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i n t e rn a t i o n a l j o u r n a l o f h y d r o g e n en e r g y 3 7 ( 2 0 1 2 ) 8 7 2 4e8 7 2 8
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Phase transformations and micro cracks induced by hydrogenin cold-rolled and annealed AISI 304 stainless steels
Yongfeng Li a,b, Limin Zhao c, Wenbin Kan a, Hongliang Pan a,*aSchool of Mechanical and Power Engineering, East China University of Science and Technology, 130 Meilong Road, Shanghai 200237, Chinab School of Mechanical and Electrical Engineering, Henan Institute of Science and Technology, East of HuaLan Road, Xinxiang 453003, ChinacManagement Institute, Xinxiang Medical University, East of JinSui Road, Xinxiang 453003, China
a r t i c l e i n f o
Article history:
Received 1 December 2011
Received in revised form
10 February 2012
Accepted 16 February 2012
Available online 8 March 2012
Keywords:
Phase transformation
Surface cracking
Hydrogen charging
Martensite
* Corresponding author. Tel./fax: þ86 21 6425E-mail address: [email protected] (H. P
0360-3199/$ e see front matter Copyright ªdoi:10.1016/j.ijhydene.2012.02.083
a b s t r a c t
The effect of hydrogen and stress on the phase transformation and surface cracking in
cold-rolled and annealed AISI 304 stainless steels was investigated. Hydrogen was intro-
duced by cathodic charging in 0.1 M H2SO4 þ 1 g/L Na2HAsO4$7H2O. Scanning electron
microscopy was used to observe structural changes and surface cracks of the specimens.
X-ray diffraction analysis was used to investigate phase transformations in the uncharged
and charged specimens immediately after charging or during aging. Cathodic charging can
cause ε martensite phase transformation and aging after cathodic charging can induce the
ε and a0 martensite transformation. There are a certain amount of surface cracks on the
specimens surface after hydrogen charging or during aging. The surface morphology of the
specimens is studied, and the mechanism of the hydrogen-induced phase transformation
and the surface cracking formation in the charged specimens immediately after charging
or during aging is discussed.
Copyright ª 2012, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights
reserved.
1. Introduction surface cracking formation are still unknown. Numerous X-
It is well known that the cathodic electrolytic charging of
austenitic stainless steel with the hydrogen that evolves from
acid solutions containing promoters brings about the forma-
tion of numerous surface micro cracks [1e3]. Additionally, ε
and a0 martensites are formed under these conditions [3e6].
Previous studies [7e12] have shown that hydrogen-induced
martensite can play an important role in pitting corrosion,
surface cracking and stress corrosion cracking propagation.
Hydrogen-induced surface cracks are both grain-oriented
transcrystalline and aligned along the grain boundaries [13].
However, the detailed nature and mechanisms of the
hydrogen-induced martensite transformations and the
3622.an).2012, Hydrogen Energy P
ray diffraction studies have confirmed that cathodic hydrogen
charging can lead to a phase transformation [5,7,14,15].
However, no detailed mechanistic or morphological studies
are available for both cold-rolled and annealed AISI 304
stainless steels.
The purpose of this study is to investigate the effect of
cathodic hydrogen charging and aging after cathodic
hydrogen charging on phase transformation in both cold-
rolled and annealed AISI 304 stainless steels, and the effect
of hydrogen charging and aging on surface cracking. We aim
to further expand the hydrogen-induced phase trans-
formation mechanism and the surface crack formation
mechanism.
ublications, LLC. Published by Elsevier Ltd. All rights reserved.
i n t e r n a t i o n a l j o u r n a l o f h y d r o g e n en e r g y 3 7 ( 2 0 1 2 ) 8 7 2 4e8 7 2 8 8725
2. Experiment procedure
2.1. Material
Experiments were performed on commercially available AISI
304 austenitic stainless steel. The specimens for this study
were 15 mm � 30 mm cold-rolled foil with a thickness of
0.2 mm. Specimens were divided into two groups, one was to
maintain cold-rolled state, that is, which was as received; the
other was annealed in a vacuum heat-treatment furnace at
a temperature of 1323K for 2 h. These two types of specimens
were used for the following experiments as the initial state.
