# The Influence of Anode Inner Contour on Atmospheric DC Plasma Spraying Process

Authors: Kui Wen; Min Liu; Kesong Zhou; Xuezhang Liu; Renzhong Huang; Jie Mao; Kun Yang; Xiaofeng Zhang; Chunming Deng; Changguang Deng
Journal: Advances in Materials Science and Engineering
 (2017)

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## Abstract

In thermal plasma spraying process, anode nozzle is one of the most important components of plasma torch. Its inner contour controls the characteristics of plasma arc/jet, determining the motion and heating behaviors of the in-flight particles and hence influencing the coating quality. In this study, the effects of anode inner contour, standard cylindrical nozzle, and cone-shaped Laval nozzle with conical shape diverging exit (CSL nozzle) on the arc voltage, net power, thermal efficiency, plasma jet characteristics, in-flight particle behaviors, and coating properties have been systematically investigated under atmospheric plasma spraying conditions. The results show that the cylindrical nozzle has a higher arc voltage, net power, and thermal efficiency, as well as the higher plasma temperature and velocity at the torch exit, while the CSL nozzle has a higher measured temperature of plasma jet. The variation trends of the plasma jet characteristics for the two nozzles are comparable under various spraying parameters. The in-flight particle with smaller velocity of CSL nozzle has a higher measured temperature and melting fraction. As a result, the coating density and adhesive strength of CSL nozzle are lower than those of cylindrical nozzle, but the deposition efficiency is greatly improved.


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## Body

## 1. Introduction

Thermal plasma spraying has been widely used to prepare high quality coatings, such as wear-, corrosion-, and oxidation-resistant coatings [1, 2] and thermal- and environmental-barrier coatings [3, 4]. Although a large number of experimental and modeling results concerning the plasma spraying process have been published [5–7], the complicated interactions of the plasma with electromagnetic, thermal, and acoustics phenomena are still not fully understood [8]. In plasma spraying, the anode nozzle is one of the key components of the plasma torch. Slight geometrical structure modification will result in a strong change in the length and stability of the plasma arc, the characteristics of plasma jet, and the thermal efficiency of plasma torch. The effects of anode nozzle on the plasma spraying process can be summarized in the following two aspects. First, the anode outer contour controls the formation and the intensity of turbulence that affects the cold ambient air entrained into the plasma jet [9, 10]. Secondly, the anode inner contour determines the behavior of plasma arc inside the torch and the distributions of plasma jet temperature and velocity. Both factors will ultimately influence the coating quality, such as porosity and adhesive strength. In addition, compared with the anode outer contour, the inner contour plays a more important role in the plasma spraying process.With regard to the vacuum plasma spraying (VPS), Cao et al. [11] reported that the plasma temperature gradient of Laval nozzle, consisting of a convergent part, a cylindrical channel, and a bell-shaped divergent exit (CCD-bell nozzle), was smaller than that of standard cylindrical nozzle (cylindrical nozzle), and it can improve the deposition efficiency and density of coatings. Rahmane et al. [12] proved that the length of the bell-shaped part also had a significant effect on the plasma jet characteristics. As the pressure decreased, the plasma jet of the longer CCD-bell nozzle reached the supersonic state, while that of the shorter one was still in the subsonic state. Certainly, only when the working parameters were set properly, the Laval nozzle could accelerate the plasma jet to supersonic and improve the plasma spraying process [13].As for the atmospheric plasma spraying (APS), Henne et al. [9, 14] proved that the CCD-bell nozzles were useful for reducing the entrainment of cold ambient air and extending the axial length hot core of the plasma jet, and also the corresponding coating qualities and deposition efficiency of the Laval nozzle were improved. In addition, Schwenk et al. [15, 16] designed several Convergent-Divergent Laval nozzles with bell-shaped diverging exit (CD-bell nozzle). In contrast to the cylindrical nozzle, these CD-bell nozzles can gain lower arc voltage fluctuations and acoustic levels and higher thermal and deposition efficiency, while there is no significant difference in porosity and adhesive strength.Obviously, the aforementioned investigations mainly focused on the effects of cylindrical nozzles and bell-shaped Laval nozzles on the APS process. Studies with regard to the Laval nozzle with conical shape diverging exit (CSL nozzle) were seldom reported. In our study, we have found that the deposition efficiency is improved by the CSL nozzle, but the corresponding adhesive strength is reduced. It is different from the results of the bell-shaped Laval nozzles that are reported in the previous work. The difference in those results indicated that the intrinsic relationship between the anode nozzle and the coating had not been fully revealed.In this paper, in order to clarify the effects of anode inner contour of cylindrical nozzle and CSL nozzle on plasma spraying process under APS conditions, the plasma jet characteristics, in-flight particle motion and heating behaviors, and coating properties were systematically investigated.


## 2. Experimental Details

### 2.1. Plasma Torch

At present, most commercial plasma torches applied in APS use anodes with cylindrical channel, and some also use anodes with Laval-like diverging exits. Therefore, all the following experiments were performed by the F6 atmospheric plasma spraying facility (GTV GmbH, Luckenbach, Germany), which was equipped with two different inner contour anode nozzles. Figure1(a) shows a cylindrical nozzle with an exit diameter of 6.0 mm and a cylindrical channel length of 20.0 mm. The schematic of a CSL nozzle is shown in Figure 1(b), the corresponding throat and nozzle exit diameters are 7.0 mm and 12.5 mm, and the axial length of the divergent part is 26.0 mm. In addition, it is worth mentioning that the total length of the CSL nozzle is 2.0 mm longer than that of the cylindrical nozzle.Figure 1
Schematic diagrams of anode nozzle inner contour: (a) cylindrical nozzle and (b) CD-conical nozzle.
(a)
(b)


### 2.2. Diagnostic Equipment

The enthalpy probe system (Tekna Plasma Systems Inc., Canada) and DPV-eVOLUTION system (Tecnar Automation Ltd., Canada) were used to measure the characteristics of plasma jet and in-flight particles, respectively. The plasma temperature was obtained by calculating the energy balance of the circulating cooling water in the enthalpy probe, while the Bernoulli equation was used to calculate the local velocity for low Mach number gas flow. The external and internal diameters of the enthalpy probe are 4.76 mm and 1.32 mm, and the corresponding area of orifice is 1.368 mm2. The shortest measurement distance to the nozzle exit was set at 60 mm to avoid thermal overload of the probe tip. In-flight particle velocity, temperature, and diameter were measured by an optical sensing device DPV-eVOLUTION system. The surface temperature of the particle was measured by a high precision two-color pyrometer based on Planck’s radiation law, which assumes the in-flight particles are gray body emitters with the same emissivity at both color bands. The velocity (V) was calculated by multiplying the real distance (S) of the slits on the photomask by the magnification factor (K) of the lens and then dividing the “time of flight” (t) between the two peaks of the particle signal; namely, V=S×K/t. It is worth mentioning that the powder particles were radially injected into the plasma jet. More detailed theoretical information on the two measurement systems can be found in [17–20].Figure2 depicts the relative position of plasma torch and enthalpy probe system, while the DPV-eVOLUTION is located at the same position as the enthalpy probe system. Plasma torch was mounted on the six degrees of freedom robot to ensure the axis of the plasma torch coinciding with the axis of the enthalpy probe tip. The axial test positions (z-direction) of the plasma jet can be adjusted by liner movement of the plasma torch along the axis, while the radial test positions (x-direction) were controlled by the displacement controller.Figure 2
The relative position of the enthalpy probe and plasma gun.


