ICMCTF2008 Session B5-1: Properties and Characterization of Hard Coatings and Surfaces

Wednesday, April 30, 2008 8:00 AM in Room Golden West

Wednesday Morning

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8:00 AM B5-1-1 Plasma Enhanced Magnetron Sputter Deposition of Ti-Si-C-N Based Nanocomposite Coatings
R. Wei (Southwest Research Institute)
Ti-Si-C-N - based nanocomposite coatings have been prepared using a Plasma Enhanced Magnetron Sputtering (PEMS) technology and shown superior properties over conventional nitride coatings against severe sand erosion, which damages gas turbine compressor blades and vanes. A large number of samples were prepared using a comprehensive Design of Experiment (DOE) method to understand the effect of deposition parameters on the microstructure, nanohardness, adhesion, and erosion resistance against sand and optimize the processing parameters. Several deposition parameters including the ion energy, ion current density, partial pressure of nitrogen, partial pressure of trimethylsilane (TMS) and deposition duration were studied, and a wide range of each parameter was selected in the study. The microstructures of thus deposited coatings were studied using scanning electron microscopy and X-ray diffraction. Rockwell C scale indentation was used to evaluate the adhesion of the coatings. Nanoindentation was used to obtain the nanohardness, modulus and toughness, while the microhardness was also measured. Energy dispersive spectroscopy was used to determine the composition. Finally, the samples were erosion tested using a sand blaster with 50 µm alumina at 20 psi pressure at two incidental angles (30° and 90°). After this comprehensive study, a few sets of processing parameters have been identified. The coatings obtained under these conditions have a dense nanostructure, high hardness and very high resistance to sand erosion. Over a few hundred times of reduction in material loss was achieved. In this review presentation, we will discuss the detailed results and their relationship with the processing parameters. A few examples for practical applications will be presented. Keywords: Nitrides, nanocomposite, thick coatings, erosion resistance, turbines.
8:40 AM B5-1-3 Stabilization of Cubic (Ti1-xAlx)1-yYyN Thin Films by Bipolar Pulsed DC Magnetron Sputtering
M. Moser, P.H. Mayrhofer (Montanuniversität Leoben, Austria); L. Szekely, P. Barna (Hungarian Academy of Sciences, Hungary)

Ti1-xAlxN thin films can be synthesised by plasma-assisted vapour deposition in the cubic NaCl structure with AlN mole fractions (x)=0.7. At higher Al-contents the hexagonal ZnS-wurtzite modification is formed. Cubic Ti1-xAlxN films with highest possible Al content are preferred in industrial applications as they combine superior mechanical properties with good oxidation protection. Further improvement can be obtained by alloying reactive elements such as yttrium, which effectively retard oxide scale growth by segregation to scale grain boundaries.

Recently, we have shown that the addition of yttrium to Ti1-xAlxN reduces the maximum possible AlN content for single phase cubic films1. DC magnetron sputtering of Ti0.45Al0.55N results in the formation of a single-phase cubic coating, whereas Ti0.46Al0.52Y0.02N, having a lower Al content, contains the hexagonal ZnS-wurtzite structure phase.

Employing x-ray diffraction, scanning and transmission electron microscopy we reveal that bipolar pulsed magnetron sputtering allows the cubic stabilization of Ti0.46Al0.52Y0.02N when low frequencies of 50-80 kHz but long positive pulse durations up to 5 µs are used. Consequently, as the formation of the hexagonal phase can be suppressed the hardness increases from 23.5 GPa for DC to 34.3 GPa for bipolar pulsed magnetron sputtered films. Langmuir measurements yield increased electron temperature and higher average ion fluxes for bipolar pulsed magnetron sputtering, which are related to overshoots in the negative pulse and fast MHz ringing in the positive pulse when the polarity of the voltage changes.

We can thus conclude that the different plasma conditions during bipolar pulsed compared to DC magnetron sputtering suppress the hexagonal phase formation. Consequently, we have developed a single-phase cubic Ti0.46Al0.52Y0.02N film which combines excellent mechanical properties with improved oxidation protection due the incorporation of Y and the benefits of a high Al content.

1M. Moser and P. H. Mayrhofer, Scripta Mater. 57 (2007), 357.

