 min at 400 °C
were required, corresponding to roughly 100 ML carbon “preexposure”.
Figure 1
Selected in situ X-ray
photoelectron spectra of the C 1s region
obtained during exposure of the Ni foam to 0.02 mbar methane at 250
°C at a photon energy of 425 eV. Sample pretreatment: Heating
in O2 to 500 °C (0.1 mbar), followed by reduction
in hydrogen at 500 °C (0.1 mbar), switching to methane at 400
°C (0.2 mbar), cooling in methane to 250 °C (0.2 mbar).
After this pretreatment routine, the methane pressure was reduced
to 0.02 mbar at 250 °C to obtain a better time resolution of
the carbide/graphene/graphitic carbon growth process. The gas phase
signal was deliberately suppressed by applying a voltage of −10
V between the sample and the nozzle to the differentially pumped lens
system. This leads to a moderate increase in noise signal, but the
gas phase contribution is largely suppressed.
After an additional isothermal period at 0.02 mbar and 250 °C
for a further 30 min, corresponding to 6 additional ML of carbon,
the last spectrum without measurable carbon intensity with respect
to the unequivocal presence of either carbidic or graphite/graphene
species in the near-surface regions (termed “onset”)
could be collected. Reduction of the methane pressure turned out to
be essential to follow the kinetics of carbon growth in a resolvable
time scale by XPS, as will be shown below. After a short period of
time (84 s), a small carbon feature at a binding energy of 283.3 eV
appears, which increases with further exposure time, as indicated
in Figures and 2. This feature is found at almost exactly the same
BE position as the species indicated by Weatherup et al.[9] on polycrystalline Ni films and Patera et al.[11] on Ni(111) after exposure to ethylene (283.2
eV). It was originally associated in ref (9) with the presence of distinctly bonded carbon
atoms on the Ni surface, but subsequently in ref (11), it was reassigned (on
the basis of complementary STM and LEED) to carbon within the Ni2C clock reconstructed surface carbide. It is worth noting
that, a few minutes after the appearance of this first feature, a
second component at higher binding energy arises. This species, found
at ∼284.2 eV, steeply increases upon raising exposure time
and is assigned in analogy to ref (11) to sp2-hybridized graphene/graphitic
carbon. In contrast, the carbidic species reaches saturation after
roughly 20 min (growing to ∼80% intensity in 7 min and slowly
saturating after 20 min), while the graphene/graphitic signal still
grows. This trend is even valid for prolonged exposure times, although
the growth rate of the graphite/graphene species slows down (after
2 h 30 min, Figure last spectrum and Figure ).
Figure 2
Detailed view of in situ XPS spectra shown
in Figure , highlighting
the initial
stages of simultaneous carbide/graphene growth. Experimental conditions
as outlined in Figure .
Figure 6
Plot of the relative contribution of carbidic precursor
and the
graphene/graphite layer to the total carbon signal (above) and plot
of the total C 1s carbide and graphene/graphite area (below) during
growth and dissolution. Note that the temperature during growth (left
panel) is 250 °C but that the temperature is ramped during the
dissolution process (right panel). Different intensity scales have
been used for carbide and graphite C 1s areas.
Interestingly, upon apparent suppression of the carbide
signal
after longer exposure times and in particular at higher temperatures,
the further graphene/graphite growth stagnates. Dissolution of the
carbide into the Ni bulk, along with a possible damping effect of
graphite/graphene overlayers with respect to the photoelectrons from
the coexisting carbide species, will be discussed below (cf. Figure ).We note
as a general observation that the presence of a sufficiently
intense carbidic “precursor” signal is quite obviously
a prerequisite both for the appearance and for the growth of the second,
graphene/graphitic, species. The growth of the latter has never been
observed in any of our experiments—which were all conducted
well below 500 °C—without the simultaneous presence of
“carbon-rich” carbide. This is again in agreement with
the in situ data by Patera et al.,[11] showing
that a clean Ni(111) surface exposed to ethylene below 500 °C
predominantly shows an initial Ni2C reconstruction, which
converts into monolayer graphene either via an in-plane mechanism[12] or via an additionally discussed two-layer “carbon-rich”
carbide–graphene conversion mechanism.[11] As, upon several attempts to induce graphene/graphite growth under
slightly altered conditions, a rather weak carbide precursor signal
was occasionally observed, but subsequently decreased again and vanished
shortly after observation without any graphene/graphite nucleation,
we suggest that the carbidic precursor needs to reach a certain concentration
to become both stable and sufficiently C-supersaturated to allow for
graphene/graphite nucleation. In summary, if the precursor is present
in a sufficiently C-rich form, it apparently acts as a template for
the subsequent growth of graphene/graphite. If the temperature exceeds
350 °C but stays below 400 °C, the carbidic precursor is
preferentially dissolved (see also Figure ); however, the graphene/graphite layers
stay intact without further growth. If this “graphene/graphite-only”
state is recooled to the initial temperature conditions of precursor
growth, no carbide and, thus, no additional graphite/graphene can
grow. Only if the carbon is quantitatively removed from the surface,
the carbidic precursor can grow again.Selected in situ X-ray
photoelectron spectra of the C 1s region
obtained during exposure of the Ni foam to 0.02 mbar methane at 250
°C at a photon energy of 425 eV. Sample pretreatment: Heating
in O2 to 500 °C (0.1 mbar), followed by reduction
in hydrogen at 500 °C (0.1 mbar), switching to methane at 400
°C (0.2 mbar), cooling in methane to 250 °C (0.2 mbar).
