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Article

Microstructure and Antioxidative Performance of Y2O3-CeO2 Co-Modified Molybdenum Silicide Coatings

1
School of Material Science and Engineering, Chang’an University, Xi’an 710061, China
2
Postdoctoral Scientific Research Station of Mechanical Engineering, Chang’an University, Xi’an 710064, China
3
Technical Center, Jinduicheng Molybdenum Co., Ltd., Xi’an 710077, China
*
Author to whom correspondence should be addressed.
Coatings 2025, 15(3), 310; https://doi.org/10.3390/coatings15030310
Submission received: 9 February 2025 / Revised: 28 February 2025 / Accepted: 3 March 2025 / Published: 7 March 2025
(This article belongs to the Special Issue Advances in Ceramic Materials and Coatings)

Abstract

:
To enhance the high-temperature oxidation resistance of molybdenum-based materials, Y2O3-CeO2 co-modified silicide coatings were produced on molybdenum substrates using two-step pack cementation. The microstructure and phase composition of Y2O3-CeO2 co-modified composite coatings were examined both before and after oxidation. A detailed analysis of the antioxidant properties of the co-modified coatings and the mechanisms behind the modifications was also conducted. The incorporation of 1.0 wt.% CeO2 and 1.5 wt.% Y2O3 into the composite coatings resulted in a dense, non-porous, maximum-thickness microstructure. This microstructure is characterized by the uniform distribution of parallel MoSi2 and MoB layers on the substrate. In particular, the coating containing 1.5 wt.% Y2O3 exhibited superior oxidation resistance, with a weight gain of 0.29 mg/cm2 and an oxidation rate constant of 6.68 × 10−4 mg2/(cm4·h) after oxidation at 1150 °C for 255 h. During oxidation, a dense SiO2 oxide film is formed through the cooperation of Y2O3 and CeO2, inhibiting further Si diffusion into the substrate and reducing the formation of the Mo5Si3 layer.

Graphical Abstract

1. Introduction

Refractory metal molybdenum and its alloys exhibit exceptional properties, including high melting points and superior electrical and thermal conductivity [1,2]. These materials are commonly utilized as structural components in high-temperature settings within the aerospace and nuclear energy sectors [3,4]. However, molybdenum and its alloys are highly susceptible to rapid oxidation, resulting in the formation of volatile molybdenum trioxide (MoO3) at temperatures above 600 °C [5]. This process causes material degradation and a significant reduction in performance. The limited oxidation resistance significantly hinders the advancement of molybdenum and its alloys across various industries [4,6,7]. Therefore, the critical issue of poor oxidation resistance requires prompt resolution.
Currently, the enhancement of oxidation resistance in molybdenum and its alloys primarily relies on protective coatings [8,9]. Molybdenum disilicide (MoSi2) is the main silicide of molybdenum and is commonly utilized in various coating systems due to its impressive characteristics, including a high melting point (2030 °C), low density (6.24 g/cm3) and low coefficient of linear expansion (7.8 × 10−6/K) [10,11,12]. When temperatures exceed 1000 °C, molybdenum disulfide (MoSi2) forms a dense protective layer of glass silica (SiO2) on the coating’s surface, effectively preventing oxygen penetration and inhibiting oxidation on both the coating and substrate [13,14,15,16]. Currently, coating methods for preparing MoSi2 coatings on molybdenum surfaces include vapor deposition, plasma spraying, slurry process, and pack cementation (HAPC) [17,18,19,20]. Among these, HAPC is preferred due to its cost-effectiveness, versatility in coating complex geometries, and ability to produce dense and adherent coatings with superior oxidation [8,21]. Researchers like Zhai et al. [22] have successfully prepared MoSi2 coatings on Mo substrates through pack cementation, observing the formation of a glass-like SiO2 layer post-oxidation at 1300 °C. This layer aids in repairing coating cracks to some extent and prevents oxygen diffusion through them. However, the MoSi2 coating is subject to microcrack initiation during oxidation, leading to “pest oxidation” and coating failure, which severely limits its application [23,24].
Studies have shown that the incorporation of additives, such as aluminum, boron, and rare earth elements, can significantly improve the performance of MoSi2 coatings [25,26]. Al-doped MoSi2 forms the Mo(Si, Al)2 phase, which generates a protective Al2O3 film with a low coefficient of volume expansion during high-temperature oxidation, minimizing stress mismatch and preventing “pest oxidation” [27]. B-modified silicate coatings were able to fill defects such as pores and cracks promptly by producing lower viscosity B2O3, but B-modified silicide coatings had low density and lacked significant structural gradients, producing weak bonding between coatings [28]. Xiao et al. [29] demonstrated that CeO2 effectively refines the grain and increases the thickness of the MoSi2 coating. Similarly, Chen et al. [30] discovered that Y2O3 can improve the grain size and density of MoSi2 coatings. Some disilicide coatings modified with rare earth elements have shown promising antioxidant properties. Zhang et al. [31] investigated the oxidation stability of rare earth co-modified coatings applied to Nb-Ti-Si-based high-temperature alloys. It was demonstrated that these coatings exhibited enhanced antioxidant properties during cyclic oxidation tests at 1250 °C, resulting in a 31% reduction in oxidation rate. However, the simultaneous introduction of CeO2 and Y2O3 to enhance the functionality of the coating on molybdenum surface variations had rarely been reported, and the precise mechanism underlying the co-modification of multiple rare earth elements within composite coatings had yet to be unraveled in full.
In a previous study [32], it was established that a Ce content of 1.00 wt.% in the pack cementation process resulted in the formation of a MoSi2 layer with a uniform density. The objective of this paper is to examine the impact of Y2O3-CeO2 co-modification on the coating formation process and the antioxidant process by preparing Y2O3-CeO2 co-modified silicide coatings using two-step cementation. In view of the established optimal Ce content of 1.00 wt.%, the present study specifically investigated the influence of Y content on the coating’s phase composition, microstructure evolution, and high-temperature oxidation behavior. Furthermore, the mechanisms through which Yttrium (Y) and Cerium (Ce) facilitate the antioxidant processes were examined in depth.

