3.1 Effect of plating solution composition on deposition rate, hardness, and P and Cr elemental contents
(1) Effect of plating solution composition on deposition rate
The orthogonal experimental results indicated that the deposition rate of chemical plating varied with changes in plating solution composition and process parameters. Table 4 lists the deposition rate records of 16 sets of orthogonal experiments. Due to the introduction of the difficult-to-reduce chromium salt in the Ni-Cr-P chemical plating process, theoretically, it should lead to a significant decrease in deposition rate. The deposition rate was determined from multiple measurements of coating thickness at a fixed magnification using a metallographic microscope, and the average value was calculated for each set[18]. Table 5 presents the range analysis table for the deposition rate, which utilizes the range values to analyze the impact of each factor on the experimental results. Ki represents the four-level variables investigated in the experiment, aiming to study their impact on the experimental results and determine the primary influencing factors. R represents the range of Ki (KiMAX–KiMIN)[19]. As R increased, the impact of level variations on the reference indicator became more significant, and as R decreased, the impact of level variations became smaller. Through the orthogonal experimental design, it was possible to analyze more effectively the impact of various factors on the experimental results, reduce the number of experiments, and identify the optimal combination of factors.
Table 4
Deposition rates in the Ni-Cr-P chemical plating orthogonal experiment.
Group
|
1
|
2
|
3
|
4
|
5
|
6
|
7
|
8
|
Deposition rate (µm/h)
|
1.386
|
3.292
|
2.773
|
6.413
|
0.693
|
1.560
|
1.144
|
0.936
|
Table 4
Group
|
9
|
10
|
11
|
12
|
13
|
14
|
15
|
16
|
Deposition rate (µm/h)
|
3.292
|
2.599
|
1.040
|
3.015
|
7.843
|
1.040
|
1.213
|
2.416
|
Table 5
Range analysis of deposition rates in the Ni-Cr-P chemical plating orthogonal experiment.
Group
|
A
|
B
|
C
|
D
|
E
|
Factor
Evaluation
indicator
|
Chromium chloride
(g/L)
|
Citric acid
(g/L)
|
Lactic acid
(ml/L)
|
pH
|
Temperature
(℃)
|
K1
|
3.466
|
3.304
|
1.612
|
1.646
|
1.534
|
K2
|
1.083
|
2.123
|
2.053
|
3.278
|
2.547
|
K3
|
2.487
|
1.543
|
2.010
|
2.132
|
3.798
|
K4
|
3.139
|
3.206
|
4.500
|
3.120
|
2.297
|
Range R
|
2.383
|
1.761
|
2.888
|
1.632
|
2.264
|
Main factor ranking
|
CAEBD
|
Best combination
|
A1B1C4D2E3
|
From the range analysis of deposition rates in the Ni-Cr-P chemical plating orthogonal experiment, the ranking of the five factors on the deposition rate was found to be in the order: lactic acid (C) > chromium chloride (A) > temperature (E) > citric acid (B) > pH (D). Lactic acid had the most significant impact on the deposition rate, while pH had the least impact. The orthogonal experimental factor and deposition rate contour plot based on the Ki values of the five factors is shown in Fig. 5.
(2) Effect of plating solution composition on surface hardness
The hardness of the coating varied with changes in plating solution composition and process parameters[20]. Using a microhardness tester, multiple points were measured on the surface of the Ni-Cr-P-coated samples, and the average value was calculated. Table 6 lists the surface hardness records for 16 sets of orthogonal experiments, and Table 7 presents the range analysis table for surface hardness as an evaluation indicator.
Table 6
Surface hardness results for the Ni-Cr-P chemical plating orthogonal experiment.
Group
|
1
|
2
|
3
|
4
|
5
|
6
|
7
|
8
|
Surface hardness (HV0.2)
|
585.22
|
577.63
|
558.01
|
601.4
|
530.53
|
564.88
|
581.52
|
545.73
|
Table 6
Group
|
9
|
10
|
11
|
12
|
13
|
14
|
15
|
16
|
Surface hardness (HV0.2)
|
627.28
|
583.18
|
574.37
|
583.26
|
604.47
|
604.47
|
569.57
|
555.36
|
Table 7
Range analysis of surface hardness for the Ni-Cr-P chemical plating orthogonal experiment.