### 2.3. Preparation of Al2O3 Coatings

A bulk AISI 1045 steel sheet with a dimension ofΦ25.4×6.0 mm was employed as the substrate. Since aluminum oxide coatings have a wide range of industrial applications, a commercial fused Al2O3 powder (5–22 μm, HC Stark GmbH, Germany) was selected as feedstock in the experiments, as shown in Figure 3. Argon was chosen as the carrier gas (5 slpm, standard liter per minute), the inner diameter of the feedstock injector is 1.5 mm, and the corresponding powder feed rate is 16.25 g/min. Other detailed spraying parameters are shown in Table 1. Note that a NiAl layer is deposited on the substrate as bonding coating prior to the deposition of Al2O3. Microstructures of the Al2O3 coatings were characterized by scanning electron microscopy (Nova NanoSEM 430, FEI, Netherlands). The adhesive strength was performed through tensile adhesion test on a universal mechanical test machine (GOPOINT Testing Equipment Co., Ltd., China) based on the ASTM C633-01 standard [21]. Three specimens for each spraying distance (90, 110, and 130 mm) were tested to obtain the mean adhesive strength and relative deposition efficiency (RDE). The latter is defined as the average increment of coating weight per spraying cycle, namely, the weight of Al2O3 coating divided by the total number of spraying cycles.Table 1
Spraying parameters for online measurement and Al2O3 coatings deposition.
Case
Current (A)
Ar (slpm)
H2 (slpm)
Spraying distance (mm)
I
650
40
10
60–150
II
450, 550, 650
40
10
90
III
550
40, 50, 60, 70, 80
10
90
IV
550
60, 62, 64, 66, 68
10, 8, 6, 4, 2
90
V
650
40
10
70, 90, 110
VI
650
40
10
90, 110, 130
Note. (1) Case III, the flow rate of H2 maintains 10 slpm; (2) Case IV, the total flow rate of mixture gas is 70 slpm.Figure 3
The morphology of fused Al2O3 powders.


### 2.4. Spraying Parameters

In the actual industrial production, the adjustable spraying parameters are mainly working current, plasma gas composition, and flow rate. Therefore, it can better understand the spraying process of the two nozzles under different conditions by changing these parameters, which can provide experimental basis for the production process. The spraying parameters used in diagnostic measurement and coating fabrication are given in Table1. Case I was used to measure the axial and radial distribution of plasma temperature and velocity. Case II, Case III, and Case IV were applied to investigate the influence of working current, argon flow rate, and hydrogen content on the plasma jet characteristics. Case V allowed measuring the in-flight particle temperature and velocity. Case VI was used to deposit the Al2O3 coatings.


## 2.1. Plasma Torch

At present, most commercial plasma torches applied in APS use anodes with cylindrical channel, and some also use anodes with Laval-like diverging exits. Therefore, all the following experiments were performed by the F6 atmospheric plasma spraying facility (GTV GmbH, Luckenbach, Germany), which was equipped with two different inner contour anode nozzles. Figure1(a) shows a cylindrical nozzle with an exit diameter of 6.0 mm and a cylindrical channel length of 20.0 mm. The schematic of a CSL nozzle is shown in Figure 1(b), the corresponding throat and nozzle exit diameters are 7.0 mm and 12.5 mm, and the axial length of the divergent part is 26.0 mm. In addition, it is worth mentioning that the total length of the CSL nozzle is 2.0 mm longer than that of the cylindrical nozzle.Figure 1
Schematic diagrams of anode nozzle inner contour: (a) cylindrical nozzle and (b) CD-conical nozzle.
(a)
(b)


## 2.2. Diagnostic Equipment

The enthalpy probe system (Tekna Plasma Systems Inc., Canada) and DPV-eVOLUTION system (Tecnar Automation Ltd., Canada) were used to measure the characteristics of plasma jet and in-flight particles, respectively. The plasma temperature was obtained by calculating the energy balance of the circulating cooling water in the enthalpy probe, while the Bernoulli equation was used to calculate the local velocity for low Mach number gas flow. The external and internal diameters of the enthalpy probe are 4.76 mm and 1.32 mm, and the corresponding area of orifice is 1.368 mm2. The shortest measurement distance to the nozzle exit was set at 60 mm to avoid thermal overload of the probe tip. In-flight particle velocity, temperature, and diameter were measured by an optical sensing device DPV-eVOLUTION system. The surface temperature of the particle was measured by a high precision two-color pyrometer based on Planck’s radiation law, which assumes the in-flight particles are gray body emitters with the same emissivity at both color bands. The velocity (V) was calculated by multiplying the real distance (S) of the slits on the photomask by the magnification factor (K) of the lens and then dividing the “time of flight” (t) between the two peaks of the particle signal; namely, V=S×K/t. It is worth mentioning that the powder particles were radially injected into the plasma jet. More detailed theoretical information on the two measurement systems can be found in [17–20].Figure2 depicts the relative position of plasma torch and enthalpy probe system, while the DPV-eVOLUTION is located at the same position as the enthalpy probe system. Plasma torch was mounted on the six degrees of freedom robot to ensure the axis of the plasma torch coinciding with the axis of the enthalpy probe tip. The axial test positions (z-direction) of the plasma jet can be adjusted by liner movement of the plasma torch along the axis, while the radial test positions (x-direction) were controlled by the displacement controller.Figure 2
The relative position of the enthalpy probe and plasma gun.


## 2.3. Preparation of Al2O3 Coatings

A bulk AISI 1045 steel sheet with a dimension ofΦ25.4×6.0 mm was employed as the substrate. Since aluminum oxide coatings have a wide range of industrial applications, a commercial fused Al2O3 powder (5–22 μm, HC Stark GmbH, Germany) was selected as feedstock in the experiments, as shown in Figure 3. Argon was chosen as the carrier gas (5 slpm, standard liter per minute), the inner diameter of the feedstock injector is 1.5 mm, and the corresponding powder feed rate is 16.25 g/min. Other detailed spraying parameters are shown in Table 1. Note that a NiAl layer is deposited on the substrate as bonding coating prior to the deposition of Al2O3. Microstructures of the Al2O3 coatings were characterized by scanning electron microscopy (Nova NanoSEM 430, FEI, Netherlands). The adhesive strength was performed through tensile adhesion test on a universal mechanical test machine (GOPOINT Testing Equipment Co., Ltd., China) based on the ASTM C633-01 standard [21]. Three specimens for each spraying distance (90, 110, and 130 mm) were tested to obtain the mean adhesive strength and relative deposition efficiency (RDE). The latter is defined as the average increment of coating weight per spraying cycle, namely, the weight of Al2O3 coating divided by the total number of spraying cycles.Table 1
Spraying parameters for online measurement and Al2O3 coatings deposition.
Case
Current (A)
Ar (slpm)
H2 (slpm)
Spraying distance (mm)
I
650
40
10
60–150
II
450, 550, 650
40
10
90
III
550
40, 50, 60, 70, 80
10
90
IV
550
60, 62, 64, 66, 68
10, 8, 6, 4, 2
90
V
650
40
10
70, 90, 110
VI
650
40
10
90, 110, 130
Note. (1) Case III, the flow rate of H2 maintains 10 slpm; (2) Case IV, the total flow rate of mixture gas is 70 slpm.Figure 3
The morphology of fused Al2O3 powders.


