1 Corrosion of One-Step Superhydrophobic Stainless
2 Steel Thermal Spray Coatings
3 Samantha Michelle Gateman,a Kristopher Page,b Ilias Halimi,†a Alexandre Romão Costa
4 Nascimento,c Sylvio Savoie,d Robert Schulz,d Christian Moreau,c Ivan P. Parkin,b and Janine
5 Mauzerolla*
6 aLaboratory for Electrochemical Reactive Imaging and Detection of Biological Systems, McGill 7 University, Montreal, QC H3A 0B8, Canada
8 bMaterials Chemistry Department, University College London, London, WC1E 6BT, United 9 Kingdom
10 cThermal Spray and Multiphase Flow Laboratory, Concordia University, Montreal, QC H3G 11 1M8, Canada
12 dInstitut de recherche d'Hydro-Québec, Varennes, J3X 1S1, Canada
13 14 KEYWORDS. High-velocity oxygen fuel, thermal spray, coatings, stainless steel, 15 superhydrophobicity, surface chemistry, corrosion
16 ABSTRACT. As most superhydrophobic coatings are made of soft material, the need for harder, 17 more robust films is evident in applications where erosional degradation is of concern. The work 18 herein describes a methodology to produce superhydrophobic stainless steel thermal spray 19 coatings using the high-velocity oxygen fuel technique. Due to the use of kerosene fuel source, a
20 carbon rich film is formed on the surface of the thermal spray coatings, lowering the surface
1 21 energy of the high-energy metallic substrates. The thermal spray process generates a hierarchical 22 micro/sub-micro structure that is needed to sustain superhydrophobicity. The effect of spray 23 parameters such as particle velocity and temperature on the coating’s hydrophobicity state was 24 explored and a high particle velocity was shown to cause superhydrophobic characteristics. The 25 coatings were characterized using scanning electron microscopy, profilometry, X-ray 26 photoelectron spectroscopy, static water contact angle measurements, water droplet roll-off 27 measurements, and water droplet bouncing properties. The corrosion behavior of the coatings 28 was studied using potentiodynamic polarization measurements in order to correlate water 29 repellency with corrosion resistance, however, all coatings demonstrated active corrosion
30 without passivation. This study describes an interesting phenomenon where superhydrophobicity 31 does not guarantee corrosion resistance and discusses alternative applications for such materials.
32 INTRODUCTION. Over the past century, different types of thermal spray coating
33 technologies have emerged including high velocity oxygen spray1,2 plasma spray,3,4 and even cold
34 spray (i.e. near ambient temperatures) technologies,5 all of which are promising or have become
35 essential for the protection of industrial infrastructure.6,7 Various materials such as metals (wire,
36 powder, or rod),8 ceramics,3,9 and polymers10,11 have been thermally sprayed onto many different
37 substrates.12,13 The particles are (semi-) melted and accelerated to high velocities directed at the 38 substrate where they impinge and rapidly solidify to form a thin “splat”. The build up of splats 39 from successive impingement and interbonding results in a deposited coating, generally > 10 μm
40 thick.7 The resulting coatings are complex in microstructure, including oxides, pores/voids, and 41 unmolten particles.
