XRD analysis
The XRD technique was used to identify the phases present during the pack cementation process. Figure 1 shows the XRD pattern that was conducted for the chromizing, chromotitanizing, and titanizing-coated low carbon steel samples.
Figure (1) (a) shows the X-ray patterns for coated specimen chromized at 900°C for 5hr (48%FeCr) together with the positions of all Bragg reflections for the identified phases. For the samples treated at 900ºC, there is the major presence of Cr1.36Fe0.52 intermetallic type, and in smaller quantities Cr2O3, C = Cr, like those indicated by the intensity of diffraction peaks. Al2O3 peaks were also found as a residue from the filler material used on the pack mixture.
Figure (1): X-ray diffraction pattern for some coated specimens
The X-ray diffraction pattern of the treated samples for chromotitanized with different percentage of ferrochrome and ferrotitanium powders at 900, 1000, and 1100°C for 3, 5, and 7hrs., resulted in the formation of Cr1.9Ti, Ti Fe intermetallic type and Cr2O3 and TiO2 oxides beside Al2O3. This suggests that the temperature in pack chromatinization is an important parameter controlling the formation of oxide and/or carbon compounds. The formation of (Cr,Fe)2N1-x is possible due to the nitriding reaction of chromium and iron after the decomposition of NH4Cl, which is added to the chromising mixture as an activator.[11] The ferritematrix is not revealed in all analyses due to the reduced penetration of the X-rays, which is in agreement with the study by Arai and Moriyama.8
Figure (1) (d) shows the X-ray patterns for coated specimen titanized at 900°C for 5hr (48%FeTi) The titanizing-coated low carbon steel samples shows TiFe phase which is known to be stable thermodynamically, the peak corresponding to TiFe phase appeared in the XRD results. It was reported that isolated TixFe particles were detected by SIMS imaging for the Ti-0.078 wt% Fe system, but they might be too tiny to be detected by the XRD method [12–13]. Other phases such as Ti O2 and Ti0.86 were detected.
SEM
Figure 2 shows the morphology of the low carbon steel surface, which was chromized, chromotitinized, and titanized to form a coated film at different bath composition.
Figures 2(a) show the morphology of the low carbon steel surface, which was chromized, the surface morphology after Chromizing treatments at 900°C shows a dense structure for the layer of expanded austenite, accompanied by a uniform chromized layer with a very smooth finish of the surface, and no visible cracks were observed. It was due to the intensive chromized precipitation that occurred and expanded austenite was also detected, as was evidenced in XRD test results. The surface morphology for the chromotitanized coating on the low carbon steel surface is shown in Figs. 2(b) deposition of Cr/Ti at a low deposition time will result in a surface that is characterized by an amorphous matrix that contains a fine nanocrystal fiber structure that is visible in SEM images of this sample. Also, a longitudinal micro void and rough surface can be detected in this image that formed in the coating's surface. which caused a increase in the amount of deposited coating. Figures 2(c) shows the deposed for Ti coating increased to 5hrs., a higher deposition rate occurred, which resulted in a change in the morphology towards a denser microstructure, more uniform coating, a much coarser surface finish than the former surface layer, and visible micro voids. Also, a nano-crystalline fiber structure can be detected.
For the chromized and chromotitanized surfaces the particles formed could be Cr oxides such as Cr2O3 and carbides [14]. Thus, the darker region can present the chromium-rich region (Fig. 2(a)) distributed across the treated surface. Moreover, no cracks were visible on the surface of the Cr chromized. However, it is known that the deposition of Cr2O3 in some parts of the Cr coated may lead to the apparition of cracks. Moreover, some pores have been observed and according to the studies conducted by Fan et al. [15], the kirkendall effect was found to be responsible for pores and voids formation in chromizing coatings. Deposition of Cr2O3 can also increase the roughness of the coated substrate [16].
Figure (2) SEM of a specimen Chromized at 900°C for 5 hr, (a) the Chromized mixture contains 48 wt%FeCr ferrochromium, 50 Wt% Al2O3 powder and 2 Wt% NH4Cl. (b) Specimen chromotitanized at 900°C for 5 hr, the chromotitanized mixture contains 24 wt%FeTi ferrotitanium + 24 wt%FeCr ferrochromium, 50 Wt% Al2O3 powder and 2%Wt NH4Cl. (c) Specimen titanized at 900°C for 5 hrs., the titanized mixture contains 48 wt%FeTi ferrotitanium, 50 Wt% Al2O3 powder and 2%Wt NH4Cl.