Group
|
A
|
B
|
C
|
D
|
E
|
Factor
Evaluation
indicator
|
Chromium chloride
(g/L)
|
Citric acid
(g/L)
|
Lactic acid
(ml/L)
|
pH
|
Temperature
(℃)
|
K1
|
580.57
|
586.88
|
569.96
|
581.07
|
570.93
|
K2
|
555.67
|
574.99
|
565.25
|
575.55
|
585.45
|
K3
|
592.02
|
570.87
|
576.33
|
556.77
|
577.66
|
K4
|
575.92
|
571.44
|
592.64
|
590.78
|
570.15
|
Range R
|
36.36
|
16.01
|
27.40
|
34.01
|
15.30
|
Main factor ranking
|
A > D > C > B > E
|
Best combination
|
A3B1C4D4E2
|
From the range analysis of surface hardness in the Ni-Cr-P chemical plating orthogonal experiment, the ranking of the effect of the five factors on surface hardness was found to be: chromium chloride (A) > pH (D) > lactic acid (C) > citric acid (B) > temperature (E). Chromium chloride had the most significant impact on surface hardness. The contour plot of orthogonal experimental factors and surface hardness, based on the Ki values of the five factors, is shown in Fig. 6.
(3) Effect of plating solution composition on P and Cr elemental contents
The P and Cr elemental contents of the coating were measured using the EDX-7200 EDX spectrometer. Table 8 lists the test results record for P and Cr contents in the 16 sets of orthogonal experiments.
Table 8
P and Cr elemental contents in the Ni-Cr-P chemical plating orthogonal experiment.
Group
|
1
|
2
|
3
|
4
|
5
|
6
|
7
|
8
|
P content (wt%)
|
7.108
|
8.495
|
9.694
|
9.772
|
8.243
|
9.331
|
8.16
|
6.886
|
Cr content (wt%)
|
0.193
|
0.102
|
0.13
|
0.182
|
0.187
|
0.196
|
0.181
|
0.231
|
Table 8
Group
|
9
|
10
|
11
|
12
|
13
|
14
|
15
|
16
|
P content (wt%)
|
9.16
|
7.687
|
8.652
|
9.562
|
9.905
|
7.835
|
8.69
|
9.037
|
Cr content (wt%)
|
0.127
|
0.16
|
0.218
|
0.137
|
0.034
|
0.221
|
0.181
|
0.143
|
In all 16 sets of orthogonal experiments, the P content in the coating of all samples ranged from 7 to 9 wt%, indicating that the Ni-Cr-P coating deposited from this plating solution composition had a medium-to-high phosphorus coating with an amorphous structure. The elevation of P content contributed to the improvement in coating hardness[21]. Range analysis of P content revealed the ranking of the five factors on the P content in the coating to have been in the order: temperature (E) > pH (D) > chromium chloride (A) > citric acid (B) > lactic acid (C).
In all 16 sets of orthogonal experiments, the Cr content in the coating of all samples ranged from 0.1 to 0.2 wt%. Within this range, the elevation of Cr content contributed to the improvement in corrosion resistance of the coating[22]. The difficulty in reducing Cr content resulted in a relatively low Cr content in the coating. The difficulty in reducing Cr content was due to ion exchange between Cr3+ and Ni during the deposition process[23]. Range analysis of the Cr content revealed the ranking of the five factors on the Cr content in the coating to have been in the order: temperature (E) > chromium chloride (A) > lactic acid (C) > citric acid (B) > pH (D). Of the five factors, temperature had the most significant impact on the P and Cr elemental contents of the coating. This was because temperature, as the direct energy source for the Ni-Cr-P chemical plating reaction, directly affected the breaking and recombination of chemical bonds in the reactants and products of the reduction chemical equations for P and Cr. Increase in temperature significantly promoted the forward progress of the reaction.
3.2 Analysis of coating surface appearance, porosity, and adhesion
(1) Coating surface appearance
Careful observation of the macroscopic appearance of the 65Mn alloy steel following the Ni-Cr-P chemical plating quickly provided a preliminary judgment as to the quality of the Ni-Cr-P coating so obtained. The presence of phenomena such as missed plating, yellow spots, peeling, etc., on the sample surface indicated poor coating quality[24]. Following observation, except for the presence of yellow spots on the surface of the coating in Group 7, the appearance of the coatings in the other 15 experimental groups was good. In Fig. 7, sample A had a bright and smooth surface, with no missed plating or peeling, presenting a good macroscopic appearance. In contrast, sample B showed the presence of yellow spots, indicating poor coating quality.
(2) Coating porosity
The coating porosity was determined using the filter paper adhesion method, in accordance with the QB/T 3823 − 1999 standard[25]. A test solution was prepared containing 20 g/L K3Fe(CN)6 and 20 g/L NaCl. Filter paper was immersed in the solution so as to thoroughly absorb it and was then applied to the coating surface for 1 min. The number of blue spots on the filter paper was then recorded.