9:00 AM B5-1-4 Structure, Stresses and Stress Relaxation of TiN-Me (Me=Ag, Cu) Multilayer and Nanocomposite Coatings
H. Köstenbauer, G.A. Fontalvo, C. Mitterer, J. Keckes (University of Leoben, Austria)
The addition of a suitable metal phase to transition metal nitride hard coatings in a multilayer arrangement or as a nanocomposite is assumed to result in improved mechanical properties of the films. Thus, in this work morphology, structure and thermal behavior of magnetron sputtered TiN/Ag and TiN/Cu multilayer thin films with a bilayer thickness Λ in the range of 75-800 nm as well as nanocomposite films with a metal content up to 45 at.% were characterized. All nanocomposite films exhibit domain sizes around 10 nm independent from the metal content. In contrast, the multilayer coatings show a strong correlation between domain size and bilayer thickness as well as initial porosity. To investigate the relationship between film structure and stress development, the films were thermally cycled from room temperature up to maximum temperatures of 500 and 700°C, dependent on the material combination. All stress-temperature curves show significant changes above the deposition temperature during heating and linear thermoelastic behavior during cooling. Plastic deformation of the metal phase and sintering effects are the reason for the changes during the heating stage and the determining factors for the stress temperature behavior in multilayer as well as nanocomposite arrangements. Additionally, tribological tests were conducted for the nanocomposite films were the coefficient of friction was below 0.2 at elevated temperatures due to the addition of the soft metal. This lubricating effect is more pronounced for the films containing Ag.
9:20 AM B5-1-5 Compressive Stress Generation in Titanium Nitride Coatings
R. Machunze, G.C.A.M. Janssen (Delft University of Technology, Netherlands)

Titanium nitride films (TiN) are used amongst other applications as wear-protecting coatings. The residual stress in the film is a key factor determining the performance of the coating.

TiN thin films with 111 fibre texture have been deposited on 100 mm Si wafers by reactive magnetron sputtering from a Ti target in an industrial coating system. During deposition (dep. rate approx. 0.1 nm/s) at 5 kW cathode power, 125 V bias, 450°C dep. temperature and 4x10-3 mbar, the samples performed a planetary motion in front of the target (target size 600x120 mm2). Stress analysis has been performed on TiN films of different thicknesses with X-ray diffraction by the so called sin2 method and with wafer curvature measurements before and after deposition.

From wafer curvature we find high compressive stress for thinner films and less compressive stress for thicker films. Films under compressive stress were analyzed by X-ray diffraction. Using the 311 reflection we find a dependence of lattice spacing on diffraction direction in accord with plane stress. For the 111 reflection we also find this relation with the exception for the diffraction vector perpendicular to the film. Also films removed from the surface were analyzed by X-ray diffraction. Here we find that after removal from the substrate the stress is about zero and the lattice parameter is equal to the equilibrium lattice parameter of TiN.

Both from wafer curvature and X-ray diffraction analysis we conclude that in TiN compressive stress is generated at the grain boundaries.

