Cancan Liuab,
Qingbiao Liab,
Jun Liang*a,
Jiansong Zhou*a and
Lingqian Wanga
aState Key Laboratory of Solid Lubrication, Lanzhou Institute of Chemical Physics, Chinese Academy of Sciences, Lanzhou 730000, People's Republic of China. E-mail: jliang@licp.cas.cn; jszhou@licp.cas.cn
bUniversity of Chinese Academy of Sciences, Beijing 100049, People's Republic of China
First published on 18th March 2016
An attempt has been made to improve the corrosion behavior of WE43 magnesium alloy by laser surface melting (LSM) using a 10 kW continuous-wave CO2 laser. The microstructure evolution of WE43 alloy after LSM treatment was analyzed by using scanning electron microscopy, energy-dispersive spectroscopy and metallographic microscope. The corrosion resistance of specimens was assessed by electrochemical and immersion tests. Results showed that the LSM treated WE43 alloy presented a uniform microstructure with refined grains, enriched alloying elements and redistributed intermetallic compounds. The LSM treatment effectively improved corrosion resistance of WE43 alloy, which was mainly associated with enrichment of alloying elements in α-Mg matrix and uniform distributions of the refined Mg14Nd2Y phase.
Corrosion of Mg alloys is essentially a surface degradation process, and it can be reduced by proper modification of the surface microstructure and/or composition.7,8 Various surface treatments including conversion coating, electrochemical deposition, plasma electrolytic oxidation, ion implantation, gas phase deposition and laser surface treatment, are applied to improve corrosion resistance of Mg alloys.8–12 Of these methods, laser surface melting (LSM) is one of the most effective techniques to modify surface properties, because it can homogenize and refine the microstructure, and dissolve the second phases.13,14 A number of attempts have been made to investigate the effects of LSM treatment on the corrosion behaviour of Mg alloys.15–24 It has been proved that the LSM treatment has positive influences on the corrosion resistance of AZ- and AM-type Mg alloys, such as AZ31, AZ61, AZ91 and AM60.15–21 The enhanced corrosion resistance was mainly attributed to the Al enrichment, pronounced grain refinement and uniform distributions of Mg17Al12 phase. For the Mg alloys free of Al element, relatively rare researches7,22–24 are carried out to explore the corrosion behaviour by LSM treatments. Majumdar7 and Khalfaoui22 studied the effect of LSM treatment on the corrosion resistance of WEZ and ZE41 Mg alloys, respectively. Results revealed that the LSM treatment improved their corrosion resistance, resulting from the refinement of grains and redistribution of the intermetallic particles. Guo et al.23 observed similar improvement in case of WE43 alloy due to the dissolution of Mg12Nd into α-Mg matrix. Unfortunately, they did not analyse corrosion mechanism in depth. However, Banerjee et al.24 indicated that the corrosion resistance of ZE41 Mg alloy was not significantly improved by LSM treatment, although microstructural refinement was achieved. This is due to absence of beneficial alloying elements such as Al.
WE43 Mg alloy can offer the required creep resistance for long-term usage at elevated temperature (up to 250 °C), which exhibits important applications in the aerospace industries.25 However, so far, little efforts have been made to examine the microstructure and corrosion behaviour of the LSM treated WE43 Mg alloy in detail. In this work, LSM treatment has been conducted on WE43 Mg alloy containing Y and Nd as the major alloying elements. Microstructural changes induced by LSM treatment are analysed and its effect on corrosion behaviour is also investigated.
Specimens | Content of elements (wt%) | ||||
---|---|---|---|---|---|
Mg | Y | Nd | Gd | Zr | |
WE43 | 91.37 | 4.84 | 2.82 | 0.42 | 0.55 |
α-Mg matrix | 95.56 | 3.44 | 0.86 | 0.33 | 0.10 |
1 | 77.21 | 5.38 | 15.89 | 1.22 | 0.31 |
2 | 25.85 | 67.90 | 2.64 | 1.27 | 2.34 |
3 | 38.02 | 0.00 | 0.39 | 0.05 | 61.55 |
α-Mg matrix (LSM) | 90.98 | 5.07 | 2.77 | 0.52 | 0.62 |
Prior to immersion test, the specimens were sealed by polyurethane with the working surface exposed. For immersion test, the specimens were suspended vertically in NaCl solutions with chloride ion concentrations of 0.01 M, 0.1 M and 0.62 M, respectively. The evolved hydrogen was collected by the combination of the funnel and the burette above the specimen. The burette was initially filled with corrosion solution, which was gradually displaced by the evolved hydrogen during immersion test. The experiment device used to collect hydrogen was similar to that described in the literature.26,27 After certain immersion periods, the surface appearances of samples were taken by a digital camera. After that, the specimens were rinsed with distilled water to remove salt deposits, and then dried in warm air. A scanning electron microscope was used to observe the surface and cross-sectional corrosion morphologies of the specimens. To calculate the weight loss, the corrosion products were removed with a chromic acid solution (200 g L−1 CrO3 + 10 g L−1 AgNO3),26 rinsed with ethanol, dried in air, and finally weighed.