## 2.4. Spraying Parameters

In the actual industrial production, the adjustable spraying parameters are mainly working current, plasma gas composition, and flow rate. Therefore, it can better understand the spraying process of the two nozzles under different conditions by changing these parameters, which can provide experimental basis for the production process. The spraying parameters used in diagnostic measurement and coating fabrication are given in Table1. Case I was used to measure the axial and radial distribution of plasma temperature and velocity. Case II, Case III, and Case IV were applied to investigate the influence of working current, argon flow rate, and hydrogen content on the plasma jet characteristics. Case V allowed measuring the in-flight particle temperature and velocity. Case VI was used to deposit the Al2O3 coatings.


## 3. Results and Discussion

### 3.1. Characteristics of Plasma Jet

Table2 shows the voltage of the two nozzles under different working currents, as well as the corresponding net power and thermal efficiency. Here, only the case of 650 A is chosen to analyze the effect of the anode structure on the plasma jet characteristics, while the effect of the working current will be discussed in detail in the following parts. It can be seen from the table that, although both cylindrical and CSL nozzles operated with the same spraying parameters, the cylindrical nozzle has a slightly higher net power. Figure 4 presents the measured plasma temperature and velocity as functions of spraying distance. The plasma temperature of the CSL nozzle is about several hundreds of Kelvin higher than that of the cylindrical nozzle at the same measurement position. But the plasma velocity of the former is smaller within the whole measurement range, and the velocity difference became increasingly large towards the nozzle exit. Moreover, the plasma jet of CSL nozzle has a slower decrease in plasma temperature and velocity.Table 2
Different working currents correspond to the arc voltage, net power, and thermal efficiency (Ar/H2: 40/10 slpm).
Current (A)
Voltage (V)
Net power (kW)
Thermal efficiency (%)
Cylindrical
Laval
Cylindrical
Laval
Cylindrical
Laval
450
75.4
75.3
18.9
17.6
55.7
52.0
550
74.8
73.3
22.9
20.9
55.7
51.9
650
74.3
72.0
26.0
23.9
53.8
51.0
Note. The voltage is the average value and is obtained by reading from the console window of spraying equipment.Figure 4
Axial profiles of measured plasma jet temperature (a) and velocity (b).
(a)
(b)For the sake of convenience, we first analyze the reason for the difference in plasma velocity. Unlike the VPS, Laval nozzles typically produce subsonic plasma jets in an atmospheric environment [16, 22], which is consistent with what we observed in experiment. In this case, the plasma velocity at the throat of cylindrical nozzle is larger than that of CSL nozzle, because the velocity is inversely proportional to the throat cross-section area. Moreover, the velocity of the CSL nozzle in the divergent channel can be briefly illustrated by the relationship between the cross-section area and the velocity of the isentropic fluid flow, which is given as follows: (1)Ma2-1·duu=dAA,where Ma is the Mach number and u, du, dA, and A are the gas velocity, increment of velocity, cross-section area, and increment of the cross-section area, respectively. The Ma of subsonic flow is less than 1.0; thereby the items in the parentheses are negative. Obviously, if dA is greater than zero, du must be less than zero in order to satisfy the equality condition. This fact means that the plasma flow experienced a deceleration process in the divergent part of the CSL nozzle, resulting in a smaller plasma velocity inside of the CSL nozzle.The higher net power indicates that the plasma of cylindrical nozzle contains more energy (E) which consists of internal energy (cpT) and kinetic energy (V2/2); namely, E=cpT+V2/2. While the plasma velocity of cylindrical nozzle is much larger than that of the CSL nozzle, so it is difficult to determine which nozzle produces plasma with a higher temperature. In order to reveal the reason for the difference in temperature, a 3D numerical model was developed to compute the heat transfer and gas dynamics for two nozzles. The predicted plasma temperature distributions at the nozzle exit are shown in Figure 5, it can be seen that the temperature of cylindrical nozzle is higher. However, this is the opposite of the measurement results shown in Figure 4(a). After careful analysis, the contradictory result should be attributed to the decay rate of plasma temperature. As mentioned by Schwenk et al., the CD-bell nozzle can reduce the arc voltage fluctuations [15, 16] which enhanced the instability of the plasma jet and caused more cold air entrainment. This phenomenon may also occur in the CSL nozzle with weaker arc fluctuations due to the similar inner structure. As a result, even though the plasma jet exits from cylindrical nozzle with a higher temperature, the strong ambient air entrainment caused the plasma temperature and velocity to decrease rapidly [23].Figure 5
Predicted plasma temperature distributions at the exit of cylindrical nozzle (a) and CSL nozzle (b).
(a)
(b)The radial distributions of plasma temperature and velocity of the two nozzles at the spraying distance of 60 mm and 110 mm are shown in Figure6. It can be seen that the radial temperature and velocity gradients of the cylindrical nozzle jet at the 60 mm are larger than those of the CSL nozzle jet. These discrepancies are mainly caused by the different nozzle outlet radius that determines the size of the plasma jet. The outlet radius of the CSL nozzle is 6.25 mm, while it is only 3.0 mm for the cylindrical nozzle. This fact means that the former can produce a plasma jet with larger diameter. Therefore, the measurement positions of the cylindrical nozzle probably reached the strong turbulent region of the plasma jet, but that of the CSL nozzle did not. As the spraying distance extended to 110 mm, the interaction between the plasma jet and the cold ambient air became more significant, which reduced the radial temperature and velocity gradients. This phenomenon was more noticeable for cylindrical nozzle. In addition, at the same spraying distance, the radial temperature of the CSL nozzle jet was higher than that of the cylindrical nozzle. For example, in the case of 60 mm spraying distance, the plasma temperature at the radial position of 6.0 mm of the CSL nozzle was about 2750.0 K, which was nearly equal to the temperature at the radial distance of 4.0 mm of the cylindrical nozzle.Figure 6
Radial profiles of measured plasma jet temperature (a) and velocity (b).
(a)