42 Among the spray methods developed, high velocity oxygen fuel (HVOF) spraying, a variation 43 of combustion spraying, utilizes a special torch design that produces particle velocities so high
44 that they achieve supersonic values.7 Thus, the particles spread out upon impact and bond to the 45 substrate and to other neighboring splats to produce a well-bonded, dense coating. Depending on
46 the temperatures/velocities of the particles upon impact, molten and/or semi-molten particles and
2 47 debris can build up across the coating’s surface, resulting in a rough hierarchical micro and sub-
48 micron/nano structure.14,15 This surface texture is one of the two characteristics required to create a 49 superhydrophobic (SH) material, that is, a surface that measures a static water contact angle
50 (WCA) ≥ 150°, as well as a dynamic functional property – water bouncing.16,17 A SH material
51 and/or film must also have inherently low surface energy to minimize interactions with water.18 52 This can enable air to become entrapped between water droplets and the material’s surface, 53 leading to low adhesion. When the drop is resting on top of the asperities of the rough substrate,
54 the material is considered to be in the Cassie-Baxter state.19,20 The apparent (macro) contact angle
55 θapp of a water drop on a partially wetted surface is given by the weighted sum:
56 ����!"" = ����� − (1 − �) [ 1 ]
57 Where f is the fractional area of contact of water with the solid and θ is the contact angle on a 58 flat surface of the same material. In competition with the Cassie-Baxter state, the Wenzel state
59 describes when a water droplet impales a material with a rough surface and no air is entrapped.21 60 Although the WCA in the Wenzel state can be almost as high as found in the Cassie-Baxter state, 61 the two differ in the contact angle hysteresis, that is, the difference in advancing and receding
62 WCAs while tilting the specimen.22 Understanding the superhydrophobic state of a material is of
63 interest in this work as such characteristic has been linked to corrosion resistance.23,24
64 The biomimicry of superhydrophobic surfaces is of industrial interest for applications in self-
65 cleaning,18,25,26 drag-reduction,27,28 anti-icing,23 and anti-corrosion.23,29 Due to most polymers’ 66 deformation upon abrasion, it is advantageous to fabricate hard and wear resistant SH materials, 67 thus making thermal spray technologies a desirable hydrophobic coating method. Chen et al. 68 reported a simple route for constructing SH surfaces by flame spray deposition of inorganic 69 materials followed by the post application of a thin polytetrafluoroethylene (PTFE, Teflon®)
70 layer.14 Another example of thermal spray coating technology being utilized for SH applications
71 is the use of the HVOF method to fabricate robust hydrophobic Fe-based amorphous coatings.15
3 72 This method also required a post modification step to decrease the surface energy, which is 73 undesirable in industrial scale-up due to time and financial costs.
74 Recently, the fabrication of ceramic rare earth oxide (REO) thermal spray coatings has been
75 explored as a one-step method for producing SH durable coatings.9,30 By employing the thermal 76 spray technique named suspension precursor plasma spray (SPPS), REO can be applied to create 77 micro/nano scale textured surfaces over various substrates with static water contact angles as
78 high as 163°.31 The origin of REO hydrophobicity was proposed to be due to their unique
79 electronic structure that inhibits hydrogen bonding with interfacial water molecules,32,33 while
80 some recent studies countered with evidence that the adsorption of contaminates (volatile organic
81 compounds, CO2, etc.) is responsible for the apparent hydrophobic nature of the inherently
82 hydrophilic materials.31,34–36 Although the mechanism of wetting is still under debate, this method is 83 extremely advantageous since SPPS is industrially scalable, it eliminates the need for a surface 84 energy decrease post modification step, and the resulting coatings are extremely robust. Despite 85 their success and abundance, REOs are costly due to production difficulties encountered. For 86 instance, the lowest price for a REO in 2018 was 46 US$/kg for holmium oxide and the highest
87 being 123 US$/kg for praseodymium oxide.37 Therefore, more cost-effective materials and 88 methods for producing erosion resistant SH materials must be investigated.
89 This work is proposing a more economical solution by creating a one-step hard 90 superhydrophobic thermal spray coating using a stainless steel (SS), SS 444, precursor and a 91 long carbon chained fuel source. SS 444 is a less expensive alternative to other stainless steels
92 such as SS 316 and 304 as it has low nickel content but portrays similar corrosion resistance.38 To 93 our knowledge, this is the first report of achieving superhydrophobicity on HVOF metallic 94 coatings. Four different coatings were fabricated using varying spray parameters, specifically 95 temperature and velocity. The resulting coatings’ microstructures and surface chemistry were 96 characterized using scanning electron microscopy (SEM), profilometry, and X-ray photoelectron
97 spectroscopy, while the corresponding hydrophobic properties were investigated using static
4 98 WCA, water droplet bouncing experiments, and sliding angle measurements to identify optimal 99 spray parameters for maximum hydrophobicity. The corrosion behavior of the stainless steel 100 thermal spray coatings was observed in 3.5 wt% NaCl, which sparked an interesting discussion 101 regarding the correlation between a material’s corrosion resistance and hydrophobic state the 102 material exhibits.