Fig. 3 exhibits the cross-section and surface micrographs of LSM treated WE43 alloy. A continuous and homogeneous modified layer formed on the top surface of WE43 alloy (Fig. 3a). The modified depth was approximately 1.15 mm. The surface microstructure revealed highly refined grain structure with uniform dispersion of fine Mg14Nd2Y phase (Fig. 3b). The average grain size decreased to 6.4 μm. Besides, relatively small amounts of Y-rich and Zr-rich phases still remained within the melted layer. Fig. 4 presents the element distribution of the LSM treated WE43 alloy. It was obvious that Mg and the alloying elements (Y, Nd, Gd and Zr) in the modified layer distributed more uniformly than that in the as-received one, which proved the redistribution of intermetallic compounds. The chemical composition of α-Mg matrix after LSM treatment is shown in Table 1. Compared to the as-received alloy, the content of all alloying elements in the α-Mg matrix was increased, especially the Y and Nd elements, manifesting the dissolution of the intermetallic compounds. In summary, LSM treatment resulted in refined grains, enriched alloying elements and redistributed intermetallic compounds in the modified layer of WE43 alloy.
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Fig. 5 Potentiodynamic polarization curves of the as-received and LSM treated WE43 alloy in 0.62 M NaCl solution. |
Specimen | Ecorr (mV vs. Ag/AgCl) | icorr (A cm−2) |
---|---|---|
As-received | −1412 | 2.93 × 10−5 |
LSM | −1271 | 8.51 × 10−6 |
EIS test was performed to obtain further information on corrosion resistance of the as-received and LSM treated WE43 alloy. As shown in Fig. 6a and b, the EIS spectrums of both specimens are characterized by three loops, i.e. a capacitive loop in the high frequency, another capacitive loop in the medium frequency and an inductive loop in the low frequency. Based on the characteristics of EIS spectrum, an equivalent circuit is proposed in Fig. 6a. In the equivalent circuit,30,31 Rs represents the solution resistance, R1 is resistance of naturally formed passive film on the substrate exposed to the corrosive electrolyte in parallel with the film layer capacitance C1, and R2 represents charge transfer resistance of the faradaic process on the metal surface in parallel with double layer capacity C2. To account for the inductive behaviour, an inductor L in series with a resistance R3 was introduced in this model. The Nyquist and Bode plots are fitted with this equivalent circuit and the fit results are shown in Fig. 6a and b. The values of the fitted circuit elements are summarized in Table 3. It can be found that the LSM treated WE43 alloy exhibited much higher resistance values (R1, R2 and R3) than the as-received one, implying an increase in corrosion resistance after the LSM treatment. These results were in good agreement with the investigations of polarization curves.
Specimen | C1 μF cm−2 | R1 Ω cm2 | C2 μF cm−2 | R2 Ω cm2 | L Ω s cm2 | R3 Ω cm2 |
---|---|---|---|---|---|---|
As-received | 3 | 268 | 2.62 | 428 | 5102 | 220 |
LSM | 3 | 1268 | 1337 | 433 | 52![]() |
2295 |
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Fig. 7 Hydrogen evolution data (a) and corresponding corrosion rates (b) for the as-received and LSM treated WE43 alloys immersed in 0.62 M NaCl solution. |
Table 4 lists the corrosion rates after immersion in 0.62 M NaCl solution for different time. The Pi,EIS was instantaneous corrosion rate evaluated from EIS data (Fig. 5) using the low frequency limit as a good measure of the polarisation resistance and using values of the Tafel slopes.33 The Pi was instantaneous corrosion rate calculated from Tafel extrapolation using icorr (Table 2).32 The PW was average corrosion rate measured from weight loss.32 As shown in Table 4, the value of PW was very close to that of PH in the same immersion time. However, the values of Pi,EIS and Pi were much lower than that of PH in the same immersion time. These indicated the electrochemical technique, either EIS data or Tafel extrapolation, could not provided good measurements of the corrosion rate of WE43 alloy.