After this pretreatment routine, the methane pressure was reduced
to 0.02 mbar at 250 °C to obtain a better time resolution of
the carbide/graphene/graphitic carbon growth process. The gas phase
signal was deliberately suppressed by applying a voltage of −10
V between the sample and the nozzle to the differentially pumped lens
system. This leads to a moderate increase in noise signal, but the
gas phase contribution is largely suppressed.To highlight the initial stages of graphene nucleation, the
XPS
spectra showing the coexistence of carbidic and graphene/graphitic
carbon are shown in Figure in more detail. The evolution of the second carbon component
is clearly visible, as well as the beginning saturation of the carbidic
precursor species. We also note that, upon increasing the temperature
well above 350 °C, the formation of the carbidic precursor species
is effectively suppressed also on the clean Ni surface, at least on
the time scale of our experiments.Detailed view of in situ XPS spectra shown
in Figure , highlighting
the initial
stages of simultaneous carbide/graphene growth. Experimental conditions
as outlined in Figure .For comparison, Figure shows the corresponding experiments
on a polycrystalline
Ni foil. Sample pretreatment is exactly the same as specified for
the Ni foam. After the pretreatment, the carbidic precursor signal
is already present at 250 °C (“onset” spectrum
at 0 min, at a binding energy of 283.4 eV), although this time it
obviously coexists with a comparably large amount of amorphous (or
“adventitious”) carbon with respect to carbidic/graphene/graphite
species (∼0.5 ML vs ∼0.1 ML), as indicated by the broad
background with an intensity maximum around 284.0 eV. However, compared
to the Ni 2p signal, this represents only modest amounts: the total
C 1s signal corresponds to ∼0.6 ML. With increasing sample
temperature and time, the small fraction of the graphene/graphitic
carbon species at 284.2 eV increases and the carbidic precursor is
decomposed. Again, in this stage, the further growth of the graphene/graphitic
type carbon is inhibited, in full analogy to the foam material. Note
that the decrease of the carbidic precursor is most likely due to
decomposition and not just due to photoelectron shielding by the other,
coexisting, carbon species, as the total amount of the latter is far
too low to fully shield the carbide species, even if they were part
of a “layered” scenario (using the overlayer model described
in the Discussion section with an integral
carbon coverage of ∼0.6 ML). Obviously, the “adventitious”
carbon of the strongly dominant background signal represents a comparably
unreactive form of carbon. It is quickly formed already at the beginning
of the methane exposure but then essentially remains unaltered up
to the highest temperature (375 °C). As all experimental parameters
were exactly the same as, e.g., in the foam experiments of Figures and 2, where hardly any contribution of the adventitious carbon
is detectable, its far higher abundance on the foil presently remains
unclear. It may be related to poorer carbon bulk diffusion properties
of the foil sample (high temperature treated metal foils frequently
exhibit large grains with low-index terminal crystallite faces such
as (111) and (100), and only a small fraction of curved (high-index)
surfaces). Since it covers a very broad BE range, not only structural
but also strong chemical heterogeneity (possibly also from C–O
containing species around 287 eV at a lower amount to carbidic contributions
around 281 eV) can be assumed.
Figure 3
In situ X-ray photoelectron spectra of
the C 1s region obtained
during exposure of the Ni foil to 0.02 mbar methane at the indicated
temperatures after sample pretreatment as described in Figure . Photon energy: 425 eV. Amorphous
background shown (A) and subtracted from spectra (B) as it does not
participate in the carbide/graphene kinetics in the chosen temperature
region.
In situ X-ray photoelectron spectra of
the C 1s region obtained
during exposure of the Ni foil to 0.02 mbar methane at the indicated
temperatures after sample pretreatment as described in Figure . Photon energy: 425 eV. Amorphous
background shown (A) and subtracted from spectra (B) as it does not
participate in the carbide/graphene kinetics in the chosen temperature
region.In order to evaluate thermally
induced changes and the overall
stability of the graphene/graphite species growing at around 250–300
°C on the foam sample, the evolution of the C 1s, Ni 2p, and
O 1s spectra was measured in 0.02 mbar pure methane in the temperature
range from 250 to 600 °C.In situ X-ray photoelectron spectra of
the C 1s (A), Ni 2p (B),
and O 1s (C) regions obtained during exposure of the Ni foam to 0.02
mbar methane at the indicated temperatures after the standard sample
pretreatment described in Figure . Photon energies: 425 eV (C 1s), 1010 eV (Ni 2p),
680 eV (O 1s). Collecting one set of C 1s, Ni 2p, and O 1s at a given
temperature takes ca. 30 min.As shown in Figure A, up to 300 °C, no nucleation of graphene/graphite took
place
on the (in the case of Figure shorter) experimental time scale (only carbidiccarbon at
283.4 eV, hardly any intensity at 284.2 eV). At and above 300 °C,
the sudden onset and fast growth of graphene/graphitic carbon leads
to a maximum intensity of the 284.2 eV signal (350 °C spectrum).
