synthesis and mechanical properties of cr–si–n coatings deposited by a hybrid system of arc ion...
TRANSCRIPT
www.elsevier.com/locate/surfcoat
Surface & Coatings Technology
Synthesis and mechanical properties of Cr–Si–N coatings deposited
by a hybrid system of arc ion plating and sputtering techniques
Jong Hyun Park, Won Sub Chung, Young-Rae Cho, Kwang Ho Kim*
School of Materials Science and Engineering, Pusan National University, Busan 609-735, Korea
Available online 11 September 2004
Abstract
Ternary Cr–Si–N coatings, in which Si was incorporated into CrN, were synthesized onto steel substrates (SKD 11) using a hybrid system
of arc ion plating (AIP) and sputtering techniques. In the hybrid coating system for Cr–Si–N coatings, the CrN coating process was
performed substantially by a cathodic AIP technique using Cr target, and Si could be added by sputtering Si target during CrN deposition. In
this work, comparative studies on microstructure and mechanical properties between CrN and Cr–Si–N coatings were conducted. The
hardness of the Cr–Si–N coatings increased from ~22 GPa for CrN, and reached a maximum value of approximately ~34 GPa at the Si
content of 9.3 at.%, and then decreased again with further increase of Si content. The high hardness of Cr–Si–N coatings was related to the
composite microstructure consisting of fine CrN crystallites and amorphous Si3N4. The average friction coefficient of Cr–Si–N coatings
gradually decreased with increase of Si content in CrN coatings.
D 2004 Elsevier B.V. All rights reserved.
Keywords: Cr–Si–N; Hybrid coating system; Microhardness; Friction coefficient
1. Introduction
CrN coatings are popularly used for applications of
tribological forming and casting [1,2], because the coatings
have superior wear resistance due to low friction coefficient
as well as fairly high hardness [3]. Besides, CrN coatings
show excellent corrosion resistance under severe environ-
mental condition [4] and superior oxidation resistance up to
800 8C [5]. Thus, CrN coatings produced by various
physical vapor deposition (PVD) techniques such as
sputtering, cathodic arc evaporation, ion beam sputtering,
etc. have been intensively studied [6–11]. Recently, multi-
component Cr–X–N coatings, where X is the alloying
elements such as Ti [12,13], Al [14,15], B [16], C [17,18],
Ta [19,20], Nb [21], and Ni [22], have been explored in
order to improve the properties of CrN coatings. Never-
theless, Cr–Si–N coatings and the effect of Si addition were
scarcely studied [23]. On the other hand, the effect of Si
0257-8972/$ - see front matter D 2004 Elsevier B.V. All rights reserved.
doi:10.1016/j.surfcoat.2004.08.045
* Corresponding author. Tel.: +82 51 510 2391; fax: +82 51 510 3660.
E-mail address: [email protected] (K.H. Kim).
addition into TiN coatings have been reported to improve
both mechanical properties [24] and oxidation resistance up
to 800 8C [25] due to its composite microstructure
comprising fine TiN crystallites and amorphous silicon
nitride [26,27].
In this paper, ternary Cr–Si–N coatings were synthesized
on steel substrates using a hybrid system of arc ion plating
(AIP) and DC magnetron sputtering techniques. The effect
of Si addition on the microstructural modification and
mechanical properties of CrN coatings were systematically
investigated.
2. Experimental
2.1. Deposition
The Cr–Si–N coatings were deposited on steel substrates
by a hybrid coating system, AIP method combined with a
magnetron sputtering technique. An arc cathode gun for the
Cr source and a DC sputter gun for the Si source were
installed inside the chamber depicted in previous works
188–189 (2004) 425–430
Table 1
Typical deposition conditions for Cr–Si–N coatings by a hybrid coating
system
Base pressure 2.7�10�3 Pa
Working pressure 4.0 Pa
Working gas ratio N2/Ar=5:2
Arc target source Cr (99.99%)
Sputter target source Si (99.99%)
Arc current 50 A
Sputter currents 0–2.2 A
Substrate temperature 300 8CSubstrate bias voltage 0 V
Rotational velocity of substrate 25 rpm
Substrate to target distance 300 mm
Typical film thickness ~3 Am
Fig. 1. X-ray diffraction patterns of Cr–Si–N coatings with various Si
contents.