(b)According to Figure6, from 60 mm to 110 mm spraying distance, the changing tendencies of the temperature difference and velocity difference of the plasma jet for two nozzles are comparable. For the sake of simplicity, only plasma temperature difference will be considered here to analyze the plasma characteristics. The symbols ∇T_Cylin and ∇T_Laval represent the plasma temperature difference of cylindrical and CSL nozzle, respectively. Both of them decreased with the increase of radial distance, and the corresponding variation of ∇T_Cylin was greater in radial direction. This fact means that the temperature reduction of the CSL nozzle jet was smoother within the entire measurement range, while a larger temperature decrease occurred in the central region of the cylindrical nozzle jet. The symbol ∇T_CL denotes the temperature difference between the cylindrical nozzle and CSL nozzle for a given spraying distance. Obviously, the ∇T_CL at the distance of 110 mm was larger than that of 60 mm. This fact proves once again that the plasma hot core was lengthened by the CSL nozzle. Based on the discussion of Figures 4–6, it is sensible to conclude that the CSL nozzle was able to obtain a homogeneous plasma jet with larger diameter and longer hot core compared to the cylindrical nozzle.The influence of the electric power on the characteristics of plasma jet was studied by using different working currents (i.e., 450, 550, and 650 A); the corresponding arc voltage, net power, and thermal efficiency were listed in Table2. As can be seen from this table, for both cylindrical and CSL nozzles, the increase in current results in increasing the net power but reducing the voltage and thermal efficiency; some previously published literatures have reported similar results [24, 25]. The plasma temperature and velocity dependencies on the current are shown in Figure 7. With the increase of current, the plasma temperature and velocity increase linearly, while there is a lesser velocity increase for CSL nozzle.Figure 7
The distribution of plasma temperature (a) and velocity (b) at the different working current conditions.
(a)
(b)In general, the arc voltage in direct current nontransferred plasma torch is approximately linearly dependent on the arc length which is determined by the balance between electromagnetic force and flow drag force [26]. The increase of current implies that a greater Lorentz force acts on the anode arc column and forces the arc to move upwards to reduce the arc voltage. Moreover, the increase in current also leads to more electric power (j2/σ, where j and σ are the current density and plasma electric conductivity) dissipating into plasma gas in the form of thermal energy, allowing more plasma forming gas to take part in the heating and ionization process. Therefore, besides the gas temperature increase, the expansion effect was also enhanced by the decreased gas density. Consequently, the plasma jet exited from the nozzle with a higher velocity and extended the plasma jet in the axial direction. In addition, the cathode jet formed in front of the cathode also played a positive role in increasing plasma velocity. Equation (2) can be used to describe the relationship between the current and the maximum velocity that the cathode jet may be reached [27]:(2)umax=μ0I2πρ1/2,where umax, μ0, I, and ρ are the maximum velocity of cathode jet, permeability of vacuum, working current, and plasma density, respectively. The numerator in (2) increased as the working current increased from 450 A to 650 A, while the denominator was reduced due to the decrease in density. As a result, the increased umax increases the velocity of the superimposed axial plasma flow.Table3 lists the relationship between the argon flow rate and the plasma arc voltage, net power, and thermal efficiency of the two nozzles. For given current, the values of these variables are increased with the argon flow rate. Take the arc voltage of cylindrical nozzle as an example: when the flow rate of argon increased from 40 to 80 slpm, the corresponding arc voltage increased from 74.8 to 82.5 V. Because the rise of the total gas flow rate increased the drag force that pushes the plasma arc to move downstream, this fact can also be qualitatively described by the following relation [28]: (3)Larc~ρ5/4UgasI,where Larc and Ugas are the arc length and the velocity of working gas, respectively. The increase of argon flow rate not only increased the density of mixed gas, but also increased the working gas velocity (Ugas). Therefore, when the working current is constant, the arc length was lengthened.Table 3
The relationship between Ar flow rate and arc voltage and net power and thermal efficiency (current: 550 A).
Working gas (slpm)
Voltage (V)
Net power (kW)
Thermal efficiency (%)
Ar
H2
Cylindrical
Laval
Cylindrical
Laval
Cylindrical
Laval
40
10
74.8
73.3
22.9
20.9
55.7
51.9
50
10
78.0
76.0
24.4
22.7
56.9
54.3
60
10
79.9
79.5
25.6
24.8
58.3
56.7
70
10
81.0
82.4
26.4
26.2
59.3
57.9
80
10
82.5
85.2
27.3
28.3
60.2
60.4
Note. H2 flow rate is 10 slpm.As shown in Figure8, the plasma velocity increases with the argon flow rate, but the corresponding temperature is reduced. Generally speaking, the increase in net electric power resulting from the increased argon flow rate implies that more energy dissipated into the plasma gas, which tends to increase the plasma temperature. Whereas if the electric power was kept constant, the rise of total gas flow rate resulted in the reduction of the gas temperature [29]. In this study, the decrease of the plasma temperature due to the argon flow rate increase cannot be compensated by the corresponding electric power increment. Similar to the temperature, there were also two opposite phenomena in plasma velocity. On the one hand, the decrease of temperature caused a higher gas density, which resulted in declining plasma velocity. On the other hand, if the temperature remains constant, the gas velocity has to increase to satisfy the continuity equation with the increase of argon flow rate. As a result, the effect of the second phenomenon was more pronounced under our experimental conditions, and the plasma velocity was increased.Figure 8
The profiles of plasma jet temperature (a) and velocity (b) with different Ar flow rate (flow rate of H2: 10 slpm).
(a)
(b)In order to investigate the influence of hydrogen content on the characteristics of plasma jet, the total gas flow rate was kept at 70 slpm. The values of plasma arc voltage, net power, and thermal efficiency for different hydrogen content were listed in Table4. The increase of hydrogen content results in an increase in arc voltage, net power, and thermal efficiency. Moreover, the hydrogen content had a greater influence on these variables of the CSL nozzle than that of the cylindrical nozzle. Figure 9 shows the profiles of plasma jet temperature and velocity as functions of the hydrogen content. It can be observed that the plasma temperature and velocity of the two nozzles increased with the hydrogen content.Table 4
The relationship between H2 content and arc voltage and net power and thermal efficiency (current: 550 A).
Working gas (slpm)
Voltage (V)
Net power (kW)
Thermal efficiency (%)
Ar
H2
Cylindrical
Laval
Cylindrical
Laval
Cylindrical
Laval
68
2
67.3
61.6
21.3
18.2
57.5
53.6
66
4
70.9
68.0
22.4
20.5
57.4
54.8
64
6
74.6
72.6
23.9
22.2
58.2
55.7
62
8
77.3
76.1
24.9
23.5
58.5
56.2
60
10
79.9
79.5
25.6
24.8
58.3
56.7
Note. Total gas flow rate is 70 slpm.Figure 9
The profiles of plasma jet temperature (a) and velocity (b) with different H2 content (total gas flow rate: 70 slpm).
(a)
(b)The hydrogen has a high specific heat and thermal conductivity, both requiring a larger electric field to sustain the plasma arc [30]. Therefore, for a given current, the arc voltage has to increase in order to provide a higher electric field strength. In other words, the increase of hydrogen content required more electric power to maintain the stability of the plasma arc, which led to the increase of the plasma temperature. As discussed in the effect of working current, the increased temperature resulting from the increased electric power leads to decreased gas density, which enhances the expansion effect of the plasma gas. In addition, the increase in hydrogen content reduces the total density of the mixed working gas, because the density of hydrogen is much lower than that of argon. Thus, the ratio in the parentheses of (2) increased with the decrease of gas density and finally increased the maximum velocity of cathode jet.