The results of the porosity measurements for the 16 sets of samples were categorized into three levels: F (few) with 1–2 spots, N (normal) with 3–5 spots, and M (many) with > 5 spots. The complete set of test results are listed in Table 9.
Table 9
Coating porosity test results.
Group
|
1
|
2
|
3
|
4
|
5
|
6
|
7
|
8
|
Result
|
M
|
F
|
F
|
N
|
F
|
F
|
F
|
N
|
Table 9
Group
|
9
|
10
|
11
|
12
|
13
|
14
|
15
|
16
|
Result
|
F
|
M
|
M
|
F
|
N
|
N
|
F
|
F
|
From Table 9, it can be seen that the coated samples from Groups 1, 10, and 11 all had > 5 porosity spots. The coated samples from Groups 4, 8, 13, and 14 had porosity spots ranging from 3 to 5. In contrast, the coated samples from Groups 2, 3, 5, 6, 7, 9, 12, 15, and 16 had only 1 to 2 porosity spots.
(3) Coating adhesion
For thin coatings, the adhesive strength between the coating and the substrate was tested using the scratch method according to the GB/T 5270 − 1985 standard[26] (Fig. 8). Measurement results indicated that there was no significant peeling of the coating along the edges of the scratches for all experimental groups. This suggested that the adhesion of the coatings in all 16 experimental groups was good.
3.3 Determination of the optimal Ni-Cr-P preparation process
Based on the analysis of porosity spots in the Ni-Cr-P chemical plating orthogonal experiment, Groups 2, 3, 5, 6, 7, 9, 12, 15, and 16 exhibited favorable porosity levels.
According to the macroscopic appearance of the Ni-Cr-P-coated samples, Group 7 showed the presence of yellow spots, while Groups 2, 3, 5, 6, 9, 12, 15, and 16 had a good macroscopic appearance.
Considering the analysis of deposition rates, the optimal range for Ni-Cr-P coating deposition rate was in the range 2.5–5 µm/h. Below 2.5 µm/h, it was challenging to uniformly cover the plating area of the weaving needle, and a rate above 5 µm/h could impact the size control of the weaving needle. Within this range, only the deposition rates of Groups 2 and 9 met the requirements.
Based on the analysis of surface hardness, the Ni-Cr-P coating in Group 2 had a surface hardness of 577.63 HV0.2, and the coating in Group 9 had a surface hardness of 627.28 HV0.2. Ultimately, it was determined that the composition and process parameters of Group 9 from the orthogonal experiment were the optimal ones. The complete set of optimal composition and process parameters are listed in Table 10.
Table 10
Optimal compositions and process parameter ranges from the orthogonal experiment.
Plating solution component/parameter
|
Parameter range
|
NiSO4·6H2O
|
10 g/L
|
CrCl3·6H2O
|
12 g/L
|
NaF
|
3 g/L
|
NaH2PO2·H2O
|
30 g/L
|
C6H8O7·H2O
|
5 g/L
|
C3H6O3
|
20 ml/L
|
NaC2H3O2·3H2O
|
20 g/L
|
H2NCSNH2
|
1 ppm
|
C19H42BrN
|
10 ppm
|
pH
|
5.5
|
Temperature
|
70℃
|
3.4 Surface hardness of the Ni-Cr-P coating following heat treatment
To investigate the impact of heat treatment on the substrate and Ni-Cr-P coating, the latter was heated to different temperatures, specifically 180°C, 200°C, 220°C, and 240°C, each maintained for 1 h, followed by cooling to room temperature. Figure 9 shows the surface hardness bar chart of the 65Mn alloy steel substrate, the untreated Ni-Cr-P coating, and the Ni-Cr-P-coated samples following heat treatment at different temperatures.
The surface hardness of the Ni-Cr-P-coated samples was significantly higher than that of the substrate, increasing from 495 to 627 HV0.2. Within the heat treatment temperature range of 180°C to 240°C, the surface hardness of the Ni-Cr-P-coated samples gradually decreased following an initial increase. At 180°C, the surface hardness reached a minimum of 548 HV0.2, while at 220°C, the surface hardness peaked at 618 HV0.2. Although the surface hardness of the sample was relatively high at 220°C, it is essential to consider that, with increasing temperature, the grain size of the sample’s metallographic structure also increased, leading to a decrease in material toughness and strength[27].