103 EXPERIMENTAL SECTION
104 Materials and reagents. The feedstock material was water-atomized (by Eutectic Castolin, 105 Granby, Quebec, Canada) AISI grade stainless steel 444 powder produced by ArcelorMittal. The
106 substrates, also produced by ArcelorMittal, were wrought 6 x 10 inch SS 444 plates prepared 107 prior to HVOF spraying via alumina grit blasting (270 μm). The same material was used as the 108 substrate in order to minimize galvanic corrosion between the coating and underlying substrate. 109 Sodium Chloride and petroleum ether were purchased from Sigma-Aldrich. 110 Fabrication of thermal spray coatings. The metallic thermal spray coatings were prepared via 111 the high velocity oxygen fuel spray (HVOF) thermal spray method. The stainless steel powder 112 was first processed using high-energy ball milling (6h) to decrease the as-atomized particle size 113 (>100 μm) and then sieved to a mean particle diameter of ~45 μm, as seen in the supporting 114 information (Figure S1). A Praxair’s JP-8000 HVOF spray gun with a gun barrel length of 4 in 115 was used for spraying all coatings. A powder feed rate of 44 g/min, stand-off distance of 13 in, 116 transversal speed of 0.5 m/s with a pitch step size of 10 mm, and 15 passes were performed to 117 create approximately 500 μm thick coatings (specifics in table S1) on wrought SS 444 plates (6 x 118 10 inch). No substrate cooling system was used. The oxygen and kerosene fuel flow rates were 119 varied to produce four velocity/temperature conditions between 500-800 m/s and 1600-2100°C. 120 Small circular coupons (16 mm in diameter) were water cut from the sprayed plates for further 121 investigation. 122 The parameters used to fabricate the SS 444 HVOF coatings can be found in table 1. The 4
123 coatings were deposited using different oxygen to fuel flow rate ratios and combustion pressures:
5 124 low velocity and low temperature (LVLT), high velocity and high temperature (HVHT), low 125 velocity and high temperature (LVHT), and high velocity and low temperature (LVHT). The 126 particles in-flight characteristics were measured using DPV-evolution system. Similar to what
127 has been shown in previous modeling studies,39,40 the particle velocity and temperature are directly 128 proportional to the combustion pressure and O/F ratio, respectively. 129 130 Table 1. HVOF thermal spray parameters used to deposit four SS 444 coatings using different
131 combustion pressure (psi) and oxygen to fuel (O/F) ratios.1
Sample O2 Flow Rate Kerosene Flow O/F Pressure Velocity Temperature (LPM) Rate (LPM) Ratio (psi) (m/s) (°C)
LVLT 470 18 0.80 54 546 ± 70 1658 ± 300
HVHT 870 23 1.17 100 790 ± 100 2107 ± 250
LVHT 588 15 1.18 60 524 ± 80 2122 ± 200
HVLT 729 28 0.80 95 792 ± 101 1569 ± 320 132 133 Microscopy Characterization. All SEM images were obtained using a Hitachi SU3500 variable 134 pressure scanning electron microscope. Topographic information was obtained by collecting the 135 secondary electron signal produced from the specimen itself while elemental composition 136 information was explored via detection of back-scattered electrons stemming from the incident
137 beam and X-ray emissions. The fraction of coatings microstructural features of SEM cross- 138 section images was determined by Image analysis using the software Image J 1.52A (National 139 Institute of Health, USA). All confocal microscopy data was recorded using a white light 140 interferometry profiler (Zygo Nexview) at 10x magnification using Mx™ Software. All
1 Abbreviations stand for: low velocity and low temperature (LVLT), high velocity and high temperature (HVHT), low velocity and high temperature (LVHT), and high velocity and low temperature (LVHT). The in-flight particle characteristics, velocity and temperature, are the average and standard deviation of 1000 particles measured.
6 141 roughness parameters, i.e., mean height (Sa), Skewness (Ssk), sharpness (sku), and peak spacing (sm), 142 of the coatings were recorded in triplicate and tabulated using Mx™ Software.