2. Materials and Methods

2.1. Specimen Preparation

The Mo substrate (chemical composition listed in Table 1) was processed into a sample with 10 mm × 10 mm × 10 mm cut by wire-cut electrical discharge machining (WEDM). The surfaces were gradually ground using sandpaper (from 400 to 2000 grit) to achieve a smooth finish, followed by polishing with a diamond paste (particle size: 1.5 µm) to ensure a mirror-like surface. Subsequently, an ultrasonic cleaning apparatus was employed to clean the surface, which was then subjected to a drying process using a vacuum oven.
The experimental process is shown in Figure 1. A two-step pack cementation method obtained the coated samples of Y2O3-CeO2 co-modified silicide coatings. The powder mixtures consisted of pure boron (B), sodium fluoride (NaF), alumina (Al2O3), silicon (Si), aluminum (Al), silica (SiO2), cerium oxide (CeO2), and yttrium oxide (Y2O3), serving as boronizing agent and siliconizing agent. Detailed compositions of the pack mixtures are summarized in Table 2. Both powders were milled in a planetary ball mill at 600 r/min for 4 h. During the first boronizing process, the molybdenum substrate was fully encapsulated in porcelain boat. The porcelain boat was sealed using a mixture of silane coupling agent and Al2O3 powder, then transferred into a corundum-lined tubular furnace (OTF-1200X) under an argon atmosphere (flow rate: 10 mL/min). The temperature was precisely controlled by a K-type thermocouple positioned near the sample, with a heating rate of 5 °C/min to the target temperature of 1000 °C. The sample was isothermally sintered for 4 h to form a boride coating. For the second siliconizing process, the boride coating sample was re-encapsulated in siliconizing agent (with varying Y2O3/SiO2 ratios) and sintered at 1100 °C for 6 h under identical argon protection.

2.2. Characterization of Microstructure

The microstructure of the coating was observed before and after oxidation using a cold field emission scanning electron microscope (Hitachi S-4800 Cold Field Emission Scanning Electron Microscope (SEM), Tokyo, Japan). The cross-sectional morphologies of the coatings were analyzed using ImageJ 2 software and the thickness of each coating was measured. Additionally, the chemical composition of the samples was examined using X-ray spectroscopy. The phase composition of the coating was analyzed by an X-ray diffractometer (Bruker AXS D8 ADVANCE X-Ray Diffractometer, Karlsruhe, Germany). The target is copper, the diffraction angle is in the range of 20°~90°, the scanning speed is 10°/min, the electron acceleration voltage is 40 kV, and the current is 40 mA.

