Mathematical Modeling and Numerical Simulation of Splat Cooling in Plasma Spray Coatings
H. Fukanuma, R. Huang, Y. Tanaka, and Y. Uesugi
Particle deformation and cooling significantly affect the characteristics of thermally sprayed coatings, such as the adhesion and cohesion strength between a splat and a substrate and between splats, as well as the internal stresses of deposits. It is essential to understand these processes for the successful industrial application of thermal spray technology. However, to date, the microstructure of the boundary of a splat and the substrate has not been clarified, although much research has been conducted on splat formation and the cooling process. We have developed a microstructure model of the boundary between the splat and the substrate, based on splat morphology obtained from experiments. In the model, it is assumed that gaps, or voids, and contact areas are arranged on the splat boundary with the substrate in an orderly fashion. The model includes phase changes and heat resistance simulating the function of the micro- structure during splat cooling. Assumptions in the model are that ambient gas trapped in the gaps, or voids, transfers heat only by conduction and not by convection or radiation. The results of the simulation indicated that the extent of gaps, or voids, significantly affects the rate of decrease of the average temperature of the splat surface, as well as the temperature distribution inside the splat.
The deformation of a splat and its cooling affect adhesion, cohesion, porosity, and residual stress of plasma sprayed deposits. It has been shown that adhesion and cohesion are influenced by the characteristics of the impinging particles such as velocity and molten state, as well as by the substrate characteristics, such as tempera- ture and oxidative state (Ref 1). Bahbou et al. (Ref 2) have shown that substrate conditions influence the cooling rate of particles, as well as the flattening speed. Arata et al. (Ref 3) have reported that plasma sprayed deposits contain gaps (nonbonded interfaces) between splats. By measuring the curvature of a substrate in situ during plasma spraying, Kuroda et al. (Ref 4) have shown that the tensile stress depended on substrate temperature, as well as spray materials and characteristics.
Research on splat morphology and flattening ratios as well as particle splash has been conducted (Ref 5-10). Fukumoto et al. (Ref 5, 6) have suggested that above a certain temperature, molten particles do not splash when they impinge on a smooth flat surface. Li (Ref 7) has indicated that substances adsorbed on a substrate cause splat splashing because of evaporation resulting from heating by the molten droplet during its spreading.
Splat cooling rates during thermal spray coating pro- cesses depend signiflcantly on the microstructure of the interface between the splat and the substrate, and on the splat and substrate materials (Ref 1, 2, 11, 12). Trapped ambient gas in pores, or gaps, causes heat resistance that affects the splat cooling rates. Although many studies have been conducted on splat forming and cooling, few studies have focused on the microstructure of the boundary between a splat and the substrate. Moreover, to date, actual contact ratios of splat/substrate boundary and defects such as gaps, or pores, on the boundary have not been clarified. Amara et al. (Ref 13) have presented a three-dimensional (3D) computational model of heat transfer between a splat and a substrate based on a splat/substrate interface model, in which contact spots were randomly distributed. The model indicated that when the contact was perfect, the thermal conductivity was equal to that of the substrate materials, whereas when it was imperfect, the thermal conductivity was equal to that of the gas trapped in the noncontact areas. McDonald et al. (Ref 11) have studied a one-dimensional heat conduction model with uniform thermal contact resistance between the splat and sub- strate. The thermal resistance of the splat/substrate interface was determined based on the model by experi- ments that measured Mo and ZrO 2 splat cooling rates on glass and Inconel substrates.
In this study, we first sprayed metal particles onto glass substrates and photographed the splat patterns. Then, a splat/substrate boundary model was developed by simpli- fying the complicated morphology of the splat bottom faces we observed. The splat bottom face was divided into two parts consisting of perfect contact and noncontact areas that were placed on the face in an orderly way. It was assumed that the noncontact regions were filled with ambient gas. In order to clarify how different the tem- perature, or cooling rate, is between the portion above the perfect and that above the imperfect contact boundary, a mathematical model was developed. This model was based on the interface model that included phase changes. A 3D simulation was conducted to see how the model functioned.