Above 350 °C, this intensity trend is reversed, and at 450 °C,
a clear decrease of the graphene/graphite related intensity is already
observable. Complete loss of the graphene/graphite signal is eventually
observed at and above 550 °C. Note that in comparison to Figure a relatively higher
amount of unreactive adventitious carbon has been observed (detailed
discussion with respect to Figure ). Although unreactive and obviously not participating
in the reaction, this difference might arise from the frequency of
methane supply line purging, leading to variable cleanliness of the
latter. The trend of the related O 1s spectra (Figure C) indicates little changes up to 400 °C,
but at and above 450 °C, the oxygen content of the surface increases,
despite the pure methane atmosphere. We assign this increase to segregation
of predissolved oxygen from the Ni bulk, since the initial cleaning
treatment involved oxidation at elevated pressures and temperatures
(0.2 mbar O2 treatment at 500 °C followed by H2) but no subsequent vacuum annealing to 650 °C. Note
that the O 1s peak only develops one single component at ∼529.5
eV, excluding hydroxylated forms of Ni2+, which were clearly
observed in the methane/water experiments described in section . The increasing
oxidation of the surface is also reflected in the corresponding Ni
2p spectra (Figure B) by slight changes of the satellite region around 858 eV. A changed
weighting of the 852.7 eV + 3.7 eV and + 6 eV satellites (surface
plasmon related, see ref (17)) due to adsorbed oxygen appears likely on the basis of
similar Ni 2p spectra obtained after O2 chemisorption.[18] Alternatively, a small contribution of surface
NiO (at ∼855.5 eV) could also contribute to the observed changes.[19−21]
Figure 4
In situ X-ray photoelectron spectra of
the C 1s (A), Ni 2p (B),
and O 1s (C) regions obtained during exposure of the Ni foam to 0.02
mbar methane at the indicated temperatures after the standard sample
pretreatment described in Figure . Photon energies: 425 eV (C 1s), 1010 eV (Ni 2p),
680 eV (O 1s). Collecting one set of C 1s, Ni 2p, and O 1s at a given
temperature takes ca. 30 min.
The general conclusion from Figure is that a combination of C dissolution at T ≥ 400 °C and clean off by oxygen, becoming
mobile above 450 °C, can cause the observed decrease of the C
1s signal. That C redissolution is an active process already at temperatures
around 400 °C will be shown in more detail in the following section in the context of Figures and 6.
Figure 5
In situ X-ray photoelectron
spectra of the C 1s region obtained
during exposure of the initially graphene/graphite covered Ni foam
to 0.02 mbar methane at sample temperatures between 390 and 470 °C.
Sample cleaning pretreatment in O2/H2 as in Figure , followed by an
additional thermal annealing step in a vacuum at 650 °C. Afterward,
exposure to 0.2 mbar methane at 500 °C, cooling to 250 °C,
and exposure to 0.02 mbar methane until the full graphene/graphite
C 1s intensity at 284.3 eV was reached. The photon energy for C 1s
and for O 1s was 425 and 680 eV, correspondingly. The O 1s spectra
are shown as an inset.
Carbon Dissolution
Equally interesting
as the growth of the different carbon species is the fate of each
of these at higher temperatures, in particular the predominant mechanism
of removal. Possible pathways are decomposition/dissolution and/or
reactive clean-off by resegregation of dissolved oxygen, as discussed
above. The latter was deliberately diminished in the experiments of Figures and 6 by applying an additional thermal annealing step at 650 °C
in a vacuum after the oxygen/hydrogen cleaning treatment at 500 °C.
During the subsequent heating experiments of the Ni foam and Ni foil
samples, both were treated in 0.02 mbar pure methane during the entire
experiment while recording the C 1s spectra. To ensure the reduced
oxygen resegregation, additional O 1s spectra between the initial
390 °C and after almost complete C dissolution at 470 °C
were also recorded, which are shown as an inset in Figure and show a rather small and
constant intensity (in contrast to Figure C).Starting out with the maximum graphene/graphite
coverage obtained at 250 °C on the Ni foam (similar initial state
as the red spectrum after 2 h 31 min in Figure , with a still visible 283.4 eV shoulder
of the carbidic precursor contribution), further increase of the temperature
to 390 °C at first leads to the complete dissolution of the precursor,
as confirmed by the loss of the shoulder. The intensity of the graphene/graphitic
carbon component then stagnates at around 390 °C. Therefore,
the 390 °C spectrum in Figure is associated with the “onset temperature”
of the dissolution process. Above 400 °C, the intensity of the
sp2-hybridized graphene/graphitic component starts to shrink
as well. Note that the temperature was switched from 390 to 410 °C
and then back to 400 °C before it was finally increased to 470
°C. The purpose of this temperature loop was to accurately determine
the thermal stability range of the graphene/graphitic carbon species.