2.3. Oxidation Test

The cyclic oxidation experiments were conducted within a high-temperature tubular furnace. The specimens were individually held in alumina crucibles during the course of the tests, and the oxidation cycle was 12 h, 24 h, and 36 h until the predetermined oxidation time was reached. The mass gain of the coated samples was then determined using an analytical balance (PTX-FA210, ±0.1 mg, OTF-1200X Tube Furnace, Hefei Kejing Material Technology Co., Ltd., Hefei, China). Three parallel samples were set in each group, and the final result was the average value of the measured data. The mass change per unit area of the sample was calculated by the Formula (1) and characterized the high oxidation resistance of the coating.
Δ m S = m m 0 S
In which Δm (mg) is the change in the specimen weight, and S (cm2) is the surface area.

3. Results and Discussion

3.1. Microstructure of the Y2O3-CeO2 Co-Modified Silicide Coating

Figure 2 illustrates the XRD pattern of a Y2O3-CeO2 co-modified coating with varying Y2O3 amounts. The prominent phases detected in the coating are MoSi2 and MoB. However, due to the limited Y2O3 and CeO2 doping, the XRD patterns do not show diffraction peaks of Y and Ce. Post-co-modification, the intensity of MoSi2 and MoB diffraction peaks was notably higher compared to solely CeO2-modified samples. With increasing Y2O3 content, the MoSi2 diffraction peaks initially rose around 40 degrees and then gradually declined. The peak intensity peaks at 1.5 wt.% Y2O3, indicating that an optimal Y2O3 content had a more pronounced effect on promoting MoSi2 crystallization. This enhancement was attributed to Y2O3 acting as nucleating agents, fostering MoSi2 and MoB crystal growth [33]. Additionally, as Y2O3 content increases within a specific range, the half-width of the MoSi2 diffraction peak gradually widens. According to the Debye–Scherrer Formula (2):
D = K γ B cos θ
In which D is the grain size, K is the constant, γ is the X-ray wavelength, B is the half peak width of the diffraction peak of the specimen, θ is the diffraction angle. This indicates a reduction in MoSi2 grain size, meaning that Y2O3 and CeO2 accumulation at grain boundaries can impede the growth and refinement of MoSi2 grains [34]. The leftward shift (toward lower angles) of the MoSi2 diffraction peaks with increasing Y2O3 content, particularly noticeable at 40° (as shown in the insert of Figure 2), can be attributed to lattice expansion caused by the incorporation of Y3+ ions into the MoSi2 crystal structure. When Y3+ substitutes for Mo4+ or occupies interstitial sites in the MoSi2 lattice, it introduces tensile stress, leading to lattice expansion [35]. According to Bragg’s Formula (3), the increase in interplanar spacing (d) due to lattice expansion directly leads to a reduction in the diffraction angle (θ), which accounts for the observed leftward shift of the peak.
2 d sin θ = n λ
Figure 3 depicts the cross-sectional morphology of the Y2O3-CeO2 co-modified composite coating, demonstrating a uniform double-layer structure across all samples. The distribution of Mo, Si, and B in the modified coatings was analyzed by EDS line scanning along lines A, B, C, and D, respectively. A detailed summary of the EDS results obtained for the phases identified in the coatings is presented in Table 3. The combined results of the X-ray diffraction (XRD) analysis and the aforementioned tests confirm the presence of MoB phases at points 1 and 4. Points 2 and 3 exhibit an atomic ratio of Mo to Si close to 1:2, indicating a bilayer structure in the composite coating with an outer layer of MoSi2 and an inner layer of light grey MoB. These findings align with the outcomes documented in Wang’s research [25]. As shown in Figure 4, the thickness of the MoSi2 layer and the MoB layer at 0 wt.%, 0.75 wt.%, and 1.5 wt.