The chemical composition of the as received AISI 304 stainless
steels is listed in Table 1.
2.2. Cathodic hydrogen charging
Prior to every cathodic hydrogen charging experiment, the
specimen was rinsed with distilled water and ultrasonically
cleaned in acetone. It was then immersed in an acid pickling
solution (H2SO4: 350 g/L, HF: 110 g/L, H2O: balance) for 3 min
before being immersed in a chemical polishing solution
(H3PO4: 25 wt%, HNO3: 6.5 wt%, H2O: 68.5 wt%, C3H8O3 7.5ml/L,
CH4N2S: 2 g/L, C7H6O6S$2H2O: 1 g/L) at 80e90 �C for a few
minutes to remove the surface oxide layer of Cr2O3, etc. and
activate the surface. The specimen surfaces were rinsed with
distilled water and ultrasonically cleaned in acetone again
and dried quickly by warm air blowing.
Hydrogen was introduced into specimens by the cathodic
charging. Cathodic charging was carried out at a temperature
of 300K with a platinum anode in 0.1 M H2SO4 solution con-
taining 1 g/L Na2HAsO4$7H2O as a hydrogen recombination
poison. The current density was a single charging current
density of 150mA/cm2 and experiments were carried out over
different periods of time ranging from 30 min to 96 h. Some of
the charged specimens were then aged at room temperature
for 20 days.
2.3. The examination of surface cracks and phasetransformations
In order to observe the structural changes and surface cracks
of the specimens, scanning electron microscope was used. X-
ray diffraction analyses were used to investigate the phase
transformation in the uncharged and charged specimens
immediately after charging or during aging. X-ray diffraction
studies were performed using a Rigaku D/max2550VB/PC X-
ray diffractometer with Cu Ka radiation at 40 kV and 100 mA.
Measurements were made from 40� � 2q � 100� in steps of
Table 1 e Chemical composition of AISI 304 stainlesssteel, wt%.
Element C Mn Si Cr Ni
Percentage (%) 0.072 1.43 0.57 18.24 8.06
Element Mo Cu S P Fe
Percentage (%) 0.16 0.07 0.0088 0.048 Balance
0.02� at a scan rate of 0.12 s/step. On the basis of Bragg’s law
and the crystallographic relationships between lattice
parameters and interplanar spacing, d, the lattice parameters
of the phases were determined.
3. Results and discussion
3.1. Effect of cathodic hydrogen charging on phasetransformation
After cathodic hydrogen charging, the annealed specimens
were immediately analyzed by X-ray diffraction. Fig. 1 shows
the effect of cathodic hydrogen charging on the phase trans-
formation. The specimens were charged at 150 mA/m2 for
various lengths of time. From the X-ray diffraction analyses,
only the austenite phase, g, (face-centered cubic (fcc) struc-
ture) was present in the uncharged specimen and the average
lattice constant, a, was 3.5851A, which was close to the
reported parameter (a ¼ 3.593 A) [3]. For the charged speci-
mens a new reflection was found. It was indexed as belonging
to an εmartensite phase, which has a close-packed hexagonal
structure. For the specimens charged ranging from 0.5 h to
96 h, the lattice parameter of g austenite phase and ε
martensite phase varied with the different hydrogen charging
time.When the specimenswere charged for 0.5, 1, 24 and 96 h,
the average lattice constant (a) of g austenite phase which
measured in this work was 3.5884, 3.5910, 3.5958 and 3.5972 A,
respectively, and the lattice parameters of ε martensite phase
were a ¼ 2.5655 A and c ¼ 4.0743 A, a ¼ 2.5696 A and
c ¼ 4.0691 A, a ¼ 2.5720 A and c ¼ 4.0615 A, a ¼ 2.5832 A and
c ¼ 4.0813 A, respectively. Peak broadening was different
between the original peaks associated with the uncharged
specimen and the subsequent peak of the charged specimen
while the peak position changed slightly. This phenomenon
may be related to the entry of hydrogen into the specimens by
cathodic charging, which severely strains the metal lattice
resulting in compressive stress at the surface and specimen
Fig. 1 e X-ray diffraction spectra of the annealed AISI 304
stainless steel taken immediately after cathodic charging
at 150 mA/cm2 at different charging times.