9:40 AM B5-1-6 Influence of Rotation During Sputtering on the Stoichiometry of TiAlN/CrN Multilayer Coating
M. Panjan, S. Sturm, P. Panjan, M. Cekada (Jozef Stefan Institute, Slovenia)
Multilayer coatings TiAlN/CrN were prepared by magnetron sputtering with rotation of samples alongside TiAl and Cr targets. Thickness of individual layers was ~50 nm. Microstructure of coatings was studied by transmission electron microscope (TEM). Electron energy loss spectroscopy (EELS) analysis was preformed in the individual layers. TEM images revealed ~20 nm thick lamellae inside some of the CrN layers. From the shape of near-edge structure of nitrogen K and chromium L2,3 edges in EELS it was determined that lamellae correspond to hexagonal Cr2N phase. Stoichiometry in TiAlN and CrN layers was determined from intensity of EELS edges. Point analysis was made at different distances from TiAlN/CrN interface. The Cr/N stoichiometry varied strongly within the CrN layers while TiAl/N stoichiometry was approximately constant through the TiAlN layers. Variation of Cr/N and existence of Cr2N phase can be explained by changes in deposition rate which occur due to rotation of sample during the deposition. Partial pressure of nitrogen during the deposition is constant, therefore only the changes in deposition rate can produce variation in the Cr/N ratio. Only at certain conditions the deposition rate is high enough for growth of Cr2N phase. The same argument could be used for TiAl/N ratio, however in this case the partial pressure of nitrogen is high enough for growth of TiAlN layer with constant TiAl/N ratio even at highest deposition rates. For the purpose of understanding the changes in stoichiometry and existence of Cr2N phase in certain CrN layers we made a computer simulation of deposition process. By modeling the deposition rate from targets and calculating the trajectory of sample we could calculate the growth rate of CrN and TiAlN layers. Results of simulation explain observed differences in stoichiometry and selected growth of Cr2N phase.
10:00 AM B5-1-7 Nitrogen-Induced Nanostructure and Property Changes in Sputtered Ti(Al)-B Films
C. Rebholz (University of Cyprus); M.A. Monclus, M.A. Baker (University of Surrey, United Kingdom); P.H. Mayrhofer (Montanuniversität Leoben, Austria)
Low aluminium (4-10 at.%) containing Ti-B(N) films, with nitrogen concentrations of between 0 and 43 at.% and B/Ti ratios in the range of 1.7 to 2.4, were synthesized by co-sputtering from TiAl and TiB2 targets in Ar/N2 mixtures at 150oC. The film stoichiometry, relative phase composition, nanostructure and mechanical properties were determined using X-ray photoelectron spectroscopy (XPS), X-ray diffraction (XRD) and transmission electron microscopy (TEM), in combination with nanoindentation and scratch adhesion measurements. XRD and TEM studies revealed nanocrystalline structures (TiB2 grain size = 4 nm) in low nitrogen ( 10 at.%) containing films; the incorporation of further nitrogen was found to decrease the crystallinity, resulting in the formation of amorphous films. TiB2 and Al bonds were observed in Ti(Al)-B films, while nitrogen additions resulted in the formation of additional Ti-N and Al-N bonds. B-N bonding was found for higher nitrogen concentrations ( 32 at.%). Correlation of composition and bonding with mechanical data indicated that film hardness, elastic modulus and adhesion decreased (from 35 to 10 GPa, 340 to 150 GPa and 40 to 15 N, respectively) with increasing nitrogen (and therefore amorphous BN) content. No correlation between friction coefficient and BN content could be established in pin-on-disc and reciprocating fretting tests. Nevertheless, low disc and ball wear rates were found for coatings containing large amounts of amorphous BN. Thermo-gravimetric analysis (TGA) revealed the on-set of oxidation at temperatures between ~650 and ~750oC for Ti(Al)-B and low nitrogen containg Ti(Al)-B-N films, respectively.
10:20 AM B5-1-8 Corrosion Behavior of (Ti-Al-Cr-Si-V)xNy Coatings Derived from RF Magnetron Sputtering
C.H. Lin, J.G. Duh (National Tsing-Hua University, Taiwan)
By using the multi-component target Ti-Al-Cr-Si-V target, multi-component metal (MC) and multi-component nitride (MCN) coatings could be deposited on mild steel substrates by adjusting nitrogen inlet in the sputtering process. Thickness of the coatings were controlled around 1.6 micro m. Sufficient hardness higher than 30 Gpa was revealed for the multi-component nitride (MCN) coating. Corrosion resistance of the MC and MCN coatings was investigated by Tafel plot and electrochemical impedance spectroscopy (EIS) in 3.5% NaCl electrolyte. Although MCN coating exhibited excellent hardness, the corrosion current for the MCN coating (icorr=19.4 micro A/cm2) was higher than mild steel (icorr=16.4 micro A/cm2), which implied poor corrosion resistance and a porous structure derived from sputtering process. From the cross-sectional observation, numerous porosities were found along the nano-columns in the MCN coating. After introduction of 100nm MC interlayer, these porosities were eliminated and the calculated porosity rate was 80% off. The improvements on corrosion potential (Ecorr=-520mV) and current (icorr=8.05 micro A/cm2) suggested that the MC/MCN coatings provided not only mechanical strength but also satisfactory anticorrosion properties
10:40 AM B5-1-9 Oxidation Behavior of Arc-Evaporated TiSiN and AlTiSiN Coatings Deposited on Steel. In situ Approach of the Phenomena by Environmental Microscopy.
A. Mège-Revil, P. Steyer (INSA de Lyon, France); R. Chiriac, C. Sigala (UCBL-LMI, France); G. Thollet, C. Esnouf (INSA de Lyon, France)

In the past few years, the development of conventional TiN coatings was slowed down because of their too poor high temperature resistance. Fortunately, with an addition of silicon both mechanical properties and oxidation resistance were simultaneously improved, owing to the formation of a hard nanocomposite structure1,2. In this study, we intend to determine the oxidation behavior of coated steel by classical thermogravimetric measurements supported by an in situ investigation by environmental SEM (ESEM). Pure Ti, TiSi (80/20) and AlTiSi (60/30/10) targets were arc-evaporated to produce hard, single-layered coatings. Magnetron sputtered SiNx films were also synthesized for a comparison purpose. The hardness was measured using depth sensing indentation. The nanocomposite structure was confirmed by XRD and TEM. A continuous heating (1 K/min) was applied to assess the critical temperatures of oxidation. Isothermal tests were also performed at temperatures ranging from 973 to 1223 K to calculate the oxidation activation energies. Besides, 10-cycle runs (300-1073-300 K) were carried out and compared to the results obtained in the isothermal mode to evaluate the effect of the thermal fatigue. The susceptibility of SiNx to thermal shock is evidenced by ESEM as well as by thermogravimetric analyses. On the contrary, no cracking appears for Si-containing nanocomposite films. The beneficial role of this structure is again evidenced by the oxidation susceptibility (EaTiSiN = 260 kJ/mol vs. EaTiN = 190 kJ/mol), the oxidation rates (kinetic constants one decade lowered) and the oxidation temperatures (Tc delayed of 300 K with respect to TiN).