### 3.2. In-Flight Particle Behavior

Figure10(a) presents the measured particle temperature decrease with the increase of the spraying distance. The temperature profile of the CSL nozzle has a greater downward trend and with a larger temperature until 90 mm distance. All measured temperatures are observed in the range of melting (2,323 K) and boiling (3,253 K) point of the Al2O3 powder; it implies that the particle surface was in the molten state. In general, the heat transfer between the plasma jet and in-flight particle can be described by the following equation:(4)qconv=β1β2Nusk-T∞-Tw2rp,where qconv is the specific heat flux at the particle surface and β1 and β2 are the two factors used to correct the Knudsen and evaporation effects. Nus, k-, T∞, Tw, and rp are the Nusselt number, average thermal conductivity within the Knudsen layer, plasma temperature, particle surface temperature, and particle radius, respectively. Apparently, the heat transfer occurred as long as there was a temperature difference. By comparing Figures 4(a) and 10(a), the temperature of plasma jet was higher than that of particle at the given spraying distance. According to (4), the temperature of particle should be further increased theoretically. However, the fact is that the particle temperature declined slightly. Actually, there is no contradiction here, because the particle temperature depends primarily on the ambient gas temperature of the flight trajectory. Recalling Section 2.2, the particles were fed along the radial direction, which means the centerline of in-flight particle jet was deviated from that of plasma jet. That is, the in-flight particle at the measured position has passed through the high temperature region; namely, T∞-Tw>0. In addition, although the CSL nozzle has a lower plasma temperature at the nozzle exit, the extended plasma jet core region and the smaller plasma velocity prolong the particles residence time, which allows the injected particles to be better heated. However, the smaller velocity also extended the residence time of the particle in the cold environment, resulting in a larger decrease rate of in-flight particle along the spraying distance. Finally, the particle temperature of CSL nozzle was lower than that of cylindrical nozzle beyond 90 mm.Figure 10
The profiles of Al2O3 particle surface temperature (a) and velocity (b).
(a)
(b)The dependence of the measured particle velocity on the spraying distance of the two nozzles is shown in Figure10(b). They show a similar behavior that the particle velocity increases first and then gradually slows down. Moreover, the particle velocity of CSL nozzle is much lower than that of cylindrical nozzle over the whole measured range. Those phenomena can be revealed by the particle motion which is mainly controlled by the fluid drag and thermophoresis forces in the plasma jet. According to Newton’s second law, the force balance can be written as [31](5)ⅆu→pdt=18ρCD24rpρp·u→-u→P·u→-u→P+F→t.Here, u→, u→p, and F→t are the vectors of plasma velocity, particle velocity, and thermophoresis force, respectively. The symbols ρp, CD, and t are the particle density, drag coefficient, and time. The increase in particle velocity means that the plasma jet has a larger velocity (u→-u→P>0), but unfortunately the plasma properties at 50 mm distance were not measured, because the high heat loads increase the risk of damaging the enthalpy probe. Combining the features of the plasma velocity in Figure 4(b), it can be deduced that the in-flight particles have a maximum velocity in the range of 50 to 60 mm, and then they show a linear decrease over the whole range beyond 60 mm spraying distance. In addition, a larger plasma velocity of cylindrical nozzle is responsible for its larger particle velocity, because the larger relative velocity (u→-u→P) corresponds to a stronger acceleration process.


### 3.3. Al2O3 Coating Properties

The surface morphologies of the Al2O3 coatings fabricated using the cylindrical and CSL nozzles are demonstrated in Figure 11, and the spraying distance is 110 mm. It can be observed that the coating prepared by the former has a rough surface consisting of semimolten particles, irregular splats, splashing fingers, and some open voids. However, the coating produced via the latter presents smoother surface with less semimolten particles and few splashing fingers. This fact indirectly reflects that the particles of the CSL nozzle were molten more sufficiently, which was mainly caused by the different characteristics of the plasma jet. As discussed earlier, the measured particle temperature was risen due to the extended plasma jet and the longer particle residence time; in fact, the particle melt fraction was also increased. In addition, the particle temperature of CSL nozzle was still above the melting point even though it has experienced a drastic decrease. All in all, the difference in particle temperature and melting fraction of the two nozzles is attributed to the residence time and small thermal conductivity of the Al2O3 powder. The later usually results in a considerable temperature gradient inside the particles, which has been confirmed by previous numerical simulation results [32].Figure 11
Surface micrographs of Al2O3 coatings prepared by cylindrical nozzle (a) and CSL nozzle (b) (current: 650 A, Ar/H2: 40/10 slpm, spraying distance: 110 mm).
(a)
(b)Figure12 depicts the cross-sectional micrographs of the Al2O3 coatings. A dense coating was obtained by the cylindrical nozzle, whereas the coating produced by the CSL nozzle had a large number of pores, and the contact between the coating splats was not very good. Figure 13 shows the adhesive strength and the RDE of the coatings produced by the two nozzles at different spraying distances. Two phenomena can be observed in Figure 13(a): one is that the adhesive strength decreased with the increase of the spraying distance, and the other one is that the adhesive strength of the coating produced via the cylindrical nozzle was almost twice higher than via CSL nozzle. Figure 13(b) presents the average incremental weight of the Al2O3 coatings per spraying cycle. It is clear that the CSL nozzle has a higher RDE in the preparation of the coating.Figure 12
Cross-sectional SEM micrographs of Al2O3 coatings prepared by cylindrical nozzle (a) and CSL nozzle (b) (current: 650 A, Ar/H2: 40/10 slpm, spraying distance: 110 mm).
(a)
(b)Figure 13
Adhesive strength (a) and average increment of coating weight per cycle (b) for different spraying distance.
(a)
(b)By overall considering the particle velocity, melting state, and coating properties, it can be found that the effect of the particle velocity on the coating adhesive strength and porosity was greater than that on the melting state under the present experimental conditions. Even though the coating prepared by the cylindrical nozzle contained more semimolten particles, the higher velocity means that the in-flight particle impacted on the substrate or as-sprayed coating with a higher kinetic energy, which enhanced the compaction effect of the coating. This improved the contact between the coating lamellas and also facilitated the filling of the pores with molten particles. As discussed in Section3.1, the plasma jet of the CSL nozzle had a larger diameter and lower velocity. In this case, more particles can stay in the high temperature core region and undergo better effective heating, which resulted in more molten particles deposited on the substrate or as-sprayed coating, thereby increasing the RDE.The results of the coating properties in this study are somewhat different from those reported in previous investigations, which presented that the coating properties of cylindrical and bell-shaped Laval nozzles were in the same range except the deposition efficiency. This fact suggests that the coating properties are strongly related to the structure of anode nozzles and the other factors such as the spraying parameters and substrate properties.