At 390 °C, it is still stable but clearly starts to decompose
at 410 °C (red and orange spectra). Therefore, the temperature
was lowered to 400 °C to deliberately slow down the decomposition
process. As can be seen by comparison of the spectra taken isothermally
at 400 °C (light and olive green traces), the dissolution process
becomes slower but is still progressing. Upon raising the temperature
to 470 °C, the process strongly accelerates, leading to almost
complete decomposition/dissolution of the initial graphene/graphite
coverage after 2 h 45 min at this temperature.In situ X-ray photoelectron
spectra of the C 1s region obtained
during exposure of the initially graphene/graphite covered Ni foam
to 0.02 mbar methane at sample temperatures between 390 and 470 °C.
Sample cleaning pretreatment in O2/H2 as in Figure , followed by an
additional thermal annealing step in a vacuum at 650 °C. Afterward,
exposure to 0.2 mbar methane at 500 °C, cooling to 250 °C,
and exposure to 0.02 mbar methane until the full graphene/graphiteC 1s intensity at 284.3 eV was reached. The photon energy for C 1s
and for O 1s was 425 and 680 eV, correspondingly. The O 1s spectra
are shown as an inset.Figure shows
the
evolution of carbide and graphene/ite on the Ni foam sample as the
percentage of the C 1s signal (above) and as the total component area
(below). Initially, very fast formation of the carbidic precursor
is observed (in 7 min to 80% of maximum carbide signal, reaching a
maximum after ∼20 min). After the carbide signal reaches ∼80%
of its maximal intensity, slow growth of the graphene/ite component
takes place (Figure : the 15 min mark corresponds to Figure upper panel: crossing point of the red and
blue percentage curves). With progressing graphene/graphite growth
at a constant temperature of 250 °C, a slow decrease of the carbide
signal is observed. After ∼3 h (corresponding to time 00:00
on the right side panel) at a isothermal temperature of 250 °C,
the graphene signal almost approaches its maximum intensity. At this
point, the damping of the carbide signal and/or conversion into graphene
is about 50%. From a comparison with a damping calculation based on
a surface layer XPS model (ref (24)), a maximum damping effect of 60% is to be expected. The
damping calculation is based on a “layered” growth model
(ref (13)). In comparison,
the damping effect of graphene/ite and amorphous carbon on the foil
(∼0.6 ML total C) should be 24% using the same calculation
(as the data are normalized to the cross section, a direct and comparative
judgment is now possible). Note that an in plane conversion model
(as suggested in ref (11)) would cause a similar effect by replacement of carbide by graphene.
The data presented in Figure therefore do not allow one to distinguish between these mechanistic
scenarios quantitatively. In principle, a superposition of a damping
overlayer and the in plane conversion mechanism is conceivable.Author: After starting the temperature-programmed experiments,
the eventual loss of carbide intensity (03:00 h + 00:45 h, temperature
increase from 370 to 390 °C) can be clearly assigned to full
carbide dissolution and/or conversion to graphene. Only if a temperature
of 400 °C is exceeded, the dissolution of graphene starts and
is complete at 03:00 h + 02:00 h at 470 °C despite ongoing supply
of CH4 from the gas phase. As stated above, deliberate
acceleration and slowing down of the dissolution process can be achieved
by changing the annealing temperature, provided the critical temperature
of 390 °C is overcome (Figure ). Isothermal treatments
at 420 °C therefore cause a slower dissolution, a temperature
increase to 430–450 °C a strong acceleration of carbon
dissolution.Plot of the relative contribution of carbidic precursor
and the
graphene/graphite layer to the total carbon signal (above) and plot
of the total C 1s carbide and graphene/graphite area (below) during
growth and dissolution. Note that the temperature during growth (left
panel) is 250 °C but that the temperature is ramped during the
dissolution process (right panel). Different intensity scales have
been used for carbide and graphite C 1s areas.Figure shows
the
analogous C dissolution experiment on the Ni foil, whereby the temperature
range was extended to 375–550 °C. Just as in the related
growth experiment of Figure , the intensity contribution of unreactive adventitious carbon
is much more pronounced than on the foam sample. Nevertheless, the
carbide component is clearly missing already at 375 °C, followed
by a gradual decrease of the graphene/graphitic component between
400 and 550 °C. At the highest temperature, complete dissolution
of the latter is established.
Figure 7
In situ X-ray photoelectron spectra of the C
1s region obtained
during exposure of the initially graphene/graphite/amorphous carbon-covered
Ni foil to 0.02 mbar methane at sample temperatures between 375 and
550 °C. Sample cleaning pretreatment in O2/H2 as in Figure , followed
by an additional thermal annealing step in a vacuum at 650 °C.
Afterward, exposure to 0.2 mbar methane at 500 °C, cooling to
250 °C, and exposure to 0.02 mbar methane until full graphene/graphite/amorphous
C 1s intensity was reached. Photon energy 425 eV. Amorphous background
shown (A) and subtracted from spectra (B) as it does not participate
in the carbide/graphene kinetics in the chosen temperature region.
In situ X-ray photoelectron spectra of the C
1s region obtained
during exposure of the initially graphene/graphite/amorphous carbon-covered
Ni foil to 0.02 mbar methane at sample temperatures between 375 and
550 °C. Sample cleaning pretreatment in O2/H2 as in Figure , followed
by an additional thermal annealing step in a vacuum at 650 °C.
