High Temperature Corrosion of Cr(III) Coatings in N /0.1%H
Transcript of High Temperature Corrosion of Cr(III) Coatings in N /0.1%H
111
한국표면공학회지J. Korean Inst. Surf. Eng.
Vol. 52, No. 3, 2019.
https://doi.org/10.5695/JKISE.2019.52.3.111<연구논문>
ISSN 1225-8024(Print)
ISSN 2288-8403(Online)
High Temperature Corrosion of Cr(III) Coatings in N2/0.1%H2S Gas
Dong Bok Lee and Shi Yuke*
School of Advanced Materials Science and Engineering, Sungkyunkwan University,
Suwon 16419, Republic of Korea
(Received 26 March, 2019 ; revised 26 April, 2019 ; accepted 9 May, 2019)
ABSTRACT
Chromium was coated on a steel substrate by the Cr(III) electroplating method, and corroded at 500-900oC for 5 h in N2/0.1%H2S-mixed gas to study the high-temperature corrosion behavior of the Cr(III) coatingin the highly corrosive H2S-environment. The coating consisted of (C, O)-supersaturated, nodular chromiumgrains with microcracks. Corrosion was dominated by oxidation owing to thermodynamic stability of oxidescompared to sulfides and nitrides. Corrosion initially led to formation of the thin Cr2O3 layer, below which(S, O)-dissolved, thin, porous region developed. As corrosion progressed, a Fe2Cr2O4 layer formed belowthe Cr2O3 layer. The coating displayed relatively good corrosion resistance due to formation of the Cr2O3
scale and progressive sealing of microcracks.
Keywords : Chromium, carbon, electroplating, H2S corrosion, oxidation
1. Introduction
Chromium electroplating on metal substrates is
widely used in industries owing to its decorative
color, high hardness, and good corrosion resistance. It
is usually performed in the hexavalent chromium (Cr+6
)
bath having CrO3. Shortcomings of Cr(VI) coating are
however low cathode efficiency that results in bad
throwing power, serious health and environmental
problems. To overcome these shortcomings, trivalent
chromium (Cr+3) plating is developed as an alternative
[1]. Coatings of Cr(III) were previously investigated,
including their electroplating condition [2], hardness
[3], wear resistance [4], corrosion resistance [5,6],
electrical contact resistance [7], and high-temperature
oxidation behavior [8]. In this study, Cr(III) coating
was electroplated onto a steel substrate, and corroded
at high temperatures in N2/H2S-mixed gas in order to
study the corrosion behavior of Cr(III) coating in the
serious H2S-containing atmosphere. Since steels
corrodes fast in H2S gas, forming thick FeS scales
incorporated with hydrogen, it is imperative to
develop optimum corrosion-resistant coatings for
steels. H2S comes off as a by-product during
processing in oil refinery, chemical and petrochemical
units, and gasification of fossil fuels [9]. It
dissociates into sulfur and hydrogen. Sulfur reacts
with metals to form nonprotective sulfides, while
hydrogen ingresses into alloys interstitially, forms
hydrogen clusters, increases corrosion rates, and
causes hydrogen embrittlement [9,10]. This study aims
to investigate the high-temperature corrosion behavior
of Cr(III) coating in H2S-environment at high
temperatures in order to find the feasibility of Cr(III)
coating in protecting steels. The microstructural and
compositional variation of the coating during
corrosion was studied.
2. Experimental
Chromium was electroplated on a low carbon steel
substrate (AISI 1024 with a nominal composition of
Fe-0.2C-1.5Mn-0.05S-0.04P in wt%) with a size of
2×0.5×0.3 cm3 to a thickness of 30-100 μm. The bath
composition and electrolysis condition are listed in
*Corresponding Author: Shi Yuke
School of Advanced Materials Science and Engineering,Sungkyunkwan University Tel: +82-3411-290-7355 ; Fax: +82-290-7379E-mail: [email protected]
112 Dong Bok Lee et al./J. Korean Inst. Surf. Eng. 52 (2019) 111-116
Table 1. Bath solution consisted of chromium
sulphate (Cr2(SO4)3·nH2O) as a source of Cr+3
,
complexing agent (HCOOK) that supersaturates
carbon in the Cr coating with an amorphous structure
[5,11], conductive improvement agent (KCl, NH4Cl),
buffer agent (H3BO3), anti-oxidant agent (NH4Br),
and an additive (polyethylene glycol). The surface
area of the anode was twice than that of the cathode.
The prepared samples were charged into the quartz
reaction tube, and corroded at 500-900oC for 5 h in
N2/0.1%H2S-mixed gas in a horizontal tube furnace.
Employed N2 and H2S gases were 99.999% and
99.99% pure, respectively. The samples were
characterized by a field-emission scanning electron
microscope (SEM) equipped with an energy
dispersive spectroscope (EDS), a field-emission
electron probe microanalyzer (EPMA), an X-ray
photoelectron spectrometer (XPS), and a high power
X-ray diffractometer (XRD) with Cu-Kα radiation at
40 kV and 150 mA.