J.H. Park et al. / Surface & Coatings Technology 188–189 (2004) 425–430426
[24]. Purities of Cr and Si targets were 99.99% and 99.99%,
respectively. A rotating substrate holder was located on a
straight line between the two sources. The rotational speed
of the substrate was 25 rpm. The steel (SKD 11) substrates,
which had been machined to disc types of 20 mm in
diameter and 3 mm in thickness, were cleaned in ultrasonic
bath cleaner using an acetone and alcohol, and cleaned
again by ion bombardment using a bias voltage of �600 V
under Ar atmosphere of 32 Pa for 12 min immediately
before deposition. The substrates were heated by a
resistance heater set inside the chamber. The base pressure
of the vacuum chamber was lower than 2.7�10�3 Pa. The
working pressure was kept at 4.0 Pa. The deposition
temperature was fixed at 300 8C. Typical deposition
conditions for Cr–Si–N coatings by a hybrid coating system
are summarized in Table 1.
2.2. Characterization
The coating thickness was measured using scanning
electron microscopy (SEM, Hitach, S-4200) and a stylus
(a-STEP) instrument. Compositional analyses of the coat-
ings to determine the contents of Cr, Si, and N were
carried out by electron probe micro-analysis (EPMA,
Shimadzu, EPMA 1600). The crystallinity of the Cr–Si–
N coatings was analyzed with low-angle X-ray diffraction
(XRD, PHILIPS, X’Pert-MPD System) using CuKa
radiation. X-ray photoelectron spectroscopy (XPS, VG
Scientifics, ESCALAB 250) was also performed to
observe the bonding status in the Cr–Si–N coatings.
Structural information on the coatings was obtained from
the high-resolution transmission electron microscopy
(HRTEM) using a field emission transmission microscope
(FE-TEM, JEM-2010F, JEOL) with a 200 kV acceleration
voltage.
Computer-controlled nanoindentation (MTS, Nanoinden-
tation XPII) equipped with Berkovich diamond indenter was
used to measure the hardness of Cr–Si–N coatings. The
indenter was operated at a constant displacement rate of 0.2
nm/s until a depth of approximately 100 nm was reached, in
order to avoid the influence of substrate effect.
The average friction coefficient and wear behavior were
evaluated through sliding tests using a conventional ball-on-
disc wear apparatus. A steel ball (diameter 6.34 mm, 700
Hv0.2) was used as a counterpart material. The sliding tests
were conducted with a sliding speed of 0.2 m/s under a load
of 1 N at ambient temperature (around 25 8C) and relative
humidity (25–30% RH) condition. Scanning electron micro-
scopy was employed to observe the morphology of the wear
track after each sliding experiment. Energy dispersive
spectroscopy (EDS) was used to reveal the compositions
of wear debris formed during the wear experiment.
3. Results and discussion
Fig. 1 shows the X-ray diffraction patterns of Cr–Si–N
coatings with various Si contents. The diffraction patterns
exhibited a pattern of crystalline CrN coatings with random
orientations of (111), (200), (220), and (311) crystal planes.
As the Si content in the CrN coating increased, the
diffraction patterns of Cr–Si–N coatings showed a weak
(200) preferred orientation, and the diffraction peak position
was a little shifted to the higher angle. However, the
diffraction peak intensity was reduced and a peak broad-
ening phenomenon took place largely from at a Si content of
9.3 at.%. Any XRD peaks corresponding to Cr2N, Cr,
Si3N4, and cromium silicide, such as CrSi2, were not
observed in Fig. 1. Fig. 2 shows the interplanar distance,
d200, of CrN (200) crystal plane as a function of Si content.
The d200 value continually decreased with increasing Si
content, and then exhibited a minimum value at the Si
content of approximately 11.0 at.%. This result can reflect
that the added Si is dissolved into CrN lattice by substitu-
tional replacement of smaller Si atoms for Cr sites. Cr–Si–N
system was scarcely reported, and the solubility data does
not appear in the literature. Although the solubility limit of
Si in the CrN phase is supposed to be very small considering
Fig. 2. Interplaner distance of (200) crystal plane as a function of Si
contents.