i n t e rn a t i o n a l j o u r n a l o f h y d r o g e n en e r g y 3 7 ( 2 0 1 2 ) 8 7 2 4e8 7 2 88726
warping. The twist and deformation of the specimen increase
with the amount of hydrogen charging and the amount of
hydrogen charging increases with an increase in the charging
current density or charging time. All the peaks, therefore, shift
to slightly lower angles and broaden considerably. Further-
more, the amount of ε phase increased with an increase in
charging time. However, no reflections that correspond to the
a0 phase for the sample was observed immediately after the
cathodic charging of the specimens. As thematrix of the cold-
rolled 304 stainless steels already contained a certain amount
of a0 martensite phase it is difficult to determine if the
a0 martensite phasewas induced by cold-rolling or by cathodic
hydrogen charging. Therefore, the cold-rolled specimenswere
not analyzed by X-ray diffraction immediately after cathodic
hydrogen charging.
3.2. Effect of aging after cathodic hydrogen charging onphase transformation
X-ray diffraction patterns of the uncharged and the charged
specimens that were aged at room temperature for 20 days are
shown in Fig. 2. During aging after the cathodic hydrogen
Fig. 2 e X-ray diffraction patterns of the uncharged and the
charged specimens aged at room temperature for 20 days.
(a) cold-rolled specimens; (b) annealed specimens.
charging, a large amount of hydrogen escaped from the
specimens and this resulted in significant structural changes.
The X-ray diffraction patterns reveal that new reflections are
present and these reflections can be indexed as belonging to
a0 and ε martensite phases whereas no a0 phase was observed
immediately after charging. From the X-ray diffraction
patterns of cold-rolled specimens in Fig. 2a, the g and a0 phaseexist in all of the specimens, and when the specimens were
charged for 0, 0.5, 1, 24 and 96 h, the average lattice constant
(a) of g austenite phase which measured in this work was
3.5786, 3.5877, 3.5900, 3.5981 and 3.6013 A, respectively, and
the average lattice constant (a) of a0 phase was 2.8621, 2.8633,
2.8641, 2.8658 and 2.8662 A, respectively. When the charging
time is 24 and 96 h, a new reflection was found. It was indexed
as belonging to an ε martensite phase, and the lattice
parameters of ε martensite phase were a ¼ 2.5800 A and
c ¼ 4.0864 A, a ¼ 2.5825 A and c ¼ 4.0918 A, respectively. In
Fig. 2b, when the specimens were charged for 0, 0.5, 1, 24 and
96 h, the average lattice constant (a) of g austenite phase
whichmeasured in this workwas 3.5767, 3.5779, 3.5786, 3.5796
and 3.5825 A, respectively, and the average lattice constant (a)
of a0 phase was 2.8872, 2.9028, 2.9331, 2.9382 and 2.9513 A,
respectively. When the charging time is 1, 24 and 96 h, an ε
martensite phase was found, and the lattice parameters of ε
martensite phase were a ¼ 2.5236A and c ¼ 4.1845 A,
a ¼ 2.5249A and c ¼ 4.200 A, a ¼ 2.5262 A and c ¼ 4.2113 A,
respectively.The uptake of hydrogen caused the expansion of
the lattice in the specimen surface layer during cathodic
hydrogen charging and this resulted in a compressive stress
on the surface [14]. During aging, hydrogen escaped from the
external surface, the hydrogen concentration at the surface is
quickly reduced to low values, redistribution of hydrogen
caused a high tensile stress at the surface and compressive
stress beneath the surface, and promoted the formation of
a0 martensite phase [14,16,17]. The intensity and amount of
a0 and ε phase increased with charging time upon aging. A
comparison between Fig. 2a and b shows that much less ε
phase is formed in the charged cold-rolled specimens than in
the charged annealed specimens. Holzworth and Louthan [6]
suggested that the cold working of 304 stainless steel before
cathodic hydrogen charging reduces the extent of the g -to- ε
transformation, which occurs upon charging.