3. Results and Discussion
Figure 1 shows SEM/EDS/XRD/XPS analytical
results of Cr(III) coating. This consisted of nodular
grains with tens of micrometer in size (Fig. 1(a)).
Intense hydrogen evolution during electroplating
generated microcracks inter- and intra-granularly.
Nodular grains grew bigger, and microcracks became
wider and deeper with the increment of plating time
and coating thickness [1,2]. Generation of
microcracks is the major drawback of the Cr(III)
coating. The EDS-analyzed composition of the spot
1, 2, and 3, which were marked in Fig. 1(b), was
69.7Cr-19.3O-11C, 68.5Cr-19.2O-12.3C, and 68.5Cr-
21.6O-10C in at%, respectively (Fig. 1(c)). Although
the quantification of light element such as carbon
was notoriously difficult, Cr, O, and C seemed to be
uniformly distributed in the adherent, microcracked
coating. The amorphous Cr(III) coating displayed a
diffuse pattern around 44o (Fig. 1(d)). It was reported
that supersaturated carbon in the coating precipitated
as chromium carbides such as Cr23C6 [2,11], Cr7C3
[12], and Cr3C2 [13] when annealed at 400-700oC,
being accompanied with increment of the coating
hardness. XPS spectra of Cr, C and O of the coating
are shown in Fig. 1(e). The Cr2p spectrum indicates
that the presence of metallic Cr and Cr2O3. The C1s
spectrum indicated C-C bond (amorphous carbon)
[12,14] and COOH bond [15]. The oxygen
dissolution in the Cr(III) coating made the intensity
of the O1s spectrum high.
Figure 2 shows SEM/EDS/XRD/XPS results of
Cr(III) coating after corrosion at 500oC for 5 h.
Fig. 1. Cr(III) coating. (a) SEM top view, (b) SEMcross-sectional image, (c) EDS spectra of spot 1, 2and 3, (d) XRD pattern, (e) XPS spectra of Cr2P, C1S,and O1S.
Table 1. Bath composition and electrolysis conditions
Bath compositionElectrolysis condition
Chemicals Content
Cr2(SO4)3·nH2O 140 g/l Temperature 30oC
HCOOK 1 M pH 2
KCl, NH4Cl1 M,
respectivelyCurrent density
20 A/dm2
H3BO3 0.65 M Anode graphite
NH4Br 10 g/l Cathodelow carbon
steel
polyethylene glycol
2 g/l Agitation air bubbling
Dong Bok Lee et al./J. Korean Inst. Surf. Eng. 52 (2019) 111-116 113
Microcracks propagated across the coating surface
consisting of nodular grains (Fig. 2(a)). The scale
was hardly recognizable owing to good corrosion
resistance of the coating (Fig. 2(b)). In Fig. 2(c), no
oxides were detected, and the diffuse amorphous
pattern changed to the crystalline Cr pattern. In order
to identify the thin scale that formed on the surface,
XPS analysis was performed, as shown in Fig. 2(d).
The XPS-analyzed composition of the thin scale was
54.7O-17.8Cr-16.7C-9.2Fe-1.3S-0.3N in at%. Here,
the carbon concentration is particularly suspicious,
because carbon signal can come out as a background
noise. Sulfur and nitrogen that originated from N2/
0.1%H2S-mixed gas were apparently dissolved in the
chromia scale, together with Fe, to a small amount.
Iron diffused out from the substrate across the coating.
The Cr2P3/2 peak position was at 576.5 eV,
corresponding to Cr2O3. The C1S peak binding energy
(Eb = 284.7 eV) corresponded to carbon. The O1s
spectrum had a peak (Eb = 530.3 eV), corresponding to
metal oxides. The Fe2P3/2 peak value corresponded to
Fe2O3 (Eb = 710.9 eV). The N1S peak binding energy
(Eb = 399.9 eV) shifted to a higher value than nitrides
(Eb = 396.4-398.3 eV), probably to coexistence of
oxygen and sulfur at the surface. The S1S peak binding
energy (Eb = 168.7 eV) corresponded to sulfate (SO42−).
The corrosion at 600oC for 5 h formed a superficial
scale on the Cr(III) coating (Fig. 3(a)). Here,
microcracks were partially sealed. Figures 3(b-c)
indicates that iron diffused outwardly along
microcracks that were an easy diffusion path. This is
responsible for the partial sealing of microcracks
with oxides of iron and chromium. The oxygen
source for this oxidation reaction was impurity
oxygen in the employed N2/0.1%H2S gas. The
Fig. 2. Cr(III) coating after corrosion at 500oC for 5 h inN2/0.1%H2S gas. (a) SEM top view, (b) SEM cross-sectional image, (c) XRD pattern, (d) XPS spectra ofCr2P, C1S, O1S, Fe2P, N1S, and S2P.
Fig. 3. Cr(III) coating after corrosion at 600oC for 5 h inN2/0.1%H2S gas. (a) SEM top view, (b) SEM cross-sectional image, (c) EDS line profiles along A-Bshown in (b).