% Y2O3 doping amounts are 53.515 μm and 9.584 μm, 56.372 μm and 11.849 μm, and 58.691 μm and 15.834 μm, respectively. The thickness of each layer was observed to increase in proportion to the quantity of Y2O3 present, demonstrating a progressive enhancement of the catalytic effect. Previous studies [31] have demonstrated a significant difference in catalytic effects between CeO2 and Y2O3. The reactivity of Si and B atoms near the substrate is enhanced by CeO2, leading to an increase in the number of Si and B atoms participating in the reaction, and in the thickness of the thickness of MoSi2 and MoB layers [36]. On the other hand, Y2O3 tends to accumulate at grain boundaries, vacancies, and defects, causing lattice distortion and creating a “gas group” structure that facilitates diffusion channels for activated Si and B atoms, promoting their diffusion to the substrate. The growth of MoSi2 and MoB grains is further stimulated by the combined use of Y2O3 and CeO2, ultimately resulting in an increase in the coating thickness. When the proportion of Y2O3 exceeds 3.00 wt.%, the thickness of the MoSi2 and MoB layers decreased to 48.813 μm and 11.014 μm, respectively. This finding suggested that an excess of Y2O3 may facilitate the accumulation of numerous active atoms at the grain boundary, which could potentially impede the growth of the composite coating [31]. Furthermore, Figure 3e illustrates the elemental distribution of Y and Ce, respectively. It can be observed that both Ce and Y are distributed uniformly across all layers of the coating.
Upon augmenting the Y2O3 proportion to 1.50 wt.%, a homogenous and compact structure was exhibited by the Y2O3-CeO2 co-modified composite coating. This occurred because large, rare earth (RE) atoms located at grain boundaries or defects could function as sinks for holes, leading to the elimination of a significant number of holes and consequently inhibiting the formation of holes [37]. However, a further increase in Y2O3 content to 3.00 wt.% led to the appearance of holes within the MoSi2 layer of the composite coating. These holes were attributed to the inward diffusion of Si atoms in the MoSi2 layer facilitated, causing vacancies at grain boundaries and phase boundaries. The accumulation of vacancies eventually leads to the formation of holes during the outward diffusion process [38]. Excessive Y2O3 doping resulted in a significant mismatch in diffusion rates between Y3+ and Mo4+, which led to the development of compositional segregation zones within the coating that accumulated over time and ultimately evolved into holes [37]. Additionally, excess Y3+ ions induced pronounced segregation at grain boundaries, accompanied by severe embrittlement [37]. The weakened grain boundaries acted as preferential sites for crack initiation, further promoting hole formation. It can be inferred that with an addition of 1.0 wt.% CeO2 and 1.5 wt.% Y2O3, the modified composite coating exhibits a compact, hole-free structure with the greatest thickness, consisting of parallel MoSi2 and MoB layers evenly distributed on the substrate.
The incorporation of doped Y2O3 had no impact on the growth mechanism of Mo. The MoB was observed to be distributed in parallel stripes (Figure 3), confirming that its production was facilitated by the inward diffusion of B atoms and their interaction with Mo, rather than by the epitaxial growth of Mo [39]. A strong bond between the metallurgical layer and the substrate resulted from this formation process, effectively reducing the risk of cracking under low-stress conditions. Additionally, the MoB layer acted as a barrier, preventing the diffusion of Si atoms from the MoSi2 layer to the substrate during oxidation. The degradation of the MoSi2 coating was minimized and its lifespan was prolonged by this barrier function [22]. The presence of diffuse light grey areas within the dark grey MoSi2 layer is evident in Figure 3a–d. This is further supported by the quantitative analysis results at points 5 and 6, where the Mo: B ratio is approximately 1:1, thereby confirming that the light grey phase corresponds to the MoB phase. Zang et al. [28] showed that the reaction of B with MoSi2 can produce the MoB phase. The formation of MoB precipitates within the MoSi2 layer is a consequence of the kinetic limitations imposed by the high concentration of B in MoSi2, which drives the reaction (4).
B + M o S i 2 = M o B + 2 S i