3.3. Effects of hydrogen charging and aging on surfacecracking
The surface morphologies of the 150 mA/m2 cathodically
charged specimens were observed by scanning electron
microscopy. The charging times of the specimens were 1 h
and 96 h while the aging time was 20 days. An examination of
the specimens surface by scanning electron microscopy
showed that as hydrogen escaped from the surface during
room temperature aging, cracking occurred on the specimens
surface. The cracks are shown in Fig. 3. No cracking was
observed in the annealed specimen uncharged, as shown in
Fig. 3a, b and c show that there is a certain amount of cracks
on the annealed specimens surface charged for 1 h and 96 h.
And when the cold-rolled specimens were charged for 96 h,
some very broad cracks appeared on the specimens surface,
as shown in Fig. 3d. Both specimens behaved in a similar
Fig. 3 e Surface cracking observed during aging after the specimen was charged at 150 mA/cm2 for different charging times.
(a) annealed specimen uncharged; (b) annealed specimen charged for 1 h; (c) annealed specimen charged for 96 h; (d) cold-
rolled specimen charged for 96 h.
i n t e r n a t i o n a l j o u r n a l o f h y d r o g e n en e r g y 3 7 ( 2 0 1 2 ) 8 7 2 4e8 7 2 8 8727
manner in that the existing cracks propagated in the length
and depth directions with charging time and, additionally,
more cracks appeared on the specimens surface. Therefore,
the crack density, the average crack depth and the crack
length increased with charging time. When the specimens
were charged for a certain time, there was high hydrogen
concentration at the surface. This will lead to the volume
expansion, and consequently will cause high compressive
stresses at the surface. The high stresses can cause the
surface deformation [17]. During outgassing stage, hydrogen
mainly escaped from the external surface, the hydrogen
concentration quickly became lower at the surface and then
decreased at greater depthswhich caused a high tensile stress
at the surface. While there was a high compressive stress
beneath the surface. As the formation of a0 martensite is
accompanied with volume expansion [3], the appearance of
the tensile stress and lack of constraint at the surface will
promote the a0 martensite and consequently surface cracking
during outgassing. Q Yang et al. [2] carried out an in situ
observation of surface cracking process during aging, they
suggested that the crack formation and growth might be
related to the hydrogen outgassing process.
4. Conclusions
Cathodic hydrogen charging can lead to ε martensite trans-
formation and aging after cathodic hydrogen charging can
induce the ε and a0 martensite phase transformation, and the
amount of both the a’ and ε martensite phases produced
increases with an increase in charging time, whilemuch less ε
phase is formed in the charged cold-rolled specimens than in
the charged annealed specimens. Additionally, surface
cracking appears on the specimens surface after hydrogen
charging or during aging, and the cracks propagate in the
length and depth directions with charging time. Permeated
hydrogen strains the metal lattice, leading to a change (a shift
to slightly lower angles) in peak position and considerable
increase in broadening of all peaks. Hydrogen charging leads
to the volume expansion and consequently high compressive
stresses beneath the surface. Hydrogen outgassing causes
a high tensile stresses at the surface. High compressive
stresses during charging and tensile surface stresses during
aging promote the formation of surface cracking.
Acknowledgments
The authors gratefully acknowledge the National Science
Council of China for financial support of this research under
Contract No. 50875084.
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