Afterward, exposure to 0.2 mbar methane at 500 °C, cooling to
250 °C, and exposure to 0.02 mbar methane until full graphene/graphite/amorphous
C 1s intensity was reached. Photon energy 425 eV. Amorphous background
shown (A) and subtracted from spectra (B) as it does not participate
in the carbide/graphene kinetics in the chosen temperature region.The results of section lead us to the general
conclusions that the carbon removal
process on the oxygen depleted samples is not due to a clean-off reaction
with O(dissolved)/O(ads), at least not below 470 °C. The sequence
in which the different types of carbon dissolve into the Ni bulk (in
the continuous presence of the methane atmosphere) is, therefore,
the following: The carbidic precursor is dissolved well below 390
°C, followed by the sp2-hybridized graphene/graphitic
carbon at 400–470 °C. The adventitious carbon completely
resists dissolution up to 550 °C and can only be removed by oxidation
in O2. As a further observation, we report that reformation
of the carbidic precursor after cooling back to 250 °C in 0.02
bar methane was neither possible on the (at least spectroscopically)
carbon-depleted foam sample nor on the (still adventitious carbon
covered) foam sample (not shown). Complete carbon removal by recycling
the Ni sample in oxygen and hydrogen and thermal annealing at 650
°C in a vacuum had to be performed to re-establish the growth
of the precursor species.
Suppression of Carbon Growth
As for
technological applications suppression of carbon growth is of paramount
importance (e.g., avoiding the formation of carbon filament on Ni-cermet
anodes in solid-oxide fuel cells), the influence of selected experimental
parameters on the carbon growth kinetics has also been studied. In
particular, this refers to the introduction of a water partial pressure
to the methane gas atmosphere and to chemical changes of the Ni surface
reactivity by doping with Cu.The effects of adding water to
methane are shown in Figure . After the already described standard pretreatment sequence
(15 min Ar+ sputtering, 0.2 mbar O2 at 500 °C,
0.2 mbar H2 at 500 °C, 0.2 mbar methane within ∼15
min at 400 °C, lowering the temperature to and keeping at 250
°C for 30 min, decreasing methane pressure to 0.02 mbar), this
time a water partial pressure of 0.02 mbar was added (CH4 + H2O at 1:1 ratio, 0.04 mbar total pressure). On the
same time scale and at the same temperature (250 °C) as previously
used without water, neither formation of the carbidic precursor nor
formation of the graphene/graphitic carbon species was observed between
250 and 300 °C. Also, a further increase of the total pressure
of the 1:1 methane–water mixture from 0.04 to 0.4 mbar and
variations of the temperature between 250 and 500 °C did not
induce the above-described carbide to graphene/graphite growth mechanism.
Rather, we observed quick formation of a small amount of adventitious
carbon already in the beginning of the experiment, which remained
essentially unreactive up to 500 °C (hardly any intensity variation
in Figure A). Thus,
neither a clean-off reaction of amorphous surface carbon by water
(and/or its dissociation products) nor dissolution of the amorphous
C in the Ni bulk take place. As the C-dissolution works well for the
carbide above 350 °C and for the graphene/graphite deposits above
400 °C, the blocking of the carbide/graphene mechanism is most
obvious in the 350 °C experiment. The corresponding O 1s intensity
increase in Figure C, which is assigned to the simultaneous growth of adsorbed oxygen
(and/or a partial coverage with a NiO surface oxide) together with
a pronounced fraction of Ni-hydroxyl species with temperature (beyond
the single O 1s peaks of Figure C), is most pronounced above 400 °C, which may
be explained by carbon depletion of the surface by a combination of
C-dissolution and reactive clean-off effects. Mass spectrometry of
CO (measured in parallel) suggests that CO formation increases markedly
above 500 °C; thus, the clean-off contribution seems to become
stronger with increasing temperature.
Figure 8
In situ X-ray photoelectron spectra of the C
1s (A), Ni 2p (B),
and O 1s (C) regions obtained during exposure of the Ni foil to a
mixture of methane and water (CH4 + H2O, 1:1
ratio, 0.04 mbar total pressure) at the indicated temperatures after
the standard sample pretreatment described in Figure . Photon energies: 425 eV (C 1s), 1010 eV
(Ni 2p), 680 eV (O 1s).