143 X-ray photoelectron spectroscopy. Chemical analysis of the carbon rich films on the HVOF 144 coatings surfaces was carried out using an Al K-Alpha X-ray photoelectron spectrometer 145 (ThermoFisher). The spot size was 400 μm and 10 scans were performed per spectrum. 146 Water contact angle, roll-off angle, and bouncing measurements. A 30 μL-sized droplet of 147 distilled water was transferred onto each of the HVOF coatings using an automated syringe 148 pump. The water contact angles were measured at ambient temperature using an optical contact
149 angle meter (FTA 1000) and fit to the Young-Laplace equation. The WCA measurements were 150 carried out 3 times on 2 different coupons to collect enough data for statistical comparison. The 151 same set up was used for the water rolling angle measurements where the stage was tilted at a 152 speed of 0.5° per second until 90° was reached. 153 Water roll-off angle tests were carried out using a 1 mL syringe to dispense 10 μL-sized 154 droplets. The water bouncing measurements were performed at a height of 15 cm from the 155 coating substrate. Both measurements were done at least twice on 2 different coupons for each 156 coating to confirm reproducibility. The videos were taken by a high-speed video camera (FPS 157 1000 HD, Slow Motion Camera Company, United Kingdom) capturing at 1000 frames per 158 second. 159 Potentiodynamic polarization measurements. Electrochemical measurements were performed 160 using a multi-channel VSP-300 potentiostat (BioLogic Science Instruments, USA) with 1 μV 161 resolution. Experimental parameters for PDP measurements were based on the relevant ASTM
162 G-61 test method.41 Briefly, the coatings were immersed at open circuit potential (OCP) for 1h 163 before applying a potential bias. Polarization commenced -250 mV lower than the measured 164 OCP and was linearly polarized to more anodic potential using a scan rate of 0.167 mV/s until a
165 current density of 0.5 mA/cm2 was reached. A standard bench top corrosion cell (K0235 Flat
166 Cell, Princeton Applied Research, AMETEK® Scientific Instruments) with an isolated area of 1
167 cm2 was used as the main corrosion cell for all measurements. A calibrated saturated calomel
7 168 electrode (SCE) and platinum mesh were used as the reference and counter electrodes 169 respectively. A Faraday cage and a vibration isolation table were used during measurements. 170 In order to minimize solution resistance and to simulate harsh corrosion conditions, 3.5 wt% 171 NaCl electrolyte made using deionized water from a Milli-Q® water purification system (18.2 172 MΩ cm resistivity) was chosen as the main test solution for immersion testing and standard 173 electrochemical measurements. All measurements on bulk SS 444 were performed on 174 sandblasted substrates in attempt to introduce surface roughness. PDP measurements on thermal 175 spray coatings were performed on as sprayed, non-polished samples. The true surface areas of 176 each coating, tabulated from the confocal microscopy data, were used to calculate corrosion
177 current densities. All polarization tests were carried out for at least 3 replicates to ensure 178 reproducibility of the material’s corrosion behavior. 179 RESULTS AND DISCUSSION 180 Microstructural and chemical characterization of coatings’ surfaces. The microstructural 181 features of HVOF coatings (Figure 1) are non-molten powdered particles and re-solidified 182 metallic material that protrude from the surface. The semi-molten, molten, and oxidized metal 183 debris from the impact with the substrate is seen scattered across the coatings’ surface in the 184 magnified inset images (Figure 1). The sub-micron structure features created from molten 185 material flying off of the heated powdered particles upon impact complete the hierarchical 186 surface texture that is required to produce a superhydrophobic material.
8 187 188 Figure 1. SEM images revealing the micro and sub-micron (inset) hierarchical structures of the 189 steel HVOF coatings for each set of parameters where the scale bar is 1 mm: low velocity high 190 temperature (LVHT), high velocity high temperature (HVHT), low velocity low temperature 191 (LVLT), and high velocity high temperature (HVLT). The inset images have a scale bar of 10 192 μm.
193 194 Differences in microstructure can be seen between each of the HVOF coatings’ SEM images. 195 The coating fabricated using low velocity and high temperature (LVHT) shows a surface texture 196 that is consistent in size to that of the powdered SS particles used to fabricate the coatings (~45 197 μm, supporting information Figure S1) as seen in Figure 1. The coatings made using HVHT and 198 LVLT show a more molten surface texture, with protrusions of powdered particles more spread 199 out than seen in the LVHT coating. The coating created using HVLT has larger protrusions 200 (>300 μm) and a cauliflower-like surface microstructure. A similar unique microstructure has
201 been documented for some SPPS coating methods due to the deposition of the material having a
9 202 significant velocity component parallel to the substrate.42,43 The submicron structure formed during 203 the HVOF process is random and no apparent differences between the coatings were observed.
204 205 Figure 2. Top panel: Topography images of each SS HVOF coating and their average surface 206 roughness values and associated standard error of the mean for 3 measurements. Bottom panel:
10 207 A 1 mm line scan across HVLT coating revealing its micro textured surface and the inset 208 showing the material’s sub-micron structure. All scale bars represent 200 μm.
