1. Introduction
With the advancement of industrial technology, optimizing the surface properties of metal materials has remained a crucial research focus, particularly in enhancing material hardness, wear resistance, and corrosion resistance through surface treatment methods. Plasma spraying technology, as an advanced surface treatment technique, holds significant importance in industrial applications [
1]. This method utilizes high-temperature plasma arc flame streams to melt coating materials, which are then ejected onto substrate surfaces under high-speed airflow to form specialized coatings. Due to its efficiency, process stability, and broad material applicability, plasma spraying has been widely adopted in aerospace, automotive manufacturing, and energy chemical industries. It can produce various coatings including metal coatings, metal-ceramic coatings, and ceramic coatings [
2,
3,
4], with Al
2O
3-based coatings demonstrating exceptional corrosion resistance and wear durability, making them extensively used. However, the poor fluidity of molten droplets during Al
2O
3 preparation leads to surface defects such as microcracks, pores, and streaks that significantly impact coating performance. The classic composite ceramic coating Al
2O
3-3% TiO
2 (AT3) [
5] reduces alumina melting point and porosity through TiO
2 addition. The formation of minor intermetallic compounds during AT3 preparation also improves coating properties. Nevertheless, AT3 coatings exhibit low toughness and high brittleness, making them prone to damage and limiting their application in high-strength, high-impact environments.
To overcome these limitations, researchers have attempted to introduce metal phases into Al
2O
3-coated materials to optimize their performance. Zhu, H.Q. et al. [
6] developed Cu-Ni-Al
2O
3 composite coatings with varying Ni content on AZ91D magnesium alloy substrates using low-pressure cold spray technology. Their analysis of microstructure, morphology, and mechanical properties demonstrated that controlled Ni content effectively reduced porosity while enhancing deposition efficiency, bonding strength, and wear resistance. Liu, X.Y. et al. [
7] created Ni-Zn-Al
2O
3 composite coatings with different zinc concentrations through the same method. The Zn powder content initially reduced pore size before increasing it, with optimal mechanical properties achieved at 14% zinc mass fraction. Sun, Y.H. et al. [
8] implemented laser cladding to produce high-hardness, corrosion-resistant Ni-x%Al
2O
3 composites on 304 stainless steel. Their study revealed that Al
2O
3 content significantly influenced coating morphology, microhardness, and corrosion resistance. The composite formed a tight metallurgical bond with the substrate, exhibiting microstructures progressing from surface to core: equiaxed grains, oriented columnar crystals, and acicular crystals. Notably, microhardness increased initially but decreased with higher Al
2O
3 content, while weight-dependent corrosion rate first decreased then increased, corrosion potential rose initially but later declined, and current density decreased initially before rebounding.
Experimental studies by the aforementioned scholars demonstrate that adding metallic phases can enhance the plastic deformation capability of ceramic coatings. These metallic phases not only fill pores in the coating to improve density but also strengthen the coating’s toughness and bonding strength with the substrate. Among various effective metallic phase additives, aluminum (Al) stands out as an ideal choice for metal-ceramic composite coatings due to its lightweight and active properties, which provide excellent plastic deformation capacity and oxidation resistance. Wang, Q.Q. et al. [
9] developed Al-Al
2O
3 composite coatings with varying aluminum content using atmospheric plasma spraying technology, systematically investigating the effects of aluminum content on coating microstructure, mechanical properties, wear resistance, and corrosion resistance. Results showed that increasing aluminum content from 5% to 30% gradually reduced coating hardness while enhancing fracture toughness. Wear resistance initially improved but later declined, whereas corrosion resistance first increased and then decreased with higher aluminum content. Wang, C.H. et al. [
10] fabricated Al/Al
2O
3 composite coatings via flame spraying, revealing that pore volume increased with Al
2O
3 powder content. The coating with 15% Al
2O
3 mass fraction exhibited the lowest porosity, while polarization curves indicated that coatings with 20% Al
2O
3 mass fraction demonstrated optimal corrosion resistance. These findings are consistent with previous studies on metal-ceramic coatings, such as Ren et al. [
11], who also observed similar microstructural improvements in Al-Al
2O
3 coatings prepared by supersonic plasma spraying. However, our study further elucidates the role of Al content in mediating the transition from brittle to ductile fracture modes. Their study investigated the effects of Al
2O
3 particle loading on microstructure, porosity, electrochemical performance, and salt spray corrosion resistance. The results revealed wavy surface patterns with tightly bonded internal structures. The 70% Al
2O
3 coating exhibited the highest porosity (6.71%), while 70% Al
2O
3 coatings showed minimal corrosion and demonstrated optimal anti-corrosion properties. Wang, K. [
12] and collaborators created high-performance 7075Al/Al
2O
3 composite layers by incorporating large-sized Al
2O
3 spherical particles into 7075Al powder. Their research demonstrated that increased Al
2O
3 particle content enhanced plastic deformation during cold spraying, improved interparticle bonding, and reduced pore formation defects.