3.2. High-Temperature Oxidation of the Y2O3-CeO2 Co-Modified Coatings

The XRD patterns of the Y2O3-CeO2 co-modified composite coatings after oxidation at 1150 °C for 255 h are displayed in Figure 5. The main phases identified in the coating after oxidation included SiO2, Mo5Si3, MoSi2, and B2O3. The formation of SiO2 was attributed to the oxidation of MoSi2, and the formation of B2O3 was attributed to the outward diffusion and oxidation of B within the Mo-B compound phase within the coating structure [40]. Upon increasing the Y2O3 content by 1.5 wt.%, the peak intensities of SiO2 and B2O3 diffraction peaks also increase, suggesting that the co-modification of Y2O3 and CeO2 facilitated the formation of a SiO2 protective film. However, with a further increase in Y2O3 content to 3.00 wt.%, the peak intensities of SiO2 and MoSi2 diffraction peaks decreased, indicating a reduction in antioxidant capacity.
The cross-sectional morphology of various modified composite coatings following oxidation at 1150 °C for 255 h was displayed in Figure 6. Quantitative analysis is conducted on different regions, and the elemental composition is presented in Table 4. Based on the elemental composition at points a, b, c, d, e, and f, the main phases in the respective regions can be determined through atomic ratio calculations as SiO2, MoSi2, Mo5Si3, MoB, Mo5Si3, and Mo5Si3. During high-temperature oxidation, the Mo5Si3 layer was formed due to the diffusion of the Si element in the MoSi2 layer of the coating into the Mo matrix. Meanwhile, the silicon present on the coating surface undergoes a chemical reaction with oxygen, resulting in the formation of silicon dioxide (SiO2). The thickness of the SiO2 layer increases to 13.42 μm with 1.50 wt.% Y2O3 and the thickness of the transition Mo5Si3 layer was thinner due to the inhibitory effect of Y2O3 and CeO2 on the inward diffusion of B and Si, resulting in conducive to the formation of SiO2. In particular, Y3+ can fill the gaps in the Si-O bond, creating a new Si-O-Y bond that enhances the density of the SiO2 layer and prevents the inward diffusion of oxygen [41,42]. The thickness of the SiO2 layer decreases as the amount of Y2O3 increased to 3 wt.%. Longitudinal cracks form in the MoSi2 layer, leading to rapid inward diffusion of oxygen from the cracks and consumption of the MoSi2 layer. This was due to the excess of Y3+ ions that could fill the gaps in the Si-O bond at high temperatures, which damaged the bond and created numerous pores that exacerbated the oxidation loss of the Y2O3-CeO2 co-modified coating [41]. In conclusion, the high-temperature oxidation resistance of the coating can be improved by the addition of Y2O3. However, excessive amounts of Y2O3 can ultimately have a detrimental effect on the coating layer.
The mass change curves of the 255 h oxidized composite coatings at 1150 °C are displayed in Figure 7a. The oxidation process of the Y2O3-CeO2 co-modified coating at 1150 °C can be divided into the early rapid oxidation stage and the slow oxidation stage. Notably, with the addition of 0.75 wt.% and 3 wt.% of Y2O3, the coating underwent rapid oxidation in the initial 50 h, resulting in a rapid weight increase. Only linear oxidation was undergone by the modified composite coating, with a minor weight increase of 0.13 mg/cm2 observed in the first 15 h prior to oxidation at a Y2O3 content of 1.50 wt.%. In contrast, at Y2O3 concentrations of 0.75 wt.% and 3.00 wt.%, the modified coating underwent linear oxidation for 35 h prior to oxidation, with the coating weight increasing by 0.42 mg/cm2 and 0.40 mg/cm2, respectively. This was attributed to the synergistic effect of appropriate amounts of Y2O3, which accelerated the formation of a SiO2 protective layer, thereby impeding oxygen diffusion. As shown in Figure 6d, the Mo5Si3 phases present in cracks undergo further oxidation, leading to the generation of MoO3 volatile products. The rapid decay of the coating weight resulted from the interaction of the oxygen released from MoO3 volatilization with Mo5Si3 in the transition layer.
Figure 7b shows the square of the weight gain per unit area (Δm/S)2 as a function of oxidation time for composite coating samples at 1150 °C for 105 h. During the experiment, the kinetic curve of the specimen follows a parabolic law after the fitting process, and the parabolic rate constant kP is calculated according to the following equation:
Δ m S 2 = k p t
In which Δm (mg) is the change in the specimen weight, S (cm2) is the surface area, and t (h) is the oxidation time. After oxidation at 1150 °C, the mass gain of the co-modified composite coating with 1.50 wt.% Y2O3 was 0.29 mg/cm2, and it exhibited an oxidation rate constant of 6.68 × 10−4 mg2/(cm4·h) for 105 h. This rate constant was lower than that of other modified composite coatings with varying Y2O3 content and significantly lower than the 1.00 wt.% CeO2-doped coating, which had a weight gain of 0.41 mg/cm2 and an oxidation rate constant of 1.70 × 10−3 mg2/(cm4·h). These results indicate that the co-modified composite coatings with 1.50 wt.% Y2O3 and 1.00 wt.% CeO2 demonstrates superior high-temperature oxidation resistance. This finding was supported by the analysis of the post-oxidation morphology of Y2O3 and CeO2 co-modified composite coatings in Figure 6.