Corrosion behavior
Figure 6 shows the Tafel polarization curves for coated and uncoated low carbon steel. It provides several significant parameters, such as corrosion current density (icorr), corrosion potential (Ecorr), and corrosion rate (CR).
The Mils Penetration per Year can be calculated by the given formula [17, 18]:
Mils Penetration per Year (MPY) = 0.13 * icorr * EW / Density
Additionally, to determine the precise calculation of the Mils Penetration per Year (MPY) of each sample that corresponded to current density of corrosion rate (icorr) from the graph, (EW) is the equivalent weight. All results are tabled as presented in Table 3. The MPY results decreased from 0.3023 to 0.0127 as the corrosion resistance properties of high carbon steel increased. As Cr content escalated, volume fraction of retained austenite increased and its stability improved, which minimised the grain boundary corrosion, as less iron atoms moved that accelerated corrosion reaction, thus improving the corrosion resistant properties.
4.6 Electrochemical Corrosion Test:
4.6.1. Linear Polarization Experiments
Table (3) shows the electrochemical parameters derived from linear polarization experiments for blank and coated low carbon steel. The table includes the different process parameters.
Figure (3) shows the effect of ferrochromium percent on the corrosion rate of the coated specimen at temperature of 900°C, 1000°C and 1100°C at different coating times in 3.5% NaCl aqueous Solution at room temperature. The corrosion resistance of the coated samples was better than without coatings. When the chromizing temperature was 1100°C, there was no percolation layer on the surface of the sample and the corrosion rate was the highest. When the chromizing temperature was 900°C, the corrosion rate was the lowest. With the increase of the chromizing temperature, the corrosion rate increased, and the corrosion resistance decreased. When the chromizing temperature was too high, holes appeared on the surface of the sample, the compactness decreased, the corrosion of the chromized layer began to increase, and the corrosion transitioned from uniform to pitting, resulting in increased corrosion. The corrosion rate decreases with increasing ferrochromium percent in the pack and increasing time. But the corrosion rate at 1000°C and 1100°C increases with increasing time and the corrosion rate at 1100°C has the highest value. This may be due to the bad effect of cracks and voids appearing at high temperature and longtime of coating.
The chromising of steel and ferrous alloys produces a surface layer composed mainly of Cr, Fe and C, which significantly increase the hardness, wear and corrosion resistance of the substrate. [19, 20]
Figure (3): Effect of ferrochromium percent in pack on the corrosion rate at different temperature and different time in 3.5% NaCl Solution at room temperature
Figure (4): Effect of ferrotitanium percent in pack on the corrosion rate at different temperature and different time in 3.5% NaCl Solution at room temperature
Figure (5): Effect of the pack cementation composition on the corrosion rate at different temperatures and time in 3.5% NaCl solution at room temperature.
Figure (6) SEM micrographs from a cross-section of a sample uncorded and corroded chromized sample.
Figure (6) shows the microstructure of the chromized coated and corroded coated samples after corrosion test in 3.5%Nacl solution. The chromizing temperature is 1100°C and 5hrs. Before corrosion, the coating surfaces are uneven Fig. 6 (A), while Fig. 6(B), shows cracks and holes on the corroded surface.
For the tetanized samples, Ti-rich precipitate particles are observed in the microstructure of designed steel (Fig. 2c). The titanium-containing corrosion products are extremely dense and free of pores and cracking, which is beneficial for corrosion resistance. Other investigations show that the addition of titanium element increases the crystallite size of geothite and produces double domain particles consisting of the particles core and porous crystallite shell [21]. During this study it is observed that the corrosion rate of the coated tetanized steel is higher than chromized samples.
After corrosion, irregular-shaped corrosion products are unevenly distributed on each coating.
Corrosion occurs mainly in coating defects such as tiny cracks and holes. The corrosion process passes through three stages. Firstly, pitting corrosion occurs in the defects of the coating. Secondly, the pitting corrosion grows into depth and spreads over the surface. Lastly, the coating is corroded.
4.6.1. potiondynamic polarization experiments
In Fig. 7, the potentiodynamic polarization curves obtained in artificial sea water (3.5% NaCl) for some pack coated samples, the low carbon steel substrate coated and uncoated samples are compared. After corrosion testing, the pack cemented layers of Ti, Cr/Ti and the hard chrome provided superior corrosion resistance when compared with the low carbon steel substrate.