In summary, the introduction of pure Al phases can modify the microstructure, hardness, and wear resistance of ceramic coatings, thereby enhancing their overall performance. This has a positive impact on the application scope of Al2O3 ceramic coatings. However, previous studies have paid insufficient attention to how the incorporation of pure Al phases affects the microstructure of coatings and the formation mechanisms between coatings. To address this gap, this paper employs plasma spraying technology to fabricate Al2O3-3%TiO2-xAl (x = 0, 20, 40, 60 wt.%) composite coatings on Q235 base materials. The study focuses on analyzing the effects of pure Al phase incorporation on the microstructure and fundamental properties of the coatings, providing theoretical foundations and technical support for optimizing the performance of plasma-sprayed coatings.
3. Experimental Results and Analysis
3.1. Surface Morphology Analysis of Coating
Figure 1 shows the surface microstructure of the AT3-X% Al coating. The macroscopic morphology exhibits characteristic lamellar distribution patterns, which are formed when powder particles are heated to a molten state during plasma spraying and rapidly solidify upon impact with the substrate surface under high-speed airflow [
15]. Macroscopic observation reveals a coexistence of fully melted zones and partially fused regions in the coating, a phenomenon closely related to powder particle size, nozzle power parameters, and spatial distribution of powders within the spray gas flow.
Figure 1a shows the surface morphology of the AT3 coating. The coating exhibits numerous granular aggregates, representing typical partially fused zones with higher porosity. During plasma spraying, when molten alumina particles contact the substrate surface and rapidly cool, the resulting thin and brittle cooling layer is prone to cracking and spatter. This spatter pattern is commonly observed in high-melting-point materials such as metal oxides and alloys.
Figure 1b–d shows the morphology of the coating after increasing the Al content. When a part of Al is added to the coating, the partial melting zone is significantly reduced. At this time, during the spraying process, the melting point of the sprayed powder is significantly reduced, forming Al-coated AT3 molten droplets.
During the coating formation process, the observed sputtering morphology primarily results from the cooling of larger droplets. When molten droplets are subjected to the spray gun’s airflow on the substrate surface, they transition from spherical to flattened or oval shapes. When the applied force exceeds the surface tension of the droplet, it breaks into smaller droplets. This sputtering pattern predominantly occurs in low-melting-point soft materials such as aluminum (Al) and chromium (Cr). Notably, as the aluminum content increases, both the particle size and quantity of sputtered particles shown in
Figure 1 show significant reduction.
The introduction of pure Al phases significantly alters the microstructure of the coating, exhibiting a bimodal distribution characterized by both classical flake-like and sputtered structures. Concurrently, as Al content increases, the coating surface color transitions from gray-black to gray-white. These structural features and color changes primarily result from differences in surface tension and solidification rates between molten Al2O3 and Al, which create distinct microstructures under spray gun airflow. Additionally, insufficient melt contraction during solidification generates localized tensile stress between particles. When this tensile stress exceeds the material’s fracture strength, microcrack defects form within the coating. This phenomenon is particularly pronounced in aluminum-based coatings, where the incorporation of pure Al phases substantially reduces the likelihood of crack formation.