2. Modeling of Splat Cooling
2.1 Splat/Substrate Interface Model
Nickel (Ni), aluminum (Al), and molybdenum (Mo) particles were sprayed onto smooth flat glass substrates with a SG-100 plasma torch (Praxair, Inc., Danbury, CT, USA), and the top and bottom views of captured splats were photographed. Both top and bottom views of typical splat examples obtained from our plasma spray experi- ments are shown in Fig. 1. The photographs in Fig. 1 show the top and bottom faces of Ni, Al, and Mo splats: (a) and (b) show the top and bottom views of a Ni splat, respec- tively. Figure 1(c) and (d) show top and bottom views of Al, and Fig. 1(e) and (f) top and bottom views of Mo splat. Many trenches or ditches are clearly seen extending from the centers of the Ni and Al splats to their peripheries in the bottom views in (b) and (d) of Fig. 1. No such trenches are seen in the photographs of the top views. It appears that in these trenches the bottom of the splat does not contact the glass substrates. The trenches may be gener- ated by ambient gas that was trapped under the particle because the flattening speed was too fast to blow the gas out from under the particle. Fine lines or trenches, however, are seen in both top and bottom views of the Mo splat. The lines on the top face might be generated in a different way from the ones on the bottom face. We do not understand how the fine lines on the top were formed. The fine lines on the bottom face could have formed as a result of the long time taken for the molten molybdenum particle to solidify; therefore, the lines became finer because most of the initially trapped gas gradually escaped from beneath the particle by the time the solidification was completed. In any event, there are radial trenches, or lines, running on the bottom view of every splat. On the other hand, none of the center areas of the bottom views had trenches, and those central areas made contact with the substrates, albeit some small defects that could be seen.
We developed a splat morphological model on the basis of the results of the above experiments. In this model, radial trenches stretch on the bottom face of the splat as shown in Fig. 2, under the assumption that at the moment when the flattening process of the particle finished (no further expansion), the splat morphology was completed, or fixed, even if the material was in a molten state.
In the model, the outer radius and thickness of the splat were R p and H p , respectively. We created a trench by aggregating some finer trenches shown in the bottom view of the splat. The dimensions of the trench were de fined: the central angle of the sector, the depth, and the length were u, h, and R p ! R 0 , respectively, where R 0 was the radius of the inner contact area. Each trench was distrib- uted at every angle of w over the splat. The substrate radius and thickness were R s and H s in the coordinate system as is shown in Fig. 3.
2.2 Mathematical Modeling and Solution Method
The splat and substrate temperature T a function of time t is written in cylindrical coordinates:
where q, c, k, L m , and f L are density, specific heat, thermal conductivity, latent heat, and local liquid fraction, respectively. The last term in Eq 1 shows that phase changes are taken into consideration in the splat solidification process using the enthalpy method (Ref 13, 14). In the numerical calculation, the solidification temperature range was taken as 10 “C between (T m + 9) and (T m ! 1) in order to save calculation time. It was assumed that the radiative and convective heat transfer from plasma jet to the splat/substrate system was negligible; therefore the boundary condition of the top face of the system and the splat side face was adiabatic. The heat transfer through the interfaces between the gas trapped in the trenches and the splat or the substrate was assumed to be conductive with neither convection nor radiation in the trenches. It was also assumed that the boundary conditions of the cylin- drical and bottom walls of the substrate were at a constant temperature. Figure 4 illustrates the boundary conditions so the reader can quickly comprehend the complicated conditions mentioned previously. The calculation domain is shown in Fig. 5. The number of cells was 347,072 in the domain. The time step for computation was 10! 9 s. The simulations were conducted with commercially available software, Fluent 6.3 (ANSYS, Inc., Canonsburg, PA, USA), which uses finite volume schemes. Thermo- physical properties of materials and the dimensions of the splat/substrate system are shown in Table 1 and 2, respectively. We selected four central angles ‘‘u’’ of 0, 2, 6, and 10” for the computation. At these angles, the ratios of the splat making contact with the substrate were 100, 90.4, 71.2, and 52.0%, respectively. The contact ratios were obtained by the formula:
3. 3D Computational Simulation Results and Discussion
Images of the computational results for the tempera- ture distributions in cross section of the splat and substrate systems including the trench with an angle ‘‘u’’ of 0, 2, 6, and 10″ are shown in Fig. 6. At 10! 8 s after splat cooling began, the splat with 100% contact with substrate uni- formly decreased in temperature. However, in the other three splats with imperfect contact with the substrates, the temperature fell around the center portions. At 10! 7 s, the temperatures in splats with 100 and 90.4% contact fell uniformly faster than those with 71.2 and 52.0% contact. The temperatures in the peripheries were much higher than those in the centers for u = 6 and 10″, because the trenches resisted heat transfer. The peripheral tempera- tures of the splats were higher on the order of 52.0, 71.2, 90.4, and 100% contact ratio. At 10! 6 s, the temperature of the splat with 100% contact fell almost uniformly to 1500 “C from the original temperature of 3500 “C; the peripheral temperature of the 52.0% contact splat, how- ever, was still higher than 2500 “C. There was a difference of 1000 “C between the splats. It is clear that the heat resistance of air trapped in the trenches was significant.