## 3.1. Characteristics of Plasma Jet

Table2 shows the voltage of the two nozzles under different working currents, as well as the corresponding net power and thermal efficiency. Here, only the case of 650 A is chosen to analyze the effect of the anode structure on the plasma jet characteristics, while the effect of the working current will be discussed in detail in the following parts. It can be seen from the table that, although both cylindrical and CSL nozzles operated with the same spraying parameters, the cylindrical nozzle has a slightly higher net power. Figure 4 presents the measured plasma temperature and velocity as functions of spraying distance. The plasma temperature of the CSL nozzle is about several hundreds of Kelvin higher than that of the cylindrical nozzle at the same measurement position. But the plasma velocity of the former is smaller within the whole measurement range, and the velocity difference became increasingly large towards the nozzle exit. Moreover, the plasma jet of CSL nozzle has a slower decrease in plasma temperature and velocity.Table 2
Different working currents correspond to the arc voltage, net power, and thermal efficiency (Ar/H2: 40/10 slpm).
Current (A)
Voltage (V)
Net power (kW)
Thermal efficiency (%)
Cylindrical
Laval
Cylindrical
Laval
Cylindrical
Laval
450
75.4
75.3
18.9
17.6
55.7
52.0
550
74.8
73.3
22.9
20.9
55.7
51.9
650
74.3
72.0
26.0
23.9
53.8
51.0
Note. The voltage is the average value and is obtained by reading from the console window of spraying equipment.Figure 4
Axial profiles of measured plasma jet temperature (a) and velocity (b).
(a)
(b)For the sake of convenience, we first analyze the reason for the difference in plasma velocity. Unlike the VPS, Laval nozzles typically produce subsonic plasma jets in an atmospheric environment [16, 22], which is consistent with what we observed in experiment. In this case, the plasma velocity at the throat of cylindrical nozzle is larger than that of CSL nozzle, because the velocity is inversely proportional to the throat cross-section area. Moreover, the velocity of the CSL nozzle in the divergent channel can be briefly illustrated by the relationship between the cross-section area and the velocity of the isentropic fluid flow, which is given as follows: (1)Ma2-1·duu=dAA,where Ma is the Mach number and u, du, dA, and A are the gas velocity, increment of velocity, cross-section area, and increment of the cross-section area, respectively. The Ma of subsonic flow is less than 1.0; thereby the items in the parentheses are negative. Obviously, if dA is greater than zero, du must be less than zero in order to satisfy the equality condition. This fact means that the plasma flow experienced a deceleration process in the divergent part of the CSL nozzle, resulting in a smaller plasma velocity inside of the CSL nozzle.The higher net power indicates that the plasma of cylindrical nozzle contains more energy (E) which consists of internal energy (cpT) and kinetic energy (V2/2); namely, E=cpT+V2/2. While the plasma velocity of cylindrical nozzle is much larger than that of the CSL nozzle, so it is difficult to determine which nozzle produces plasma with a higher temperature. In order to reveal the reason for the difference in temperature, a 3D numerical model was developed to compute the heat transfer and gas dynamics for two nozzles. The predicted plasma temperature distributions at the nozzle exit are shown in Figure 5, it can be seen that the temperature of cylindrical nozzle is higher. However, this is the opposite of the measurement results shown in Figure 4(a). After careful analysis, the contradictory result should be attributed to the decay rate of plasma temperature. As mentioned by Schwenk et al., the CD-bell nozzle can reduce the arc voltage fluctuations [15, 16] which enhanced the instability of the plasma jet and caused more cold air entrainment. This phenomenon may also occur in the CSL nozzle with weaker arc fluctuations due to the similar inner structure. As a result, even though the plasma jet exits from cylindrical nozzle with a higher temperature, the strong ambient air entrainment caused the plasma temperature and velocity to decrease rapidly [23].Figure 5
Predicted plasma temperature distributions at the exit of cylindrical nozzle (a) and CSL nozzle (b).
(a)
(b)The radial distributions of plasma temperature and velocity of the two nozzles at the spraying distance of 60 mm and 110 mm are shown in Figure6. It can be seen that the radial temperature and velocity gradients of the cylindrical nozzle jet at the 60 mm are larger than those of the CSL nozzle jet. These discrepancies are mainly caused by the different nozzle outlet radius that determines the size of the plasma jet. The outlet radius of the CSL nozzle is 6.25 mm, while it is only 3.0 mm for the cylindrical nozzle. This fact means that the former can produce a plasma jet with larger diameter. Therefore, the measurement positions of the cylindrical nozzle probably reached the strong turbulent region of the plasma jet, but that of the CSL nozzle did not. As the spraying distance extended to 110 mm, the interaction between the plasma jet and the cold ambient air became more significant, which reduced the radial temperature and velocity gradients. This phenomenon was more noticeable for cylindrical nozzle. In addition, at the same spraying distance, the radial temperature of the CSL nozzle jet was higher than that of the cylindrical nozzle. For example, in the case of 60 mm spraying distance, the plasma temperature at the radial position of 6.0 mm of the CSL nozzle was about 2750.0 K, which was nearly equal to the temperature at the radial distance of 4.0 mm of the cylindrical nozzle.Figure 6
Radial profiles of measured plasma jet temperature (a) and velocity (b).
(a)
(b)According to Figure6, from 60 mm to 110 mm spraying distance, the changing tendencies of the temperature difference and velocity difference of the plasma jet for two nozzles are comparable. For the sake of simplicity, only plasma temperature difference will be considered here to analyze the plasma characteristics. The symbols ∇T_Cylin and ∇T_Laval represent the plasma temperature difference of cylindrical and CSL nozzle, respectively. Both of them decreased with the increase of radial distance, and the corresponding variation of ∇T_Cylin was greater in radial direction. This fact means that the temperature reduction of the CSL nozzle jet was smoother within the entire measurement range, while a larger temperature decrease occurred in the central region of the cylindrical nozzle jet. The symbol ∇T_CL denotes the temperature difference between the cylindrical nozzle and CSL nozzle for a given spraying distance. Obviously, the ∇T_CL at the distance of 110 mm was larger than that of 60 mm. This fact proves once again that the plasma hot core was lengthened by the CSL nozzle. Based on the discussion of Figures 4–6, it is sensible to conclude that the CSL nozzle was able to obtain a homogeneous plasma jet with larger diameter and longer hot core compared to the cylindrical nozzle.The influence of the electric power on the characteristics of plasma jet was studied by using different working currents (i.e., 450, 550, and 650 A); the corresponding arc voltage, net power, and thermal efficiency were listed in Table2. As can be seen from this table, for both cylindrical and CSL nozzles, the increase in current results in increasing the net power but reducing the voltage and thermal efficiency; some previously published literatures have reported similar results [24, 25]. The plasma temperature and velocity dependencies on the current are shown in Figure 7. With the increase of current, the plasma temperature and velocity increase linearly, while there is a lesser velocity increase for CSL nozzle.Figure 7