1P. Steyer, D. Pilloud, J.F Pierson, J.P. Millet, M. Charnay, B. Stauder, P. Jacquot, Surf. Coat. Technol. 201 (2006) 4158.

2D. Pilloud, J.F. Pierson, P. Steyer, A. Mege, B. Stauder, P. Jacquot, Mater. Lett. 61 (2007) 2506.

11:00 AM B5-1-10 Effect of the Oxygen Content on the Structure, Morphology, Thermal Stability and Oxidation Resistance of Cr-O-N Coatings
L. Castaldi (Empa, Switzerland); D. Kurapov, A. Reiter (OC Oerlikon Balzers AG, Liechtenstein); V. Shklover (ETH, Switzerland); P. Schwaller, J. Patscheider (Empa, Switzerland)
Cr-O-N coatings were produced at different N2/O2 flow ratios by cathodic arc deposition onto cemented carbide substrates. The structure, composition, and electronic properties of the coatings depend strongly on their oxygen content. The crystallite size of the nanocrystalline cubic Cr-O-N phase decreases at higher oxygen content and exhibit an enhancement of a (200) preferred orientation. The microstructure of the samples, studied by scanning electron microscopy (SEM), is columnar and becomes denser and smoother for the oxygen-rich cubic Cr-O-N coatings. The hardness of the coatings increases with increasing the oxygen content up to a value of 28 GPa. Higher oxygen contents lower the hardness of the coatings. X-ray powder diffraction (XRD) studies were performed in situ at high temperatures, in high-vacuum (HV) and in air. In general, the crystallite growth, occuring at elevated temperatures both in HV and in air, is hindered significantly by the presence of oxygen. The Cr-O-N coatings with the B1 structure, annealed both in HV and in air, provide an improved thermal stability, with no evidence of oxidation or the formation of the Cr2N phase up to 900°C.
11:20 AM B5-1-11 The Role of Al for the Structure and Performance of Al-Cr-N Coatings
K. Polychronopoulou (University of Cyprus); N. Demas (University of Illinois at Urbana-Champaign); M.A. Baker (University of Surrey, United Kingdom); E. Spain, J.C Avelar-Batista, J. Housden (Tecvac Ltd., United Kingdom); A.A. Polycarpou (University of Illinois at Urbana-Champaign); C. Rebholz (University of Cyprus)
Cr-N coatings are widely used to enhance the service life of tools and components. However, the concentration of chromium, e.g. in coolants during machining, can often exceed permitted tolerance limits, raising serious environmental concerns. The focus of this work is on Al-Cr-N coatings with Al/Cr ratios in the range of ~ 1 to 7 (and nitrogen concentrations of ~ 45 at. %) with the aim of replacing Cr with Al, and their comparison to Cr-N reference samples. Al-Cr-N coatings were deposited by co-evaporating Cr and Al material from a thermionically enhanced twin-crucible EB evaporation source at 450oC. The composition, structure, mechanical and tribological properties of the coatings were determined using X-ray photoelectron spectroscopy (XPS), X-ray diffraction (XRD) and transmission electron microscopy (TEM), in combination with nanoindentation, ball-on-disc sliding and (wet and dry) drilling experiments. XRD patterns for all Al-Cr-N coatings exhibited only reflections corresponding to Cr2N and metallic Cr phases. Hardness and elastic modulus values were found to vary between 25 to 30 GPa and 240 to 320 GPa, respectively, depending on the Al/Cr ratio. Al-Cr-N coatings presented higher hardness values and stresses (measured using a XRD sin2psi method) compared to reference Cr-N coatings. Ball-on-disc tests against Ruby counterparts revealed lower wear rates for Al-Cr-N coatings with Al/Cr - 4 compared to Cr-N coatings at room temperature and high temperatures (500 and 850°C). Al-Cr-N coated drills with Al/Cr = 1 and 7 showed an 11- and 4-fold increase in wet and dry cutting performance, respectively, compared to Cr-N reference coatings.
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