J.H. Park et al. / Surface & Coatings Technology 188–189 (2004) 425–430 427
the crystal structure and formation enthalpy of Si3N4 and
CrN, Si can be solved to some extent into CrN crystal
because the vapor depositions, which are proceeded under
high non-equilibrium status are not often related with
expectations from thermodynamics. In Ti–Al–N system,
the phase diagram data indicates that TiN and AlN cannot
have a solubility into each phase [28]. Nevertheless, it is
well reported that Al is dissolved into TiN up to more than
60 at.% [29]. An evidence for the solubility appears with the
change of lattice parameter.
In order to investigate the microstructural change of Cr–
Si–N coatings with addition of Si, TEM observations were
performed on two different coatings. Fig. 3 shows the cross-
sectional HRTEM images, electron diffraction patterns, and
Fig. 3. Cross-sectional HRTEM images, electron diffraction patterns, and dark-
dark-field TEM images for CrN and Cr–Si(9.3 at.%)–N
coatings. From the HRTEM image, electron diffraction
pattern, and dark-field TEM image of the CrN coatings (Fig.
3a and b), the coating layer was found to have a well-grown
crystalline phase having a columnar structure. From the
TEM works (Fig. 3c and d) for the Cr–Si(9.3 at.%)–N
coatings, it was observed that the coating layer was a
composite microstructure consisting of crystallites and an
amorphous phase. In addition, it was also found that large
columnar microstructure of CrN was modified into the
refined grains with relatively random orientation with Si
addition. The electron diffraction patterns of Fig. 3a and c
clearly show this change.
Fig. 4 shows XPS spectra near the binding energies of
Si 2p and Cr 2p for the Cr–Si–N coatings with various Si
contents. The peak corresponding to 101.8 eV, which is in
good agreement with that of Si3N4 compound, was clearly
observed as the Si content increased above 9.3 at.% (Fig.
4a). On the other hand, the peak corresponding to 575.8
eV was found to be that of stoichiometric CrN [30], and
this peak intensity decreased with increase of Si content
(Fig. 4b). The decrease of CrN peak intensity above 9.3
at.% Si content is believed to be attributed to the
appearance of Si3N4 phase. From our XPS results it was
found that the coatings were synthesized as a composite
comprising CrN and Si3N4 as the Si content increased
above 9.3 at.%.
It was concluded from our instrumental analyses of
XRD, TEM, and XPS that the coatings with Si contents
above 9.3 at.% must be a composite consisting of fine CrN
crystallites and amorphous Si3N4.
field TEM images for CrN (a, b) and Cr–Si(9.3 at.%)–N (c, d) coatings.
Fig. 4. XPS spectra near the binding energies of Si 2p (a) and Cr 2p (b) for
the Cr–Si–N coatings with various Si contents.
J.H. Park et al. / Surface & Coatings Technology 188–189 (2004) 425–430428
Fig. 5 shows the microhardness of Cr–Si–N coatings as a
function of Si content. As the Si content increased, the
hardness of the Cr–Si–N coatings gradually increased from
~22 GPa for CrN, and reached maximum values of
approximately 34 GPa at the Si content of 9.3 at.%, and
then steeply decreased again with further increase of Si
Fig. 5. Microhardness of Cr–Si–N coatings as a function of Si content.