The distribution of plasma temperature (a) and velocity (b) at the different working current conditions.
(a)
(b)In general, the arc voltage in direct current nontransferred plasma torch is approximately linearly dependent on the arc length which is determined by the balance between electromagnetic force and flow drag force [26]. The increase of current implies that a greater Lorentz force acts on the anode arc column and forces the arc to move upwards to reduce the arc voltage. Moreover, the increase in current also leads to more electric power (j2/σ, where j and σ are the current density and plasma electric conductivity) dissipating into plasma gas in the form of thermal energy, allowing more plasma forming gas to take part in the heating and ionization process. Therefore, besides the gas temperature increase, the expansion effect was also enhanced by the decreased gas density. Consequently, the plasma jet exited from the nozzle with a higher velocity and extended the plasma jet in the axial direction. In addition, the cathode jet formed in front of the cathode also played a positive role in increasing plasma velocity. Equation (2) can be used to describe the relationship between the current and the maximum velocity that the cathode jet may be reached [27]:(2)umax=μ0I2πρ1/2,where umax, μ0, I, and ρ are the maximum velocity of cathode jet, permeability of vacuum, working current, and plasma density, respectively. The numerator in (2) increased as the working current increased from 450 A to 650 A, while the denominator was reduced due to the decrease in density. As a result, the increased umax increases the velocity of the superimposed axial plasma flow.Table3 lists the relationship between the argon flow rate and the plasma arc voltage, net power, and thermal efficiency of the two nozzles. For given current, the values of these variables are increased with the argon flow rate. Take the arc voltage of cylindrical nozzle as an example: when the flow rate of argon increased from 40 to 80 slpm, the corresponding arc voltage increased from 74.8 to 82.5 V. Because the rise of the total gas flow rate increased the drag force that pushes the plasma arc to move downstream, this fact can also be qualitatively described by the following relation [28]: (3)Larc~ρ5/4UgasI,where Larc and Ugas are the arc length and the velocity of working gas, respectively. The increase of argon flow rate not only increased the density of mixed gas, but also increased the working gas velocity (Ugas). Therefore, when the working current is constant, the arc length was lengthened.Table 3
The relationship between Ar flow rate and arc voltage and net power and thermal efficiency (current: 550 A).
Working gas (slpm)
Voltage (V)
Net power (kW)
Thermal efficiency (%)
Ar
H2
Cylindrical
Laval
Cylindrical
Laval
Cylindrical
Laval
40
10
74.8
73.3
22.9
20.9
55.7
51.9
50
10
78.0
76.0
24.4
22.7
56.9
54.3
60
10
79.9
79.5
25.6
24.8
58.3
56.7
70
10
81.0
82.4
26.4
26.2
59.3
57.9
80
10
82.5
85.2
27.3
28.3
60.2
60.4
Note. H2 flow rate is 10 slpm.As shown in Figure8, the plasma velocity increases with the argon flow rate, but the corresponding temperature is reduced. Generally speaking, the increase in net electric power resulting from the increased argon flow rate implies that more energy dissipated into the plasma gas, which tends to increase the plasma temperature. Whereas if the electric power was kept constant, the rise of total gas flow rate resulted in the reduction of the gas temperature [29]. In this study, the decrease of the plasma temperature due to the argon flow rate increase cannot be compensated by the corresponding electric power increment. Similar to the temperature, there were also two opposite phenomena in plasma velocity. On the one hand, the decrease of temperature caused a higher gas density, which resulted in declining plasma velocity. On the other hand, if the temperature remains constant, the gas velocity has to increase to satisfy the continuity equation with the increase of argon flow rate. As a result, the effect of the second phenomenon was more pronounced under our experimental conditions, and the plasma velocity was increased.Figure 8
The profiles of plasma jet temperature (a) and velocity (b) with different Ar flow rate (flow rate of H2: 10 slpm).
(a)
(b)In order to investigate the influence of hydrogen content on the characteristics of plasma jet, the total gas flow rate was kept at 70 slpm. The values of plasma arc voltage, net power, and thermal efficiency for different hydrogen content were listed in Table4. The increase of hydrogen content results in an increase in arc voltage, net power, and thermal efficiency. Moreover, the hydrogen content had a greater influence on these variables of the CSL nozzle than that of the cylindrical nozzle. Figure 9 shows the profiles of plasma jet temperature and velocity as functions of the hydrogen content. It can be observed that the plasma temperature and velocity of the two nozzles increased with the hydrogen content.Table 4
The relationship between H2 content and arc voltage and net power and thermal efficiency (current: 550 A).
Working gas (slpm)
Voltage (V)
Net power (kW)
Thermal efficiency (%)
Ar
H2
Cylindrical
Laval
Cylindrical
Laval
Cylindrical
Laval
68
2
67.3
61.6
21.3
18.2
57.5
53.6
66
4
70.9
68.0
22.4
20.5
57.4
54.8
64
6
74.6
72.6
23.9
22.2
58.2
55.7
62
8
77.3
76.1
24.9
23.5
58.5
56.2
60
10
79.9
79.5
25.6
24.8
58.3
56.7
Note. Total gas flow rate is 70 slpm.Figure 9
The profiles of plasma jet temperature (a) and velocity (b) with different H2 content (total gas flow rate: 70 slpm).
(a)
(b)The hydrogen has a high specific heat and thermal conductivity, both requiring a larger electric field to sustain the plasma arc [30]. Therefore, for a given current, the arc voltage has to increase in order to provide a higher electric field strength. In other words, the increase of hydrogen content required more electric power to maintain the stability of the plasma arc, which led to the increase of the plasma temperature. As discussed in the effect of working current, the increased temperature resulting from the increased electric power leads to decreased gas density, which enhances the expansion effect of the plasma gas. In addition, the increase in hydrogen content reduces the total density of the mixed working gas, because the density of hydrogen is much lower than that of argon. Thus, the ratio in the parentheses of (2) increased with the decrease of gas density and finally increased the maximum velocity of cathode jet.