The component at 529.9
eV can be both O(ads) and NiO,[22,23] and the high BE component
at 531.7 eV is characteristic for hydroxyls
on Ni.[19,23] Apparently, the related oxygen species are
unreactive toward the adventitious carbon residue but could be nevertheless
important for the blocking of the carbide-to-graphene growth mechanism
and/or clean-off of the carbidic/graphene species. The Ni surface
remains largely in the metallic state, as evidenced by the related
Ni 2p spectra in Figure B. In analogy to Figure B, the slight changes of the satellite region around 858 eV
appear to be characteristic for the influence of chemisorbed oxygen[18] and/or minute amounts of surface NiO. In essence,
the Ni 2p region did not show spectral fingerprints characteristic
of larger amounts of bulk NiO, NiO(OH), or Ni(OH)2[17,19] in any of the experiments reported in this work and only spectra
characteristic of metallic Ni with slight indications of surface oxidation/oxygen/hydroxyl
chemisorption were observed.In situ X-ray photoelectron spectra of the C
1s (A), Ni 2p (B),
and O 1s (C) regions obtained during exposure of the Ni foil to a
mixture of methane and water (CH4 + H2O, 1:1
ratio, 0.04 mbar total pressure) at the indicated temperatures after
the standard sample pretreatment described in Figure . Photon energies: 425 eV (C 1s), 1010 eV
(Ni 2p), 680 eV (O 1s).To test the potential of bimetallic doping by Cu for the
suppression
of carbon growth, 5 ML equivalents of Cumetal were deposited on the
Ni foam at 25 °C by means of an electron-beam microevaporator
(measured in situ by a quartz crystal microbalance). Subsequently,
the sample was annealed in a stepwise manner to 400 °C to induce
intermixing of Ni and Cu in the near-surface regions. As a result,
the atomic ratio between Ni and Cu (derived from the ratio of the
cross-section-corrected Ni 2p and Cu 2p signal intensities, which
were measured at ∼120 eV kinetic energy to ensure maximum surface
sensitivity, IMFP ∼ 0.5 nm) was determined to be ∼1:1
within the uppermost 2–3 surface layers. After the standard
sample pretreatment and methane preexposure as described in Figure , no carbon formation
of any kind could be observed during the subsequent exposure to 0.02
mbar pure methane between 250 and 600 °C on a comparable time
scale, as shown in Figure .
Figure 9
In situ X-ray photoelectron spectra of the C 1s region obtained
on the Ni:Cu = 1:1 near-surface alloy in 0.02 mbar methane. Sample
pretreatment as described in Figure followed by methane pressure reduction to 0.02 mbar
at 250 °C. Photon energy: 425 eV.
In situ X-ray photoelectron spectra of the C 1s region obtained
on the Ni:Cu = 1:1 near-surface alloy in 0.02 mbar methane. Sample
pretreatment as described in Figure followed by methane pressure reduction to 0.02 mbar
at 250 °C. Photon energy: 425 eV.Below 400 °C, the Ni:Cu ratio remained at the initial
50:50
ratio, despite the simultaneous presence of CH4. Above
400 °C, a fast increase of the Ni:Cu ratio was observed (Figure ). Nevertheless,
carbon deposition remained completely blocked until 600 °C. The
related O 1s series of spectra did not show any signs of oxygen segregation
to the surface, as previously observed on the pure Ni foam (Figure C). We conclude that
near-surface Cu provides a highly effective adsorption barrier for
methane, in combination with an increased diffusion barrier in both
directions, inward carbon diffusion, and outward oxygen diffusion.
Figure 10
In situ
X-ray photoelectron spectra of the Cu 2p and Ni 2p regions
of the initial 50:50 near-surface NiCu alloy in 0.02 mbar CH4 in the temperature range 200–600 °C.
In situ
X-ray photoelectron spectra of the Cu 2p and Ni 2p regions
of the initial 50:50 near-surface NiCu alloy in 0.02 mbar CH4 in the temperature range 200–600 °C.At the highest temperature (600 °C), the Cu
signal decreases
to almost zero, indicating a change of the surface termination toward
almost clean Ni and/or progressive dissolution of Cu into deeper Ni
layers. This is already a well-established fact and has been reported
to also happen under UHV conditions.[25−29] Similar surface modification processes during methane
decomposition on Cu-promoted Ni–ZrO2 catalysts were
recently reported, concluding that Cu does enhance the desired coking
resistance but only in a certain temperature range. In analogy to
the results of this study, it showed only limited stability under
relevant reaction conditions. Beyond ∼400 °C, surface
segregation of Ni caused a fast increase in methane decomposition
rate.[30] This stability issue will be particularly
important in SOFC anode applications, where temperatures around 800
°C are common. Nevertheless, it appears possible that the bulk-diffusion
blocking function of Cu can be utilized to inhibit the well-known
growth mechanism of C nanofilaments, while still keeping up the advantage
of a catalytically active Ni terminated surface, which is important
for effective internal reforming of the respective fuel. The question
remains open of how the obviously Cu-depleted surface region at 600 °C
can still act as an effective adsorption barrier. As the carbon blocking
effect is an experimental matter of fact, this question can only be
answered by future directed experiments of a similarly Cu-diluted
system (deviating from the 1:1 stoichiometry) treated in methane at
400 °C. Note, however, that at 600 °C under the chosen experimental
conditions (methane pressure) both the precursor and the graphite/graphene
layers are unstable also on the pure Ni foil/foam toward decomposition
and the resulting carbon is dissolved.