At 10! 5 s, all the temperature distributions become nearly identical. It appears that when contact ratios are less than approximately 70%, the temperature distribution in the splat becomes uneven. The simulations indicated that noncontact interfaces between splats and substrates significantly affected cooling rates. Images of the temperature distribution on the upper side of the splats are shown at 10! 7 , 10! 6 , and 10! 5 s in Fig. 7. The temperature distribution of the splat making perfect contact with the substrate shows that the temper- ature differences on the top were less than 200 “C at each time period. Moreover, in these splats, the temperature of the periphery was lower than that of the center. On the other hand, for the splat with 52.0% contact, the tem- perature differences on the top were more than 500 “C at 10! 7 s and about 1000 “C at 10! 6 s. The temperature above a trench was much higher than that above a contact point. It can be seen that at 10! 7 and 10! 6 s the temper- ature distribution images for the top were identical to the configuration of trenches. Moreover, the temperature of the periphery, above the trench, was much higher than that of the center. At 10! 5 s, the temperature of the periphery became lower than that of the center for all contact ratios. In Fig. 8, the average temperatures on the top faces with 100, 90.4, 71.2, and 52.0% contact with the substrate are shown against the passage of time. It is clear that the cooling rates for the splats with 100 and 90.4% contact were identical. The cooling rates for the splats with 71.2 and 52.0% contact were slower than those for the splats with 100 and 90.2% contact. The average surface tem- perature of the splat with 52.0% contact decreased more slowly. The temperature on the splat with 52.0% contact was nearly 500 “C higher than that on the splat with 100% contact after about 0.5 ls. The gradient for the curves was gradual at 0.1 to 0.5 ls because of the effect of latent heat. The infiuence of latent heat on cooling time was relatively small, because the time to needed to solidify was only 0.1 to 0.2 ls. The definition of the average temperature T av is written:
where T p is the top surface temperature of the splat and S is the area of the top surface.
The splat temperature cooling curves at the center and at the periphery above the contact and the noncontact points are shown for the splat with 52.0% contact in Fig. 9. It can be seen that the temperature on the periphery above the noncontact point fell slowly compared with that at other points until 3 ls, then, it became similar to that of other points, and finally the temperature became lower than that of the center. The temperature was signiflcantly higher than that of the other points until nearly 2 ls and the temperature deference was more than 1000 “C around 1 ls. This indicates that the trenches or gaps filled with ambient gas play a critical role in the splat cooling process. Figure 10 shows that from the start, the temperature at the rim of the splat that made perfect contact cooled faster than the temperature at the center.
As for the validity of our splat morphology and cooling model, the authors compared their calculated results with experimental results conducted by McDonald et al., who have reported that the cooling rate of Mo splat on a pre- heated Inconel substrate was 22 9 10 7 K/s at the splat temperature of 2300 “C (Ref 12). In the model, the cooling rates of Mo splat on Fe substrate were 354 9 10 7 and 158 9 10 7 K/s at 2250 “C of splat temperature when the contact ratios were 100 and 52.0%, respectively. The cooling rate even in the case of 52.0% contact was one digit larger than that of Mo splat on Inconel in McDonald!s experiments.
Both cooling curves were similar, although these cooling rates were different. More experimental results on splat cooling are necessary to appreciate precisely the model since cooling rates depend on many factors such as the microstructure of the boundary between a splat and a substrate, splat thickness and diameter, substrate materi- als, and temperature.
4. Summary and Conclusions
A splat/substrate interface model was created by ana- lyzing the morphology of Ni, Al, and Mo splats sprayed onto glass using a plasma torch. The splats contained many fine lines, or microscopic trenches, on the bound- aries between the glass substrate and the splats. The model was characterized by grouping many radial lines into a number of fine trenches, or ditches, on the splat bottom for mathematical modeling and computation. The assumptions of the model were (1) that the trenches were filled with ambient gas that acted as heat resistance during the splat cooling, and (2) that the boundary conditions on the interfaces between the gas trapped in the trenches and the splat, or the substrate, were only conductive, such that radiative and convective heat transfers inside the trenches were not taken into consideration in the com- putational simulations of the splat cooling process. The splat cooling rates depended signiflcantly on the ratios of noncontact areas occupied by the trenches filled with ambient gas. The average temperature on the top face of the splat that had more noncontact areas fell more slowly than that of the splat with fewer noncontact areas. The temperature on the top face above a trench cooled much slower than that above a contact position. The temperature gap between the positions above the trench and the contact point was more than 1000 “C in the case of the splat in which the trench had 10” of central angle. The images of temper- ature patterns on the top faces were the same as the distri- bution of trenches in the splats. The simulation results showed that the trapped ambient gas on the boundary between the splat and the substrate plays a critical role in the splat cooling process. Further research on the mor- phology of the splat/substrate interfaces is needed to clarify how the microstructure of the boundary is formed in order to further understand the cooling processes.
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