## 3.2. In-Flight Particle Behavior

Figure10(a) presents the measured particle temperature decrease with the increase of the spraying distance. The temperature profile of the CSL nozzle has a greater downward trend and with a larger temperature until 90 mm distance. All measured temperatures are observed in the range of melting (2,323 K) and boiling (3,253 K) point of the Al2O3 powder; it implies that the particle surface was in the molten state. In general, the heat transfer between the plasma jet and in-flight particle can be described by the following equation:(4)qconv=β1β2Nusk-T∞-Tw2rp,where qconv is the specific heat flux at the particle surface and β1 and β2 are the two factors used to correct the Knudsen and evaporation effects. Nus, k-, T∞, Tw, and rp are the Nusselt number, average thermal conductivity within the Knudsen layer, plasma temperature, particle surface temperature, and particle radius, respectively. Apparently, the heat transfer occurred as long as there was a temperature difference. By comparing Figures 4(a) and 10(a), the temperature of plasma jet was higher than that of particle at the given spraying distance. According to (4), the temperature of particle should be further increased theoretically. However, the fact is that the particle temperature declined slightly. Actually, there is no contradiction here, because the particle temperature depends primarily on the ambient gas temperature of the flight trajectory. Recalling Section 2.2, the particles were fed along the radial direction, which means the centerline of in-flight particle jet was deviated from that of plasma jet. That is, the in-flight particle at the measured position has passed through the high temperature region; namely, T∞-Tw>0. In addition, although the CSL nozzle has a lower plasma temperature at the nozzle exit, the extended plasma jet core region and the smaller plasma velocity prolong the particles residence time, which allows the injected particles to be better heated. However, the smaller velocity also extended the residence time of the particle in the cold environment, resulting in a larger decrease rate of in-flight particle along the spraying distance. Finally, the particle temperature of CSL nozzle was lower than that of cylindrical nozzle beyond 90 mm.Figure 10
The profiles of Al2O3 particle surface temperature (a) and velocity (b).
(a)
(b)The dependence of the measured particle velocity on the spraying distance of the two nozzles is shown in Figure10(b). They show a similar behavior that the particle velocity increases first and then gradually slows down. Moreover, the particle velocity of CSL nozzle is much lower than that of cylindrical nozzle over the whole measured range. Those phenomena can be revealed by the particle motion which is mainly controlled by the fluid drag and thermophoresis forces in the plasma jet. According to Newton’s second law, the force balance can be written as [31](5)ⅆu→pdt=18ρCD24rpρp·u→-u→P·u→-u→P+F→t.Here, u→, u→p, and F→t are the vectors of plasma velocity, particle velocity, and thermophoresis force, respectively. The symbols ρp, CD, and t are the particle density, drag coefficient, and time. The increase in particle velocity means that the plasma jet has a larger velocity (u→-u→P>0), but unfortunately the plasma properties at 50 mm distance were not measured, because the high heat loads increase the risk of damaging the enthalpy probe. Combining the features of the plasma velocity in Figure 4(b), it can be deduced that the in-flight particles have a maximum velocity in the range of 50 to 60 mm, and then they show a linear decrease over the whole range beyond 60 mm spraying distance. In addition, a larger plasma velocity of cylindrical nozzle is responsible for its larger particle velocity, because the larger relative velocity (u→-u→P) corresponds to a stronger acceleration process.


## 3.3. Al2O3 Coating Properties

The surface morphologies of the Al2O3 coatings fabricated using the cylindrical and CSL nozzles are demonstrated in Figure 11, and the spraying distance is 110 mm. It can be observed that the coating prepared by the former has a rough surface consisting of semimolten particles, irregular splats, splashing fingers, and some open voids. However, the coating produced via the latter presents smoother surface with less semimolten particles and few splashing fingers. This fact indirectly reflects that the particles of the CSL nozzle were molten more sufficiently, which was mainly caused by the different characteristics of the plasma jet. As discussed earlier, the measured particle temperature was risen due to the extended plasma jet and the longer particle residence time; in fact, the particle melt fraction was also increased. In addition, the particle temperature of CSL nozzle was still above the melting point even though it has experienced a drastic decrease. All in all, the difference in particle temperature and melting fraction of the two nozzles is attributed to the residence time and small thermal conductivity of the Al2O3 powder. The later usually results in a considerable temperature gradient inside the particles, which has been confirmed by previous numerical simulation results [32].Figure 11
Surface micrographs of Al2O3 coatings prepared by cylindrical nozzle (a) and CSL nozzle (b) (current: 650 A, Ar/H2: 40/10 slpm, spraying distance: 110 mm).
(a)
(b)Figure12 depicts the cross-sectional micrographs of the Al2O3 coatings. A dense coating was obtained by the cylindrical nozzle, whereas the coating produced by the CSL nozzle had a large number of pores, and the contact between the coating splats was not very good. Figure 13 shows the adhesive strength and the RDE of the coatings produced by the two nozzles at different spraying distances. Two phenomena can be observed in Figure 13(a): one is that the adhesive strength decreased with the increase of the spraying distance, and the other one is that the adhesive strength of the coating produced via the cylindrical nozzle was almost twice higher than via CSL nozzle. Figure 13(b) presents the average incremental weight of the Al2O3 coatings per spraying cycle. It is clear that the CSL nozzle has a higher RDE in the preparation of the coating.Figure 12
Cross-sectional SEM micrographs of Al2O3 coatings prepared by cylindrical nozzle (a) and CSL nozzle (b) (current: 650 A, Ar/H2: 40/10 slpm, spraying distance: 110 mm).
(a)
(b)Figure 13
Adhesive strength (a) and average increment of coating weight per cycle (b) for different spraying distance.
(a)
(b)By overall considering the particle velocity, melting state, and coating properties, it can be found that the effect of the particle velocity on the coating adhesive strength and porosity was greater than that on the melting state under the present experimental conditions. Even though the coating prepared by the cylindrical nozzle contained more semimolten particles, the higher velocity means that the in-flight particle impacted on the substrate or as-sprayed coating with a higher kinetic energy, which enhanced the compaction effect of the coating. This improved the contact between the coating lamellas and also facilitated the filling of the pores with molten particles. As discussed in Section3.1, the plasma jet of the CSL nozzle had a larger diameter and lower velocity. In this case, more particles can stay in the high temperature core region and undergo better effective heating, which resulted in more molten particles deposited on the substrate or as-sprayed coating, thereby increasing the RDE.The results of the coating properties in this study are somewhat different from those reported in previous investigations, which presented that the coating properties of cylindrical and bell-shaped Laval nozzles were in the same range except the deposition efficiency. This fact suggests that the coating properties are strongly related to the structure of anode nozzles and the other factors such as the spraying parameters and substrate properties.


## 4. Conclusions

Thermal plasma spraying is normally regarded as a mature technology, but the detailed effect of the anode nozzle contour on the spraying process is still not fully understood. In this work, both for cylindrical and CSL nozzles, the plasma jet characteristics, in-flight particle behaviors, and coating properties have been systematically studied by experimental method, and the intrinsic relationship between them has been also revealed. The essential results obtained are as follows:(1)
For given current and plasma forming gas, the cylindrical nozzle exhibits higher arc voltage, net power, and thermal efficiency and has a higher temperature and velocity distributions at the nozzle exit. However, the plasma jet of the CSL nozzle is characterized by a higher temperature and smaller velocity with a slower downward trend in the whole measured range, which is attributed to the less entrainment of ambient cold air.(2)
Both for cylindrical and Laval nozzles, the values of arc voltage, net power, thermal efficiency, plasma temperature, and velocity are increased with the working current, Ar flow rate, and H2 content, whereas the increase in current and argon flow rate leads to a decrease of the thermal efficiency and plasma temperature, respectively.(3)
The smaller particle velocity of CSL nozzle prolongs the residence time in the high temperature region, which leads to a higher particle temperature and a larger melting fraction, but it also increases the particle residence time in the cold environment and results in a larger cooling rate. Moreover, there should be a maximum particle velocity in the range of 50–60 mm distance.(4)
In contrast to the cylindrical nozzle, the smaller particle velocity of the CSL nozzle leads to lower coating density and adhesive strength. Nevertheless, the RDE is higher because the homogeneous plasma jet has a lager diameter, which allows more particles to experience better heating.



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*Source: 2084363-2017-10-31.xml*