In contrast, at 200°C, the surface hardness reached 613 HV0.2, and was also more conducive to suppressing the growth of metallographic structure grains. Considering these factors, it was determined that the optimal heat treatment temperature for 65Mn alloy steel with a Ni-Cr-P coating is 200°C.
3.5 Microscopic morphology of the Ni-Cr-P coating following heat treatment
Four 65Mn alloy steel samples with the Ni-Cr-P coating under optimal process conditions were subjected to heat treatment at temperatures of 180°C, 200°C, 220°C, and 240°C, respectively, each maintained for 1 h, followed by cooling to room temperature. Figure 10 presents the microscopic morphology of the untreated Ni-Cr-P coating on the 65Mn alloy steel substrate under a metallographic microscope, both at the surface and in cross-section, with magnifications of × 693 and × 1040, respectively.
In Fig. 10a and b, the surface microscopic morphology of the coating is shown. Due to the thinness of the coating, it was challenging to completely cover the original polishing marks on the substrate[28]. Overall, the coating appeared to evenly cover the substrate, but there were still a few microscopic pores and water droplet-shaped nodular protrusions. Figure 10c and d depicts the cross-sectional microscopic morphology of the coating, revealing a uniform and smooth white appearance, tightly bonded to the substrate.
Figure 11 shows the microscopic morphology of the Ni-Cr-P-coated samples following heat treatment at four different temperatures for 1 h, with magnifications of ×2000 (left) and ×1000 (right). From the images, it can be seen that, at the highest heat treatment temperature of 240°C, the surface morphology of the Ni-Cr-P coating shows minimal changes compared to before heat treatment. The coating structure consists of accumulated, unevenly sized, closely arranged cell-like units. The surface microscopic structure is dense, with a few microscopic pores and water droplet-shaped nodular protrusions.
3.6 XRD spectra of the Ni-Cr-P coating following heat treatment
Figure 12 displays the XRD spectra of the four samples of Ni-Cr-P coating following 1 h of heat treatment at different temperatures, which, from the graphs, can be seen to be essentially identical. Two distinct characteristic peaks are present at around 2θ = 45° and 65°, corresponding roughly to the characteristic peaks of the Ni(111) crystal plane at 44.5°, the Cr(110) crystal plane at 44.5°, and the Cr(200) crystal plane at 64.5°, according to the standard card.
3.7 Friction and wear performance analysis of the Ni-Cr-P coating following heat treatment
The UMT-2 friction test machine was employed to conduct reciprocating friction and wear experiments on the Ni-Cr-P coating. The tests were performed on the 65Mn alloy steel substrate, the Ni-Cr-P coating substrate, and the Ni-Cr-P coating substrate following heat treatment at 200°C. Figure 13(a), (b), and (c) shows the microscopic morphology of wear scars obtained from the friction and wear experiments on the 65Mn alloy steel substrate, the Ni-Cr-P coating substrate, and the Ni-Cr-P coating following heat treatment at 200°C, respectively
From Fig. 13(a), it can be seen that the wear scar exhibits a comet-like tail from left to right, with rust-colored ends and noticeable traces of oxidation. The widest part of the wear scar measured 1025.18 µm. A large amount of wear debris was generated during the friction process, and frictional heat oxidized it. Numerous quantities of wear debris were found adhering to the substrate on the local wear scars, indicating significant adhesive wear. The main reason for the comet-like tail of the wear scar was the poor wear resistance of the substrate[29]. As the GCr15 steel ball continuously penetrated the 65Mn alloy steel sample, the resistance of reciprocating friction increased, and the stroke gradually decreased.
In Fig. 13(b), the overall shape of the wear scar appears as a long rod with circular ends. The upper edge of the wear scar shows a white coloration, with only the central part exhibiting the color of oxidized iron filings and a sky blue coloration. This indicates that the coating had been partially worn, and the oxidized wear debris from coating delamination appears sky blue, while the oxidized wear debris from substrate wear appears rust-colored. The widest part of the wear scar measured 1008.58 µm, with some adhering wear debris in the local area, indicating adhesive wear.
In Fig. 13(c), the main body of the wear scar also presents a long rod shape with circular ends. The overall wear scar appears white, with sky blue wear debris in the left half, suggesting that the coating has not been worn through. The wear debris acts as a lubricant during reciprocating friction, continuously moving back and forth and eventually adhering to the left half of the wear scar. The widest part of the wear scar measured 930.10 µm. Under identical experimental conditions, a wider maximum width of the wear scar in reciprocating friction experiments indicated poorer wear resistance. In summary, the wear resistance of the Ni-Cr-P coating following heat treatment was superior to that of the untreated Ni-Cr-P coating and significantly better than the 65Mn alloy steel substrate.