content. The hardness value (~34 GPa) of Cr–Si–N coatings
having a Si content of 9.3 at.% was significantly increased
compared with that (~22 GPa) of CrN coatings. The
hardness change of CrN coatings in Fig. 5 results from
the microstructural change with Si addition. The hardness
increase of Cr–Si–N coatings must be strongly related with
grain size refinement of CrN and fine composite micro-
structure. The coatings with 9.3 at.% Si were already proved
by our instrumental analyses to be a fine composite
comprising fine CrN crystallites and amorphous Si3N4. As
seen in Fig. 3, the crystallite size was largely reduced with
codeposition of amorphous silicon nitride. Thus, the grain
boundary hardening described by Hall–Petch relationship
would take place. Furthermore, the codeposition of amor-
phous Si3N4 phase among CrN crystallites would enhance
cohesive energy of the interphase boundaries [30]. On the
other hand, the hardness reduction with further increase of
Si content after maximum hardness, as indicated in Fig. 5,
was suggested to be due to the increase of volume fraction
of amorphous Si3N4 phase. It was reported that the increase
in volume fraction of amorphous Si3N4 phase resulted in the
hardness reduction [24,27]. The Si effect on the micro-
structural evolution and the hardness has been reported
similarly in other systems such as Ti–Si–N [24,26] and Ti–
Al–Si–N [31] systems. Recently, Martinez et al. [23] have
synthesized Cr–Si–N coatings using a sputtering method
and reported that the hardness of Cr–Si–N coatings
increased from ~17 GPa for CrN to the maximum value
of ~23 GPa at Si content of 3 at.%, and then dramatically
decreased. They explained the hardness increase with Si
content due to a solid solution of Si in the CrN lattice, and
the hardness drop beyond the maximum was attributed to
the formation of Si3N4. The differences in the maximum
hardness and Si content between our study and that of
Martinez et al. are considered to be due partly to the
difference of the coating process.
Fig. 6 shows the friction coefficients of the CrN, Cr–
Si(9.3 at.%)–N, and Cr–Si(12.5 at.%)–N coatings against a
Fig. 6. Friction coefficients of the CrN, Cr–Si(9.3 at.%)–N, and Cr–Si(12.5
at.%)–N coatings against a steel ball.
Fig. 7. SEM morphologies of wear track and composition analyses for the wear debris after sliding test: (a) CrN, (b) Cr–Si(9.3 at.%)–N, and (c) Cr–Si(12.5
at.%)–N coatings.
J.H. Park et al. / Surface & Coatings Technology 188–189 (2004) 425–430 429
steel ball. The average friction coefficient of coatings
largely decreased from 0.5 for CrN up to 0.2 with increasing
Si content. Fig. 7 shows SEM morphologies of wear track
and composition analyses for the wear debris after the
sliding test with different Si contents. As the Si content
increased, the wear track morphology became smooth as
shown in Fig. 7. From EDS analyses of Fig. 7, the Fe
element in wear debris decreased with increasing Si
contents. On the other hand, Si and O elements increased
with addition of Si. It is considered that the wear behavior
between the coatings and the steel ball would be adhesive
wear, which was generally caused by hard material and
relatively soft steel ball [32]: the wear tracks were torn off
and the Fe elements from counter material were transferred
into the CrN coating as shown in Fig. 7. The decrease in
friction coefficient with the increase in Si contents would be
caused by a smoother surface due to codeposition of the
amorphous phase and by a tribo-chemical reaction, which
often takes place in many ceramics, e.g., Si3N4 reacts with
H2O to produce SiO2 or Si(OH)2 tribo-layer. These products
of SiO2 and Si(OH)2 are known to a function as a self-
lubricating layer [33]. The formation of tribo-layer would be
more promoted with increasing Si content. The increase of
the self-lubricating layer resulted in decreasing quantity of
transferred Fe from the steel ball. These results correspond
well with the EDS results.
4. Conclusions
Cr–Si–N coatings were deposited on steel substrates by
the hybrid coating system, where the AIP method was
combined with a magnetron sputtering technique. The Cr–
Si–N coatings with the Si contents above 9.3 at.% were a
composite consisting of fine CrN crystallites and amor-
phous Si3N4. The hardness of the Cr–Si–N coatings
exhibited a maximum value of ~34 GPa at a Si content
of 9.3 at.% due to the microstructural change to a fine
composite microstructure and the refinement of CrN
crystallites. The average friction coefficient of the Cr–Si–
N films largely decreased with an increase in Si content.
This behavior can be attributed to the tribo-chemical
reaction between Si and ambient humidity, which enables
to formation of SiO2 or Si(OH)2 tribo-layer, playing a role
as self-lubricant.
Acknowledgement
This work was performed through National Research
Laboratory (NRL) project supported by Ministry of Science
and Technology of Korea (MOST). Authors also thank Dr.
Won of Korea Basic Science Institute for obtaining and
discussing XPS results.
J.H. Park et al. / Surface & Coatings Technology 188–189 (2004) 425–430430
References
[1] C. Rebholz, H. Ziegele, A. Leyland, A. Matthew, Surf. Coat. Technol.