3.3. Modification Mechanism of Ce and Y in the Coatings

Figure 8 shows the formation process of the Y2O3-CeO2 co-modified coating. During the high-temperature embedding, Si and B particles were activated under the action of the NaF activator. The reaction Equations (6)–(11) occurred in the diffusion of atomic Si and B to Mo substrate to form a composite coating [22].
B s + 2 N a F s B F 2 g + 2 N a g
2 B F 2 g B F 4 g + B g
B g + M o s M o B s
2 S i s + 4 N a F s S i F 4 g + S i g + 4 N a g
2 S i g + M o s M o S i 2 s
2 S i g + M o B s M o S i 2 s + B g
The rare earth oxides doped in the penetrant can promote the infiltration of Si and B to a certain extent, but their action mechanisms were significantly different. CeO2 was mainly distributed on the surface of the Mo substrate and promoted the diffusion of Si and B to Mo substrate to form a protective coating (shown in Figure 8 (step 2)) [31]. However, the Y atom (179.7pm) has smaller size than that of a Ce atom (185pm). The radius of Y3+ had a small radius (179.7pm) and significant diffusion rate and tended to aggregate at grain boundaries, vacancies, and other defects, resulting in lattice distortion and “gas group” structure (shown in Figure 8 (gas group structure)). Meanwhile, it can absorb active atoms and promote the diffusion of atoms from the “gas group” into the interior of the coating [31]. Under the synergistic effect of CeO2 and Y2O3, the number of active Si and B atoms increased, and their diffusion rate was also enhanced. During the diffusion of active Si and B atoms, CeO2 was driven to migrate to the interior of the coating so that the coating–substrate interface gradually moved towards the substrate, and the thickness of the coatings gradually increased (shown in Figure 8 (step 2)). The Ce2+ and Y3+ distributed at grain boundaries, vacancies, and other defects act as heterogeneous nucleating agents, reducing the activation energy and promoting the crystal growth of MoSi2. Furthermore, the solute drag effect produced by these agents refines and hinders the growth of MoSi2 grains, thereby enhancing the compactness of the coating microstructure and reducing the incidence of cracks. Therefore, as a consequence of the combined action of CeO2 and Y2O3, a composite coating with a substantial thickness and a compact structure was formed.
Figure 9 illustrates the oxidation process of the Y2O3-CeO2 co-modified coating. During oxidation, MoSi2 reacted with O2 to produce a small amount of SiO2, Mo5Si3, and volatile MoO3. The MoSi2 layer was further diffused into the substrate by the Si atoms to form the Mo5Si3 layer (shown in Figure 9 (1150 °C, step 1)). A complete and dense SiO2 layer was formed on the coating surface, and the MoB layer can inhibit the mutual diffusion of Si and Mo atoms in the MoSi2 layer. The B2O3 produced in the oxidation process can improve the high-temperature fluidity of SiO2 and enhance the self-healing of the SiO2 layer to quickly cover the coating surface and fill in cracks [28]. Meanwhile, the B2O3-SiO2 improved the compactness of the coating [17,43]. The doped Y2O3 can provide a large number of Y3+ to occupy the Si-O bond gap and form a Si-O-Y bond, thus improving the compactness of SiO2 (shown in Figure 9 (1150 °C, step 2)) [41]. The strong absorption can stabilize the distribution of O atoms in SiO2 and inhibit the cracking of the Si-O bond at high temperatures to inhibit the diffusion of O atoms and the consumption of SiO2 [44]. In addition, a pinning effect can be produced by the segregation of CeO2 and Y2O3 at the grain boundary, which hinders the internal diffusion of Si and promotes the external diffusion of Si atoms. On the other hand, the binding of rare earth elements to oxygen vacancies facilitates the formation of defect clusters, enhancing both the binding energy and phase stability of the material [45]. The lattice distortion results from the simultaneous introduction of multiple rare earth elements due to variations in atomic radius. Furthermore, the fluctuations caused by differences in elemental characteristics contribute to the emergence of defects, which subsequently impede the diffusion processes of the components [46,47]. Consequently, the introduction of supplementary doping elements serves to augment the solution entropy within the coating, thereby impairing the spontaneity of chemical reactions as a consequence of the augmented mixing entropy of a solid solution. The synergistic interaction between Y2O3 and CeO2 during the antioxidant process significantly prolongs the service life of antioxidant coatings by promoting lattice distortion and facilitating defect clustering.