3.8 Friction coefficient analysis of the Ni-Cr-P coating following heat treatment
Figure 14 shows the friction coefficient plots for the 65Mn alloy steel substrate, Ni-Cr-P-coated sample, and the Ni-Cr-P-coated sample following heat treatment at 200°C. From the graphs, it can be seen that the friction coefficient of the substrate rapidly jumped from 0.1 to 0.35 within a short time and then slowly increased over time, stabilizing around a value of 0.5. The friction coefficient of the Ni-Cr-P coating sample quickly jumped from 0.1 to 0.5 within an extremely short time and fluctuated thereafter. For the Ni-Cr-P-coated sample following heat treatment, the friction coefficient rapidly jumped to 0.4 within a very short time, then slightly decreased before gradually climbing, roughly stabilizing around a value of 0.4.
In terms of friction coefficient, the Ni-Cr-P coating following heat treatment exhibited better wear resistance compared to the untreated Ni-Cr-P coating, and was also superior to the 65Mn alloy steel substrate.
The above experimental results indicate that the surface hardness of the Ni-Cr-P coating significantly increased following heat treatment at 200°C compared to the substrate, approaching the surface hardness of the untreated Ni-Cr-P coating. However, in terms of wear resistance and friction coefficient, the Ni-Cr-P coating following heat treatment outperformed both the substrate and the untreated Ni-Cr-P coating.
3.9 Corrosion resistance performance comparison and analysis of the Ni-Cr-P coating following heat treatment
The corrosion resistances of the 65Mn alloy steel substrate, the Ni-Cr-P-coated sample, and the Ni-Cr-P-coated sample following heat treatment at 200°C were evaluated using the CH1660E electrochemical workstation. Figure 15 presents the polarization curves for these three samples, and Table 10 provides the electrochemical corrosion parameters obtained after fitting the polarization curves. Ecorr and Icorr represent the corrosion potential and current density, respectively. Cat slp and Ano slp represent the reciprocals of the absolute values of the cathodic and anodic slopes, while Rp represents the linear polarization resistance after fitting[30]. A more positive corrosion potential indicates a lower tendency for corrosion, a smaller corrosion current density suggests a slower corrosion rate, and a higher polarization resistance reflects better corrosion resistance.
A more positive corrosion potential, smaller corrosion current density, and higher polarization resistance for the Ni-Cr-P coating following heat treatment would indicate improved corrosion resistance compared to the untreated Ni-Cr-P coating and the substrate.
Table 11
Electrochemical corrosion test results.
Sample
|
−Ecorr/mV
|
Rp/Ω
|
Icorr/µA
|
Cat slp (1/V)
|
Ano slp (1/V)
|
Substrate
|
569
|
531.6
|
61.4
|
5.311
|
8.006
|
Ni-Cr-P coating
|
445
|
939.2
|
42.24
|
4.873
|
6.087
|
Ni-Cr-P coating following heat treatment at 200°C
|
389
|
3197.8
|
14.48
|
5.540
|
3.852
|
From the curves in Fig. 15, it can be seen that the anodic resistances of the 65Mn alloy steel substrate and Ni-Cr-P-coated samples were greater than the cathodic resistance, while the cathodic resistance of the Ni-Cr-P coating sample following heat treatment was greater than the anodic resistance. This indicates that the former two rely on the anodic protection mechanism[31], while the latter shows a relatively constant corrosion current in the range − 0.1–0.2 V, suggesting the occurrence of significant passivation. The corrosion resistance depends on whether the sample can quickly form a passivation film in the corrosive medium, preventing further corrosion[32]. From Table 11, it can be seen that the self-corrosion potentials of the three samples were 569, 445, and 389 mV, respectively, and the corrosion currents were 61.4, 42.24, and 14.48 µA, respectively. Both the self-corrosion potential and self-corrosion current showed a gradual decreasing trend. The polarization resistances of the three samples were 531.6, 939.2, and 3197.8 Ω, respectively, showing a gradual increasing trend. The corrosion current density was the lowest, and the corrosion potential was relatively the most positive for the Ni-Cr-P coating treated at 200°C. Under the given potential, the Ni-Cr-P coating following 200°C heat treatment exhibited the lowest corrosion rate. These results indicate that the Ni-Cr-P coating following 200°C heat treatment had better corrosion resistance compared to the other two samples.