Figure 2 shows the SEM image of the coating surface and elemental distribution patterns. The plasma spray-coated layer exhibits an uneven surface due to airflow impact, sputtering, and molten droplet spreading. During EDS electron bombardment, charge accumulation in depressions hinders electron escape, resulting in weak secondary electron signals that obscure elemental analysis [
16]. Consequently, the elemental distribution maps display completely black areas primarily located in depressions, which are not impurities but rather material components.
As the Al content in the spray powder is gradually added, the proportion of Al elements in the coating increases while the O content decreases. SEM image analysis reveals that the surface layers predominantly consist of Al2O3 phases, whereas the wavy patterns mainly form pure Al structures. This phenomenon arises from the differing melting points and solidification shrinkage rates of Al and Al2O3. During spraying, under airflow action, Al particles disperse before solidification, resulting in wavy patterns. In the formation of AT coatings, titanium elements coexist with oxygen but concentrate in coating defects such as pores and sputtered particle edges. With increasing Al content in the coating, titanium content decreases progressively, thereby reducing its impact on coating performance.
3.2. Cross-Sectional Morphology Analysis of Coating
Figure 3 presents the cross-sectional image and elemental distribution of the AT3-X% Al coating. The results demonstrate that coatings with varying aluminum content all exhibit the characteristic lamellar structure typical of thermal spray coatings. Under identical spraying conditions, the coating thickness decreases as aluminum content increases, which stems from two primary mechanisms: First, higher aluminum content causes excessive heating of powder at the spray gun’s feeding nozzle, leading to reduced fluidity and decreased powder feed rate. Second, when aluminum content exceeds 40% in the powder, rapid agglomeration and coagulation of aluminum particles occurs within the spray gun’s molten arc. These aggregated particles form solidified chunks before reaching the substrate, resulting in detachment from the spray gun beam and ultimately thinning the coating.
When pure aluminum phase is incorporated into the coating, the layered structure undergoes subtle transformations. The original elongated strip-like morphology becomes slender and elongated, with a marked reduction in pores and defects in the underlying coating. This occurs because during the coating preparation process, molten Al2O3 droplets contact the cooler substrate, rapidly solidifying an outer cooling layer while maintaining a semi-solid or softened interior. Subsequent droplet impacts cause plastic deformation in the partially cooled interior, forming elongated strip-like lamellar structures. The addition of pure aluminum phase results in a lower layer with slender elongated strips and an upper layer exhibiting thickened lamellar morphology. The lower layer demonstrates optimized coating performance and reduced defects due to the pure aluminum phase. Meanwhile, the upper layer achieves a naturally spherical structure through spontaneous slow cooling after the spraying process, free from subsequent particle bombardment or pressure effects.
The elemental distribution analysis indicates that as Al content increases, green bright regions (Al elements) become more abundant and uniformly distributed, while internal black voids (defects like pores and cavities) gradually diminish with fewer cracks appearing. Simultaneously, red areas (O elements) disintegrate into smaller regions, which correlates with reduced Al2O3 content. The reduction in coating defects after increased Al content stems from two mechanisms: During spraying, high-temperature spray guns melt powder into molten droplets, forming Al-coated Al2O3 droplets. Since molten Al exhibits superior fluidity and thermal conductivity compared to Al2O3, these droplets deposit into more homogeneous structures. Additionally, slight oxidation between molten droplets and ambient oxygen improves elemental distribution uniformity while reducing coating defects. Yellow areas (Ti elements) exhibit band-like distributions at coating striations and pores, positively contributing to lowering the porosity of AT3 coatings. However, with increased Al content, defects in the coating significantly decrease, while Ti element proportions diminish markedly, predominantly appearing as dot-like dispersion across different coating regions.