The electrochemical reactions that occur on the surfaces of the coated samples are far less destructive than those which occurred on the unprotected carbon steel substrate. This is shown by the potentiodynamic polarization curves of the three coatings and the hard chrome that exhibit a passivity region in which the rate of corrosion reaction is low. Moreover, the corrosion currents are shifted to the left, which indicates minor current values relative to the substrate.
Among the pack chromizing conditions, the ones treated at 900ºC for 7 hrs resulted in better corrosion behavior.
The increase in corrosion resistance for the samples treated at 900ºC can be attributed to the fact that these samples are externally composed mainly of (Cr1.36Fe0.52, Cr, and Cr2O3), as shown by the X-ray diffraction analysis (Fig. 3b). The polarization curves also show that the protection against corrosion increases with the pack cementation time and temperature, which is the most significant parameter.
It is well known that the higher Cr concentration that the coating possesses, the better corrosion resistance that the coating exhibits. This fact suggests that at 900ºC, for 7 hrs. the Cr concentration on the layer is higher, which results in better corrosion protection (0.0127).
Figure (7), the potentiodynamic polarization curves obtained in artificial sea water (3.5% NaCl) for some pack coated samples
Table 5 shows the electrochemical parameters, such as corrosion potential Ecorr, corrosion current Icorr and polarization resistance Rp, of the tested samples collected from the polarization curves. Rp is calculated by the quotient V(Ecorr)/I(Icorr), which indicates that if Rp decreases, corrosiveness of the medium increases.
The decreasing order of corrosion resistance of the samples is hard chrome, followed by the sample chromized at 900ºC for 7 h, 900ºC for 5 h, 900ºC for 3 h and the substrate which undergoes major corrosion rate.
The protection against corrosion increases with pack treatment time and temperature, with temperature being the most significant factor. All chromium coatings are more corrosion resistant than the low carbon steel substrate.
Table (5) shows the electrochemical parameters derived from linear polarization experiments for blank and coated low carbon steel alloy. The table includes the different process parameters.
Table (5): Result of linear polarization experiments at different temperatures for different times in 3.5% NaCl solution at room temperature
Specimen No
|
Ecorr, V
|
Rp, Ω.
|
Icorr, A/cm2
|
Corr. Rate, mm/year
|
%Cr
|
%Ti
|
Temp. (ºC)
|
Time (h)
|
Blank
|
-0.622
|
1.217E + 00
|
6.89E-04
|
0.3023
|
--
|
--
|
--
|
--
|
1
|
-0.443
|
3.382E + 01
|
1.734E-06
|
0.02502
|
100
|
0
|
900
|
3
|
2
|
-0.51
|
7.702E + 01
|
2.56E-06
|
0.0369
|
75
|
25
|
900
|
3
|
3
|
-0.452
|
2.897E + 02
|
2.974E-06
|
0.0429
|
50
|
50
|
900
|
3
|
4
|
-0.441
|
9.806E + 01
|
4.685E-06
|
0.05307
|
25
|
75
|
900
|
3
|
5
|
-0.502
|
8.503E + 0
|
4.968E-06
|
0.07168
|
0
|
100
|
900
|
3
|
6
|
-0.567
|
2.882E + 01
|
2.245E-06
|
0.03239
|
100
|
0
|
900
|
5
|
7
|
-0.48
|
2.539E + 01
|
3.48E-06
|
0.05021
|
75
|
25
|
900
|
5
|
8
|
-0.463
|
3.866E + 01
|
4.401E-06
|
0.0638
|
50
|
50
|
900
|
5
|
9
|
-0.521
|
2.704E + 01
|
7.423E-06
|
0.08406
|
25
|
75
|
900
|
5
|
10
|
-0.444
|
7.463E + 00
|
6.481E-06
|
0.09351
|
0
|
100
|
900
|
5
|
11
|
-0.454
|
4.8E + 01
|
2.515E-06
|
0.0127
|
100
|
0
|
900
|
7
|
12
|
-0.527
|
9.503E0 + 1
|
1.875E-06
|
0.0212
|
75
|
25
|
900
|
7
|
13
|
-0.392
|
1.88E + 02
|
8.80E-07
|
0.02681
|
50
|
50
|
900
|
7
|
14
|
-0.455
|
7.06E + 01
|
2.412E-06
|
0.02732
|
25
|
75
|
900
|
7
|
15
|
-0.511
|
4.518E + 01
|
2.804E-06
|
0.04046
|
0
|
100
|
900
|
7
|
1
|
-0.401
|
4.12E + 01
|
2.201E-06
|
0.03175
|
100
|
0
|
1000
|
3
|
2
|
-0.540
|
1.387E + 01
|
2.095E-06
|
0.04199
|
75
|
25
|
1000
|
3
|
3
|
-0.480
|
2.539E + 01
|