Discussion
The focus of this work centers on the investigation of the more
application-relevant graphene/graphitic carbon formation mechanism
from methane at rather low temperatures (250–400 °C) on
“Ni-cermet-like” polycrystalline Ni surfaces and on
comparing these experiments to those on structurally “ideal”
Ni(111) single crystals with sticky hydrocarbons such as ethylene,
acetylene, or toluene. In order to develop a comprehensive model for
the growth, dissolution, and prevention of carbon species on curved
and polycrystalline Ni surfaces, we first needed to calculate the
maximum average thickness of the observed graphene/graphite layers
and subsequently to compare the XPS quantification on the foam with
those reported for Ni single crystals exposed to ethylene. This comparison
should help to clarify the structural and morphological analogies
and discrepancies between the “ideal” and “realistic”
model systems.The carbon film thickness was estimated from
XPS via an attenuated
overlayer model assuming an atomically flat substrate and overlayer
(for details, we refer to ref (31))where
ρ = atom density (cm–3); I = X-ray flux, which varies depending on photon
energy (different photon flux at different photon energy); dσ/dΩ = differential cross section; θ =
photoemission angle measured with respect to the surface normal, 50°; t = overlayer thickness; N = normalized
XPS intensity (peak area); Λ(E) = electron
attenuation length (EAL data from SRD 82 database[32]); indices: s, substrate; l, overlayer/adlayer.To
further corroborate our coverage estimation on the basis of
this model and to back-check its applicability, we utilized a XPS
depth profile analysis recorded at three different photon energies
and thus C 1s kinetic energies and compared the results. This provides
us with three independently determined coverage values for the same
overlayer. Under consideration of the three pairs of Ni 2p and C 1s
peak areas (deduced from Figure , which highlights the spectra obtained from depth
profiling, after background subtraction), we estimated the overlayer
coverage to be 2 ± 0.2 ML (based on the surface atom density
of graphene and Ni(111) and the respective attenuation length; recalculating
to the thickness of the graphite layer yields a value of ∼4.9
Å). Because of the fact that the EAL is effectively an electron
energy-dependent entity, this value is the common solution for all
three resulting electron kinetic energies (150, 350, and 550 eV).
This good compliance for all three pairs of Ni/C spectra supports
the validity of the attenuated overlayer model within certain constraints,
even though there are certain limits for applying it in this system:
(1) One obstacle is the porosity of the foam, which conflicts to some
extent with the restriction of a homogeneous, evenly thick overlayer
(this of course also applies to the used emission angle, which is
50° in the experiments), and (2) residual dissolved carbon in
Ni may still contribute to the C 1s intensity.
Figure 11
In situ X-ray photoelectron
spectra of the C 1s (A) and Ni 2p (B)
regions used for obtaining the depth profile. Sample preparation and
graphene/graphite growth as described in Figure , photoelectron kinetic energies: 150, 350,
and 550 eV. Fits required for background subtraction are also shown.
In situ X-ray photoelectron
spectra of the C 1s (A) and Ni 2p (B)
regions used for obtaining the depth profile. Sample preparation and
graphene/graphite growth as described in Figure , photoelectron kinetic energies: 150, 350,
and 550 eV. Fits required for background subtraction are also shown.Over the past few years, several
groups investigated carbide and
graphene formation on Ni(111) in an ethylene- or toluene gas atmosphere
in the low and intermediate temperature region (∼250–600
°C). A common observation is the initial formation of a C 1s
component at a XPS binding energy of ∼283.3 eV already at low
temperatures around 250 °C and small exposures in the 10–100
L range (Weatherup et al.[9] on polycrystalline
Ni films and Patera et al.[11] on Ni(111)).
This component was originally associated in ref (9) with adsorbed carbon atoms
on the Ni surface but subsequently in ref (11) reassigned (on the basis of STM and LEED) to
carbon within the Ni2C clock reconstructed surface carbide,
an ordered 2D species with coverages of ΘNi = 0.9
and ΘC = 0.45 with respect to the Ni substrate, which
was first described by Klink et al.[10] We
conclude that a related but structurally probably much more heterogeneous
and disordered near-surface carbide phase is initially formed also
on the Ni foam. Obviously, also methane dissociation delivers the
carbon atoms to build a related structure at a comparable rate, but
roughly 5 orders of magnitude higher pressures are required to compensate
for the lower sticking probability relative to ethylene (this holds
at least for the foam sample, on the foil the predominant species
is inactive adventitious carbon). The growth of the ∼284.2
eV component is assigned in analogy to ref (11) to sp2-hybridized graphene/graphitic
carbon. On the basis of the coverage estimation given above, 2 ML
(based on layer distance and surface atom density of Ni(111) would
correspond exactly to a full single layer of graphene, reported also
as C saturation coverage for the Ni(111)/ethylene system).[11] In contrast, the carbidic species reaches saturation
at a lower coverage also in the foam system described herein, while
the graphene/graphitic signal still grows up to 2 ML and fully replaces
the carbide species around 350 °C. Again, in analogy to ref (11), we may discuss the possibility
that complete decomposition of a sufficiently C-supersaturated “metastable”
carbide/dissolved carbon precursor around 350 °C leaves single
graphene layers/flakes on top of Ni metal (in an unknown degree of
order) behind. Consequently, upon suppression of the carbide signal,
the further graphene/graphite growth is expected to stagnate, because
(a) the near-surface regions are depleted of dissolved/carbidiccarbon
feedstock to build graphene and (b) the full graphene layer inhibits
further supply of carbon from the gas phase by blocking methane chemisorption
and lowering its effective sticking probability. Vice versa, the presence
of a sufficiently intense carbidic “precursor” signal
is quite obviously an indication of sufficient supersaturation of
near-surface regions to nucleate and grow graphene/graphitic carbon
patches. The nucleation and growth of the latter has thus never been
observed in any of our experiments—which were all conducted
well below 500 °C—without the simultaneous presence of
a sufficiently strong carbide signal and thus “carbon-rich”
metastable carbide precursor. In this context, we imply an analogy
to the three-dimensional nickel–carbon phase stability diagram
reported in ref (33). Also for the related bulk phases, formation of a metastable Ni3C bulk carbide from a supersaturated solid solution of C in
Ni metal is expected, which becomes unstable well above 500 °C
and is finally converted to the thermodynamically stable graphite
phase and Ni metal with a lower carbon content.We suggest that
the in-plane/two-layer carbide–graphene
conversion mechanisms, which rely on continuous carbon supply from
the gas phase, may in our case also occur in combination with the
“C-contaminated subsurface segregation” mechanism,[11] which operates without continuous carbon supply
and is based on a preexposure-induced, extended subsurface/dissolved
carbon reservoir. This reservoir should in our case also exist beneath
the carbidic surface reconstruction, and thus help to supply the full
carbon amount to form a fully surface-covering 2 ML graphene film.