3.3. XRD Analysis of Coating
Figure 4 shows the XRD patterns of AT3 composite coatings with Al content levels of 0%, 20%, 40%, and 60%. The XRD analysis reveals distinct differences between the pure AT3 curve and the three Al-containing curves. As pure Al phases are introduced, the number of peaks significantly decreases, the curves become smoother, and the intensity of the main peak markedly diminishes. The three Al-containing curves exhibit nearly identical peak positions and intensities, each displaying three strong diffraction peaks at 38.6°, 44.8°, and 65.2° corresponding to the pure Al phase. The primary phases consist of pure Al and α-Al
2O
3 phases, with minor amounts of TiO
2 and γ-Al
2O
3 phases present.
The XRD pattern reveals two characteristic peaks in the coating: α-Al
2O
3 (stable state) and γ-Al
2O
3 (unstable state). The stable α-Al
2O
3 originates from the original powder, determined by its grain boundary structure. This structure features oxygen ions arranged in a close-packed hexagonal lattice, with aluminum atoms filling the octahedral voids, resulting in a high melting point that resists melting [
17].
When spraying high-alumina powder, reduced spraying power causes changes in the spray gun’s central temperature. The lowered flame temperature becomes insufficient to complete the conversion from γ-Al
2O
3 to α-Al
2O
3 phases. This results in noticeable γ-Al
2O
3 phase formation within the coating after adding pure aluminum phase. Additionally, the excellent thermal conductivity of pure aluminum enables rapid temperature reduction. The molten α-Al
2O
3 phase contacts the cooler aluminum or substrate, leading to accelerated cooling and non-equilibrium solid-state transformation that generates γ-Al
2O
3 phase. Due to its lower critical free energy, γ-Al
2O
3 undergoes faster nucleation during spraying [
18,
19], resulting in partial γ-Al
2O
3 phase formation in the coating. Al
2TiO
5 phase appears in pure AT3 coatings. As the aluminum content increases, the intensity of Al
2TiO
5 diffraction peaks decreases significantly, which correlates with reduced TiO
2 content in the powder.
3.4. Analysis of Friction and Wear Behavior of AT3 Coatings with Different Al Contents
Figure 5 shows the friction coefficient versus time curves of coatings with varying aluminum content under a 10 N load. The results indicate that the pure AT3 coating exhibits the lowest friction coefficient, which initially rises from 0 to 260 s before stabilizing without significant fluctuations. Coatings containing 20% and 40% aluminum show comparable friction coefficients, but the 40% aluminum coating demonstrates dramatic fluctuations throughout the experiment, failing to reach a stable state until completion. In contrast, the 20% aluminum coating maintains a relatively smooth trajectory. The 60% aluminum coating exhibits an initial rise followed by a decline, attributed to aluminum agglomeration that creates uneven surface irregularities. These high-aluminum regions exhibit poor wear resistance, resulting in higher friction coefficients. When these protrusions are worn away, the coating becomes smoother and the coefficient decreases, explaining the observed rise-and-fall pattern. As pure aluminum content increases, the friction coefficient rises significantly, with the 60% aluminum coating reaching a peak of 0.659 while the AT3 coating remains the lowest at 0.418.
By analyzing the results in
Figure 5 and
Figure 6 alongside the friction coefficient curves, it is evident that the pure AT3 coating, due to its high material hardness and superior wear resistance, showed no surface scratches. The coating only exhibited flake-like surface wear forming bright areas. As the proportion of pure Al phase increased, surface abrasions became more pronounced with widened grooves. While scratch edges developed partial convex patterns, fewer holes appeared at these marks, fewer strip-shaped plow grooves remained, and the coating base gradually became smoother. The 60% Al content coating demonstrated particularly neat grooves with minimal convexity. Notably, adhesive wear was observed on 60% Al scratches, where removed pure Al particles adhered to the grinding balls and migrated with mechanical movement. In contrast, 20% and 40% Al coatings exhibited uneven surface irregularities. The visible scratches on the coating surface indicate significantly reduced wear resistance from added Al phases, consistent with observed changes in hardness and friction coefficients. The groove-like surface features with distinct undulations originate from incompletely melted particles or excessive agglomerates (Al
2O
3 particles) during spray deposition. These hard, poorly fused components detach from the coating surface under grinding ball pressure, creating characteristic grooves.