3.48E-06
|
0.05021
|
50
|
50
|
1000
|
3
|
4
|
-0.463
|
3.866E + 01
|
4.401E-06
|
0.0638
|
25
|
75
|
1000
|
3
|
5
|
-0.521
|
2.704E + 01
|
7.423E-06
|
0.08406
|
0
|
100
|
1000
|
3
|
6
|
-0.467
|
6.782E + 01
|
2.415E-06
|
0.03484
|
100
|
0
|
1000
|
5
|
7
|
-0.344
|
6.507E + 01
|
5.213E-06
|
0.05904
|
75
|
25
|
1000
|
5
|
8
|
-0.571
|
2.087E + 01
|
5.297E-06
|
0.07643
|
50
|
50
|
1000
|
5
|
9
|
-0.471
|
9.787E + 0
|
8.416E-06
|
0.09523
|
25
|
75
|
1000
|
5
|
10
|
-0.409
|
1.095E + 02
|
1.007E-06
|
0.09532
|
0
|
100
|
1000
|
5
|
1
|
-0.397
|
1.767E + 01
|
7.259E-06
|
0.1047
|
100
|
0
|
1100
|
3
|
2
|
-0.457
|
1.518E + 01
|
8.611E-06
|
0.1242
|
75
|
25
|
1100
|
3
|
3
|
0.1242
|
6.947E + 00
|
1.39E-05
|
0.1574
|
50
|
50
|
1100
|
3
|
4
|
-0.387
|
1.235E + 01
|
1.498E-05
|
0. 1697
|
25
|
75
|
1100
|
3
|
5
|
-0.473
|
2.213E + 01
|
1.465E-05
|
0.211
|
0
|
100
|
1100
|
3
|
6
|
-0.459
|
1.704E + 01
|
7.485E-06
|
0.108
|
100
|
0
|
1100
|
5
|
7
|
-0.521
|
5.123E + 0
|
1.329E-05
|
0.1918
|
50
|
50
|
1100
|
5
|
8
|
-0.312
|
2.797E + 00
|
2.797E + 00
|
0.2516
|
0
|
100
|
1100
|
5
|
The increase in corrosion resistance for the samples treated at 900°C can be attributed to the fact that these samples are externally composed mainly of Cr and Cr1.36Fe0.52, as shown by the X-ray diffraction analysis (Fig. 1a). The polarization curves also show that the protection against corrosion increases with the pack chromising time but decreases with temperature, which is the most significant parameter.
It is well known that the higher Cr concentration that the coating possesses, the better corrosion resistance that the coating exhibits.[22]. This fact suggests that at 900°C, the Cr concentration on the layer is higher, which results in better corrosion protection.
From the experiments, it can be concluded that pack chromizing treatment is an effective way to obtain layers with high chromium concentration, high hardness and good wear and corrosion resistance. An increase in activator concentration from 6 to 12% did not generate significant changes in the thickness and morphology of the produced layers, which were found to increase with treatment temperature and time. [23–24]
The sample pack chromized at 900°C for 7 h yielded a corrosion resistance close to the hard chrome coating, which is a promising condition for replacing the commercial hard chromium coating [25].
Thus, chromizing at 900°C for 7 h provides an optimum condition to obtain higher corrosion and wear resistance.
There are only a few mentions concerning the solution tetanized layers, consisting of a solid solution of Ti in α-Fe, on low carbon steels, because of a low titanium content in these layers, and consequently, their poor quality [26, 27].
The thickness of the coated later increased gradually with the increase of time or temperature. The higher the coating temperature or the longer the holding time, the greater the tendency to form holes in the coat, as well as the greater the chances of melting or fusion bonding on the surface.
The results obtained denote that the corrosion resistance of steel was enhanced significantly by coating. This can be followed shifted of Ecorr in the noble direction (more positive values) for all coated specimens rather than the blank. Icorr for coated specimen decreased than the blank. At all coating times and coating temperatures, the corrosion rate was increased with increasing ferrotitanium percent in the cementation pack.
It can be noted that the corrosion resistance at 900°C of the coated specimen better than the corrosion resistance at 1000°C and 1100°C, it means that:
C.R at 900°C < C.R at 1000°C < C.R at 1100°C.
To address this challenge, turning to the process pack cementation, wherein the addition of dopant elements and substitutions to the mixture cementation pack can alter its properties and improve surface characteristics. [28]