115 (1999) 222.
[2] J. Creus, H. Idriss, H. Mazille, F. Sanchette, P. Jacquot, Surf. Coat.
Technol. 107 (1998) 183.
[3] P.H. Mayrhofer, H. Willmann, C. Mitterer, Surf. Coat. Technol.
146–147 (2001) 222.
[4] B. Navinsek, P. Panjan, I. Milosev, Surf. Coat. Technol. 97 (1997)
182.
[5] B. Navinsek, P. Panjan, Surf. Coat. Technol. 74–75 (1995) 919.
[6] X. Nie, A. Leyland, A. Matthews, Surf. Coat. Technol. 133–134
(2000) 331.
[7] P.H. Mayrhofer, G. Tischler, C. Mitterer, Surf. Coat. Technol.
142–144 (2001) 78.
[8] J.D. Demaree, C.G. Fountzoulas, J.K. Hirvonen, Surf. Coat. Technol.
86–87 (1996) 309.
[9] Ghislaine Bertrand, Catherine Savall, Cathy Meunier, Surf. Coat.
Technol. 96 (1997) 323.
[10] C. Gautier, H. Moussaoui, F. Elstner, J. Macht, Surf. Coat. Technol.
86–87 (1996) 254.
[11] P. Hones, R. Sanjines, F. Levy, Surf. Coat. Technol. 94–95 (1997)
398.
[12] D.H. Jung, J.H. Joo, Surf. Coat. Technol. 169–170 (2003) 424.
[13] J.J. Nainaparampil, J.S. Zabinski, A. Korenyi-Both, Thin Solid Films
333 (1998) 88.
[14] S. Ulrich, S. Sattel, Thin Solid Films 437 (2003) 164.
[15] J. Vetter, E. Lugschider, S.S. Guerreiro, Surf. Coat. Technol. 98 (1998)
1233.
[16] B. Rother, H. Kappl, Surf. Coat. Technol. 96 (1997) 163.
[17] J. Almer, M. Oden, G. Hakansson, Thin Solid Films 385 (2001) 190.
[18] S.H. Yao, Y.L. Su, Wear 212 (1997) 85.
[19] M. Cekada, P. Panjan, B. Navinsek, F. Cvelbar, Vacuum 52 (1999)
461.
[20] Ranjana Saha, Rama B. Inturi, John A. Barnard, Surf. Coat. Technol.
82 (1996) 42.
[21] J.N. Tan, J.H. Hsieh, Surf. Coat. Technol. 167 (2003) 154.
[22] F. Regent, J. Musil, Surf. Coat. Technol. 142–144 (2001) 146.
[23] E. Martinez, R. Sanjines, O. Banakh, F. Levy, Thin Solid Films
447–448 (2004) 332.
[24] K.H. Kim, S.R. Choi, S.Y. Yoon, Surf. Coat. Technol. 298 (2002) 243.
[25] J.B. Choi, K. Cho, M.H. Lee, K.H. Kim, Thin Solid Films 447–448
(2004) 365.
[26] S. Veprek, M. Haussmann, S. Reiprich, Li Schzhi, J. Dian, Surf. Coat.
Technol. 86–87 (1996) 394.
[27] S. Veprek, S. Reiprich, Thin Solid Films 268 (1995) 64.
[28] S. PalDey, S.C. Deevi, Mater. Sci. Eng., A 342 (2003) 58.
[29] Ayako Kimura, Hiroyuki Hasegawa, Kunihiro Yamada, Tetsuya
Suzuki, Surf. Coat. Technol. 120–121 (1999) 438.
[30] Q.G. Zhou, X.D. Bai, X.W. Chen, D.Q. Peng, Y.H. Ling, D.R. Wang,
Appl. Surf. Sci. 211 (2003) 293.
[31] I.W. Park, S.R. Choi, M.H. Lee, K.H. Kim, J. Vac. Sci. Technol., A 21
(4) (2003) 895.
[32] S. Wilson, A.T. Alpas, Wear 245 (1996) 223.
[33] J. Takadoum, H. Houmid-Bennani, D. Mairey, J. Eur. Ceram. Soc. 18
(1998) 553.