Generally, Al
2O
3 has high inherent hardness. When pure aluminum is added to the coating, the overall hardness of the coating significantly decreases, and its friction coefficient also drops accordingly [
20,
21]. However, experimental results show that the friction coefficients of coatings containing 20% aluminum are comparable to those with 40% aluminum, and the surface wear morphology remains relatively similar.
Figure 7 isScratch edge morphology of coatings with different aluminum contents. The performance differences in coatings with varying aluminum content in sliding friction tests are closely related to their composition, phase structure, and defects. Coatings with 20% aluminum content contain more Al
2O
3 particles, exhibiting high hardness, excellent wear resistance, low friction coefficients, and stable fluctuations. During friction, Al
2O
3 particles may emerge or be driven out, causing surface cavities and irregularities. In 40% aluminum-content coatings, the ratio of pure aluminum phase to Al
2O
3 is approximately 1:1, with both phases diffusely distributed. During wear, alternating contact between the soft pure aluminum phase and hard Al
2O
3 phase causes continuous fluctuations in the friction coefficient. Coatings with high γ-Al
2O
3 content show significant differences in hardness and support force compared to pure aluminum, resulting in numerous groove defects and large fluctuations in the friction coefficient curve. Coatings with 60% aluminum content contain the most pure aluminum phase, exhibit the lowest porosity and hardness. High aluminum content leads to adhesive friction during operation. The pure aluminum phase envelops Al
2O
3 phases, causing aluminum adhesion to the grinding ball surface during friction. This forms an adhesive friction morphology, and repeated friction between the grinding ball causes Al
2O
3 phases to adhere and detach, leading to noticeable initial fluctuations in the friction coefficient.
Figure 8 presents wear data for coatings with varying aluminum content under a 10 N load for 30 min. The results show that pure AT3 specimens exhibited the least wear, while specimens containing 60% aluminum demonstrated the highest wear, significantly exceeding other groups. Error bars representing standard deviation (
n = 3) are included in
Figure 8. This discrepancy likely correlates with adhesive wear mechanisms [
22,
23]. As aluminum content increased, wear rates progressively rose, indicating that pure aluminum phase exhibits poor wear resistance. The addition of aluminum substantially reduces the coating’s wear performance.
3.5. Cross-Sectional Analysis of AT3 Coatings with Different Al Contents
Figure 9 shows the macroscopic morphology of the coating fracture. The pure AT3 coating fracture showed no impurity particles but exhibited elliptical pores and distinct cracks. These pores formed during the coating spraying process when molten droplets rapidly contracted, creating enclosed cavities that developed into elliptical voids during fracture propagation. Additionally, unmelted particles detached from the coating surface under external forces, also forming elliptical voids. The 20% aluminum content coating showed significantly fewer pores and no visible cracks, though minor pits at the fracture site likely resulted from partially melted particles. As aluminum content increased further, various particle types emerged in the coating: two primary forms were identified-non-conductive bright-side Al
2O
3 and dark-side pure aluminum phases. The bright-side particles markedly decreased at fracture surfaces, with both pore formation and crack probability being substantially reduced. Minor tear ridges appeared at fracture locations, particularly evident in 20% aluminum content coatings.
Figure 10 shows the high-magnification morphology of the fracture surface. The four coatings exhibit distinct trapezoidal, spherical, and irregular regions under high magnification. The AT3 coating demonstrates the largest trapezoidal area, containing stepped or spherical crystal planes formed by brittle fracture of its layered structure under mechanical stress. The prominent spherical regions originate from internal pores and coarse strip-like defects within the coating.
As the proportion of pure aluminum phase increases, the area of trapezoidal zones caused by brittle fracture formation decreases significantly. In coatings containing 60% aluminum content, trapezoidal zones become nearly undetectable. The spherical zone at fracture surfaces gradually diminishes while irregular zones progressively expand. Therefore, incorporating pure aluminum phase can enhance coating toughness, mitigate excessive brittleness issues, and effectively prevent detachment or fracture during service.