4. Conclusions

In this study, Y2O3-CeO2 co-doped composite coatings were prepared on molybdenum substrates using a two-step pack cementation method. The co-doping of Y2O3 and CeO2 in the composite coatings has been shown to enhance the thermal stability and oxidation resistance of the coatings under high-temperature environments. The results indicate that the co-doped composite coating exhibits superior high-temperature oxidation resistance compared to coatings modified with a single dopant. Additionally, the impact of varying Y2O3 content on the microstructure of the composite coating and its high-temperature oxidation behavior has been analyzed. The conclusions are as follows:
(1)
CeO2 and Y2O3 have a synergistic modification effect, which can promote the diffusion of Si and B atoms to the substrate, refine and promote MoSi2 crystal growth, and make the coating more compact. The thickness of the coating is the largest as the additional amount of CeO2 and Y2O3 are 1 wt.% and 1.5 wt.%, respectively. The coating is composed of MoSi2 and MoB layers, which are both distributed parallel to the substrate, and the thickness is 58.691 μm and 15.834 μm, respectively.
(2)
After oxidation, the coating structure from the inside out is the SiO2 layer, Mo5Si3 layer, MoSi2 layer, Mo5Si3, and MoB layer. The thickness of the SiO2 layer increases to 13.42 μm with 1.50 wt.% Y2O3 and the thickness of the transition Mo5Si3 layer was 20.08 μm. The co-modified composite coating with 1.50 wt.% Y2O3 exhibits a mass gain of 0.29 mg/cm2 after 105 h of oxidation at 1150 °C, with an oxidation rate constant of 6.68 × 10−4 mg2/(cm4·h).
(3)
The doped Y2O3 can provide a large number of Y3+ to occupy the Si-O bond gap and form a Si-O-Y bond, thus improving the compactness of SiO2. CeO2 and Y2O3 segregated at the grain boundary can also produce a pinning effect, hinder the internal diffusion of Si, and promote the external diffusion of Si atoms.

Author Contributions

Conceptualization, Y.Z. and M.Z.; methodology, Y.Z.; software, G.Z.; validation, M.Z., Q.L. and Y.Z.; formal analysis, M.Z and G.Z.; investigation, P.F.; resources, Y.Z.; data curation, M.H.; writing—original draft preparation, M.Z.; writing—review and editing, Y.Z.; visualization, M.Z.; supervision, Y.L.; project administration, Y.Z.; funding acquisition, Y.Z. All authors have read and agreed to the published version of the manuscript.

Funding

This work was funded by the Key Research Plan of Shaanxi Province (2023-YBGY-465, 2020GY-278, 2020ZDLGY12-07), the Special Fund for Basic Scientific Research of Central Colleges, China (300102312407).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

Authors Yong Zhang and Pengfa Feng were employed by the company Jinduicheng Molybdenum Co., Ltd. The remaining authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