209 210 Topographical imaging and analysis were performed for each coating, as surface roughness 211 and parameters are critical for producing a superhydrophobic material. The lowest mean surface 212 roughness (height) was measured for the coating produced at high velocity and high temperature, 213 HVHT, as seen in the topography image presented in the top panel of Figure 2. This may be due 214 to the ability of the molten particles to flatten and pack together when striking the substrate due 215 to the high amount energy and flexibility they posses upon impact. Large cauliflower protrusions 216 greater than 300 μm in diameter are observed on coating HVLT as seen in Figure 2 bottom 217 panel. Although the powder diameter is about 45 μm, some smaller, 1-2 μm sized particles are 218 present in the feedstock. Therefore, the columnar/cauliflower pattern could be due to either
219 horizontal flow of fine, primary powder particles,42 or to perturbation in the deposition of primary
220 particles.44 This coating has the highest surface roughness of 13.7 ± 0.8 μm, which may be caused 221 by the lower particle temperature decreasing deformation capabilities on impact. All coatings 222 showed a sub-micron textured surface at 100x magnification as seen in Figure 2 bottom panel 223 consisting of sub-micron peaks both in height and width protruding from the coating’s surface 224 where the peaks are separated by ~ 2 μm.
225 We also report the skewness of peaks (Rsk), sharpness of peaks (Rku), and the average spacing 226 between peaks (S) for all coatings in table 2. All HVOF coatings portray positive skewness 227 values, which correspond to non-symmetric, predominance of peaks comprising all of their 228 surfaces. The roughest coating, HVLT, showed the lowest degree of symmetry of all the coatings
229 with a large Ssk value of 0.68 ± 0.12. This coating also showed a kurtosis value greater than 3, 230 indicating a perfectly random spikey surface as opposed to the other bumpy HVOF coatings with 231 values less than 3. The average spacing between peaks was also larger for the HVLT coating in 232 comparison to the rest of the HVOF materials. All of these parameters may have an affect on the
233 coatings’ hydrophobicity and will be taken into consider in following sections.
11 234 235 Table 2: Tabulated surface parameters for each coatings fabricated: mean height of the 236 roughened surface, skewness of the peaks, kurtosis of the roughness profile, and the average 237 spacing between peaks and associated standard errors the mean.
Sample Mean Height, Ra Skewness, Rsk Sharpness, Rku Peak Spacing, Sm LVLT 10.6 ± 0.6 0.14 ± 0.02 2.8 ± 0.3 61 ± 3 μm HVHT 9.5 ± 0.1 0.15 ± 0.04 2.8 ± 0.2 61 ± 10 μm LVHT 11.4 ± 1.3 0.40 ± 0.09 2.9 ± 0.4 60 ± 4 μm HVLT 13.7 ± 0.8 0.68 ± 0.12 3.3 ± 0.3 80 ± 7 μm 238 239 X-ray photoelectron spectrometry was used to identify and quantify surface carbon species on 240 all of the HVOF coatings. Using an Al K-Alpha X-ray source with a beam size of 400 μm and 241 the sample surface normal to the detector, C 1s peaks were obtained for each coating (Figure 242 3A). All spectra are convoluted with three peaks assigned to C-C, (284.5 eV), C-O (285.6 eV), 243 and C=O (288.2 eV) and seen in Figure 3B, where all coatings contain mostly graphite structured 244 carbon, probably due to the high amount of carbon residue from the kerosene fuel source. The 245 presence of C-O and C=O peaks indicates the existence of organic contaminants via adsorption 246 from the atmosphere, as previous studies have confirmed that metal and metal oxides can
247 spontaneously adsorb organic materials, lowering their surface energy.45–47 Surface chemical 248 analysis was performed much later than the amount of time needed to plateau the WCA from
249 atmospheric carbon adsorption (>7 days),47 so it is expected to observe such peaks. The amount 250 of oxygen-containing adsorbed carbon from the atmosphere is similar for all coatings, while the 251 C-C peaks seem to vary between coatings. The C-C peaks documented here are much larger than
252 what has been seen for similar studies reported on Fe-based thermal spray coatings,47 indicating 253 that the increase in carbon content is due to the use of the kerosene fuel source. The amount of 254 graphite-like carbon was much larger for the HVHT coating than the rest of the coatings studied,
12 255 while the counts for the LVHT coating is lower. This may be due to the high and low kerosene 256 flow rates used to make each coating, respectively.