Specimens | 0.5 h | 1 h | 24 h | |||
---|---|---|---|---|---|---|
Pi,EIS (mm per year) | PH (mm per year) | Pi (mm per year) | PH (mm per year) | PW (mm per year) | PH (mm per year) | |
As-received | 0.50 | 9.49 | 0.67 | 10.54 | 100.68 | 128.18 |
LSM | 0.089 | 6.52 | 0.19 | 8.37 | 40.16 | 45.63 |
Fig. 8 gives the photographs of the as-received and LSM treated specimens after immersion in 0.01, 0.1 and 0.62 M NaCl solutions for certain time. For all specimens, the surface was characterized by local corrosion, although the extent of corrosion was different. The extent of corrosion damage of specimens, revealing a similar change trend as that of corrosion rates, increased with immersion time and chloride ion concentration. In addition, compared to the as-received one, the LSM treated specimens showed relatively light corrosion damage within the same immersion time and chloride ion concentration. It should be noted that the as-received specimens in 0.1 and 0.62 M NaCl solutions suffered from severe corrosion damage, a mass of corrosion products fell off from the alloy surface and thus the alloy surface became bumpy.
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Fig. 8 Photographs of the as-received (a1–c1) and LSM treated (a2–c2) WE43 alloy after immersion in NaCl solutions of different chloride for different time. |
To more clearly observe the corrosion features of the as-received WE43 alloy, the surface and cross-sectional micrographs of the specimens after immersion in 0.1 M NaCl solution for certain time are analysed. As shown in Fig. 9, the as-received alloy showed typical pitting corrosion. After 24 h immersion, the sample surface featured discrete corrosion damage (Fig. 9a). With the extending of immersion time, several adjacent corrosion pits merged together to form a large one. At the same time, the corrosion penetrated gradually into the interior of substrate. Up to 120 h, lots of corrosion products accumulated at the sample surface with the depth more than 470 μm (Fig. 9e). However, there were many cracks in the corrosion layer, indicating the limited corrosion protection to alloy. Interestingly, corrosion developed heterogeneously in the interior of the alloy. As shown in Fig. 9a2–e2, corrosion attack mainly focused on α-Mg matrix (grey region) while intermetallic grains (bright region) remained unchanged. Moreover, the Mg14Nd2Y phase identified by blue arrows could serve as a barrier to prevent the corrosion progress (Fig. 9a2 and b2).
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Fig. 9 Surface (a1–e1) and cross-section (a2–e2) corrosion morphologies of the as-received WE43 alloy after immersion in 0.1 M NaCl solution for different time. |
Fig. 10 presents the surface and cross-sectional micrographs of the LSM treated WE43 alloy during the immersion tests. In contrast to the as-received alloy, some raised corrosion products existed on the alloy surface after immersion for 24 h (Fig. 10a1). A larger corrosion pits could be observed until the 96 h of immersion. Meanwhile, the cross-sectional micrographs (Fig. 10a2–e2) indicated that the corrosion depth was much smaller than that of the as-received WE43 alloy in the same immersion time. The results of immersion tests further proved the positive effect of LSM treatment on the corrosion resistance of WE43 alloy.
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Fig. 10 Surface (a1–e1) and cross-section (a2–e2) corrosion morphologies of the LSM treated WE43 alloy after immersion in 0.1 M NaCl solution for different time. |
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Fig. 11 Schematic diagrams for the corrosion process of the as-received (a, b) and LSM treated (c, d) WE43 alloy. |
For the LSM treated WE43 alloy, some of intermetallic compounds (Mg14Nd2Y, Y-rich and Zr-rich phases) dissolved into α-Mg matrix, which significantly decreased the volume fraction of effective cathodes. On the other hand, the enrichment of alloying elements made corrosion potential of α-Mg matrix shift to the positive direction, lowering the corrosion susceptibility of α-Mg matrix. In addition, once the corrosion was initiated, the refined Mg14Nd2Y phases distributed evenly and mainly served as a barrier to impede corrosion process. Compared to the as-received WE43 alloy, the LSM treated specimen suffered slighter corrosion damage within the same immersion time (Fig. 11c and d).
(2) After LSM treatment, a modified layer with the depth of 1.15 mm formed on the top surface of WE43 alloy. In modified layer, grains were refined, alloying elements were enriched in α-Mg matrix and intermetallic compounds were dissolved and redistributed.
(3) The LSM treated WE43 alloy revealed better corrosion resistance than the as-received one, due to the combined effect of the lowering corrosion susceptibility of α-Mg matrix and the barrier effect of refined Mg14Nd2Y phase.
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