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Figure 1. Schematic diagram of coating preparation.
Figure 1. Schematic diagram of coating preparation.
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Figure 2. XRD pattern of Y2O3-CeO2 co-modified coating with different amounts of Y2O3.
Figure 2. XRD pattern of Y2O3-CeO2 co-modified coating with different amounts of Y2O3.
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Figure 3. Cross-sectional morphology of the Y2O3-CeO2 co-modified composite coating with different amounts of Y2O3 (a) 0.10CeO2–0Y2O3, (b) 0.10CeO2–0.75Y2O3, (c) 0.10CeO2–0Y2O3, (d) 0.10CeO2–3Y2O3, (e) EDS maps scanning results of (c).
Figure 3. Cross-sectional morphology of the Y2O3-CeO2 co-modified composite coating with different amounts of Y2O3 (a) 0.10CeO2–0Y2O3, (b) 0.10CeO2–0.75Y2O3, (c) 0.10CeO2–0Y2O3, (d) 0.10CeO2–3Y2O3, (e) EDS maps scanning results of (c).
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Figure 4. Thickness of the co-modified coating with different amounts of Y2O3.
Figure 4. Thickness of the co-modified coating with different amounts of Y2O3.
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Figure 5. XRD patterns of Y2O3-CeO2 co-modified coating after oxidation for 255 h at 1150 °C.
Figure 5. XRD patterns of Y2O3-CeO2 co-modified coating after oxidation for 255 h at 1150 °C.
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Figure 6. The cross-section morphology of Y2O3-CeO2 co-modified coating with different amounts of Y2O3 after 255 h oxidation at 1150 °C: (a) 0.10CeO2–0Y2O3, (b) 0.10CeO2–0.75Y2O3, (c) 0.10CeO2–1.50Y2O3, and (d) 0.10CeO2–3.00Y2O3.
Figure 6. The cross-section morphology of Y2O3-CeO2 co-modified coating with different amounts of Y2O3 after 255 h oxidation at 1150 °C: (a) 0.10CeO2–0Y2O3, (b) 0.10CeO2–0.75Y2O3, (c) 0.10CeO2–1.50Y2O3, and (d) 0.10CeO2–3.00Y2O3.
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Figure 7. Oxidation result of co-modified coating with different amounts of Y2O3. (a) Oxidation weight gain, (b) oxidation kinetics behavior in the first 105 h.
Figure 7. Oxidation result of co-modified coating with different amounts of Y2O3. (a) Oxidation weight gain, (b) oxidation kinetics behavior in the first 105 h.
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Figure 8. Formation process of Y2O3-CeO2 co-modified coating.
Figure 8. Formation process of Y2O3-CeO2 co-modified coating.
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Figure 9. Oxidation process of Y2O3-CeO2 co-modified coating.
Figure 9. Oxidation process of Y2O3-CeO2 co-modified coating.
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Table 1. Chemical composition of molybdenum substrate/%.
Table 1. Chemical composition of molybdenum substrate/%.
MoFeNiOCSiNCaMg
Balance0.00310.0010.0030.0030.0030.0010.00050.0003
Table 2. Composition and content of embedding agent.
Table 2. Composition and content of embedding agent.
Process StepsSamplePack Mixtures (wt.%)
BNaFAl2O3SiSiO2CeO2Y2O3
First boronizingBoronizing agent4591----
Second Si-Ce-Y depositingSiliconizing agent-10.55-2073.510
Siliconizing agent-20.55-2072.7510.75
Siliconizing agent-30.55-207211.5
Siliconizing agent-40.55-2070.513
Table 3. The elemental composition at different points in Figure 3.
Table 3. The elemental composition at different points in Figure 3.
SpotComposition/at.%Main Phase
MoSiB-
154.40.145.4MoB
234.565.2-MoSi2
332.367.6-MoSi2
453.60.246.2MoB
554.40.145.4MoB
654.20.145.67MoB
Table 4. The elemental composition at different points in Figure 6.
Table 4. The elemental composition at different points in Figure 6.
SpotComposition/at.%Main Phase
MoSiOB-
a1.232.760.40.7SiO2
b62.036.7-0.3Mo5Si3
c34.565.3-0.2MoSi2
d63.436.5-0.1Mo5Si3
e53.41.3-44.3MoB
f60.438.80.8-Mo5Si3
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Zhang, Y.; Zhang, M.; Zhang, G.; Liu, Q.; Huang, M.; Lan, Y.; Feng, P. Microstructure and Antioxidative Performance of Y2O3-CeO2 Co-Modified Molybdenum Silicide Coatings. Coatings 2025, 15, 310. https://doi.org/10.3390/coatings15030310

AMA Style

Zhang Y, Zhang M, Zhang G, Liu Q, Huang M, Lan Y, Feng P. Microstructure and Antioxidative Performance of Y2O3-CeO2 Co-Modified Molybdenum Silicide Coatings. Coatings. 2025; 15(3):310. https://doi.org/10.3390/coatings15030310

Chicago/Turabian Style

Zhang, Yong, Minglong Zhang, Gengfei Zhang, Qiaoyun Liu, Meilin Huang, Yongqiang Lan, and Pengfa Feng. 2025. "Microstructure and Antioxidative Performance of Y2O3-CeO2 Co-Modified Molybdenum Silicide Coatings" Coatings 15, no. 3: 310. https://doi.org/10.3390/coatings15030310

APA Style

Zhang, Y., Zhang, M., Zhang, G., Liu, Q., Huang, M., Lan, Y., & Feng, P. (2025). Microstructure and Antioxidative Performance of Y2O3-CeO2 Co-Modified Molybdenum Silicide Coatings. Coatings, 15(3), 310. https://doi.org/10.3390/coatings15030310

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