Nevertheless, without continuous supply of 0.02 mbar methane via the
gas phase, the formation of the full 2 ML graphene coverage has experimentally
not been observed, suggesting a “weighted” combination
of all mechanistic scenarios described in ref (11).Our general conclusion
is that the methane-on-foam growth mechanism
bears strong analogies to the one described for ethylene on Ni(111)
but all individual processes appear to be shifted to at least 100°
lower temperatures, likely due to the “open” structure
of the curved foam surface. Structurally, the formation of a single
graphene layer or disordered flakes/patches on the foam is obviously
difficult to proof by modern high-end electron microscopic techniques
and/or STM. Thus, we cannot exclude a high degree of disorder and
heterogeneity in the graphene film coexisting, e.g., with thin patches
of disorderedgraphite, which may extend over a few layers. At rather
high carbon supersaturations of polycrystalline Ni, the nucleation
of rotated graphene domains in multilayer graphene by decoupling of
the layers from the Ni surface has been recently shown on the basis
of postgrowth STM data.[34]
Conclusions
It has been shown that the initial formation
of a sufficiently
C-supersaturated carbidic/dissolved carbon phase is a necessary precondition
for the nucleation and growth of graphene/graphitic carbon on Ni foam
already at lower temperatures than usually applied on Ni(111) (<400
°C). Any chemical surface modification which inhibits the buildup
of this precursor state, or at least lowers its C-content below a
critical value, necessarily also inhibits graphene/ite growth. Addition
of H2O effectively suppresses the initial formation of
the precursor and thus the fundamental growth condition for graphene.
The same holds for already present carbon deposits such as “adventitious”
carbon and, of course, bimetallic dopants such as Cu alloyed into
Ni. Thus, a broad choice of structural and chemical modifications
of the Ni surface opens up exciting possibilities to circumvent pending
problems in technological applications such as coking of the Ni anode
catalyst surface of SOFCs and associated formation of deleterious
carbon nanofilaments.
Authors: Ali Rinaldi; Jean-Philippe Tessonnier; Manfred E Schuster; Raoul Blume; Frank Girgsdies; Qiang Zhang; Timo Jacob; Sharifah Bee Abd Hamid; Dang Sheng Su; Robert Schlögl Journal: Angew Chem Int Ed Engl Date: 2011-02-24 Impact factor: 15.336
Authors: Robert S Weatherup; Bernhard C Bayer; Raoul Blume; Caterina Ducati; Carsten Baehtz; Robert Schlögl; Stephan Hofmann Journal: Nano Lett Date: 2011-09-16 Impact factor: 11.189
Authors: Peter Jacobson; Bernhard Stöger; Andreas Garhofer; Gareth S Parkinson; Michael Schmid; Roman Caudillo; Florian Mittendorfer; Josef Redinger; Ulrike Diebold Journal: ACS Nano Date: 2012-03-20 Impact factor: 15.881
Authors: Laerte L Patera; Cristina Africh; Robert S Weatherup; Raoul Blume; Sunil Bhardwaj; Carla Castellarin-Cudia; Axel Knop-Gericke; Robert Schloegl; Giovanni Comelli; Stephan Hofmann; Cinzia Cepek Journal: ACS Nano Date: 2013-08-15 Impact factor: 15.881
Authors: Harald Gabasch; Konrad Hayek; Bernhard Klötzer; Axel Knop-Gericke; Robert Schlögl Journal: J Phys Chem B Date: 2006-03-16 Impact factor: 2.991
Authors: Robert S Weatherup; Carsten Baehtz; Bruno Dlubak; Bernhard C Bayer; Piran R Kidambi; Raoul Blume; Robert Schloegl; Stephan Hofmann Journal: Nano Lett Date: 2013-09-27 Impact factor: 11.189