114 Dong Bok Lee et al./J. Korean Inst. Surf. Eng. 52 (2019) 111-116
carbon peak at the front of the carbon line profile
shown in Fig. 3(c) came from carbon in the epoxy
mount.
When the Cr(III) coating was corroded further at
700oC for 5 h, microcracks were partially sealed, and
a thin scale covered the surface along the contours of
the coating surface (Fig. 4(a)). A thin scale was
shown in Fig. 4(b), indicating that the coating still
had good corrosion resistance despite of microcracks
in the coating. The scale consisted of slowly growing
Cr2O3 (Fig. 4(c)). Here, neither sulfides nor nitrides,
which could form owing to N2/0.1%H2S gas, were
detected because of their thermodynamic nobility
compared to the corresponding oxides.
The scale consisting primarily of Cr2O3 grew
thicker as the corrosion progressed, leading to
detection of strong Cr2O3 peaks (Fig. 5(a)). Here,
there was a faint indication of FeCr2O4 peaks,
implying that Cr2O3 reacted with FeO to a small
extent. In Fig. 5(b), microcracks were sealed further.
The scale was ~15 μm-thick (Fig. 5(c)). Sulfur
dissolved in Cr2O3. Its amount was not large enough
to form any sulfides as shown in Fig. 5(a), because
the solubility of sulfur in Cr2O3 was limited [16,17].
Chromia grew by the outward diffusion of Cr3+ ions
[18], which led to formation of Kirkendall voids
beneath the scale (Fig. 5(b)). Oxygen and sulfur
could diffuse easily along voids and along
microcracks (Fig. 5(c)). Voids and mechanical
weakness arisen by the dissolution of sulfur and
oxygen were responsible for formation of cavernous
area below the scale (Fig. 5(b)). A close look at the
carbon map shown in Fig. 5(c) indicates the presence
of carbon in the uncorroded coating. The Fe map
shown in Fig. 5(c) indicates the outward diffusion of
Fe especially along microcracks and toward voids.
The crack healing effect was similarly reported when
Cr(III) coating was oxynitrocarburized and steam-
oxidized in order to form Fe3O4, Fe2O3, and/or Fe4N
[4]. Nitrogen in N2/0.1%H2S-mixed gas could not
penetrate the scale due mainly to its negligible
solubility in Cr2O3.
When the Cr(III) coating was corroded at 900oC
for 5 h, the scale consisted of Cr2O3 as the major
phase and FeCr2O4 as the minor one (Fig. 6(a)).
Microcracks were almost completely sealed off (Fig.
6(b)). The EPMA maps shown in Fig. 6(c) indicates
Fig. 4. Cr(III) coating after corrosion at 700oC for 5 h inN2/0.1%H2S gas. (a) SEM top view, (b) SEM cross-sectional image, (c) XRD pattern.
Fig. 5. Cr(III) coating after corrosion at 800oC for 5 h inN2/0.1%H2S gas. (a) XRD pattern, (b) EPMA cross-sectional image, (c) EPMA maps of (b).
Dong Bok Lee et al./J. Korean Inst. Surf. Eng. 52 (2019) 111-116 115
that FeCr2O4 formed beneath the Cr2O3 scale,
apparently suggesting that the outward migration of
Fe was blocked by the Cr2O3 scale. Sulfur diffused
inwardly to dissolve in the bi-layered scale with a
thickness of ~30 µm. Oxygen also diffused inwardly,
but to a large amount particularly along microcracks.
The inner FeCr2O4-containing scale was mechanically
weak, because it formed around pre-formed voids
that were outlined in Fig. 5(c). Additional factors that
deteriorate the soundness of the matrix were
anisotropic volume expansion owing to simultaneous
formation of Cr2O3 and FeCr2O4, stress that
accumulated owing to thickening of the scale, and
hydrogen escape from H2S gas. The carbon map
shown in Fig. 6(c) indicates that there still existed
carbon in the uncorroded coating.
4. Conclusions
The amorphous Cr(III) coating consisted of
oxygen-dissolved nodular grains with microcracks. Its
corrosion behavior in N2/0.1%H2S gas for 5 h was
studied. At 500oC, the coating crystallized to Cr. At
600oC, a superficial oxide scale formed. Microcracks
began to be filled with oxides of Cr and Fe. At 700oC,
a thin Cr2O3 scale formed owing to thermodynamic
stability of oxides compared to the corresponding
sulfides or nitrides. When corroded at 800oC, a Cr2O3
scale formed through the outward diffusion of Cr,
which formed voids underneath the Cr2O3 scale.
When corroded at 900oC, an outer Cr2O3 layer and
inner (Cr2O3, FeCr2O4)-mixed layer formed. The
increment of corrosion temperature resulted in the
thickening of the scale, the progressive sealing of
microcracks, and the enhancement of outward
migration of Cr and Fe as well as the inward
transport of oxygen and sulfur.
Acknowledgement
This research was supported by Basic Science
Research Program through the National Research
Foundation of Korea (NRF) funded by the Ministry
of Education (2017R1D1A1B03028792).
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