Abrasive Research Articles

Microstructures, Properties, and Wear Mechanism of Binderless WC-ZrO2 Cemented Carbide

High-performance binderless WC-ZrO2 cemented carbides were prepared via spark plasma sintering. Subsequently, the microstructure and properties of carbides with varying ZrO2 contents were investigated, focusing on their friction wear performance and wear mechanisms under different loads (40, 60, and 80 N) with Si3N4 as the counterbody material. The results indicated that the WC-10 wt% ZrO2 alloy exhibited optimal overall properties at a sintering temperature of 1650 °C, sintering pressure of 40 MPa, and holding time of 5 min. The relative density, Vickers hardness, and fracture toughness were 99.9%, 2054 HV, and 11.3 MPa·m1/2, respectively. Under an 80 N load, the steady-state friction coefficient decreased from 0.625 for pure WC to 0.326 for WC-10 wt% ZrO2. Further, the wear mechanisms in pure WC included abrasion, adhesion, and oxidation. The steady-state friction coefficients of the WC-10 wt% ZrO2 alloy under different loads ranged from 0.27 to 0.33, and the wear mark width and wear amount increased with an increase in load. Additionally, the wear mechanism changed with increasing load: abrasive wear was observed at 40 N, and a combination of abrasive and adhesive wear was observed at 80 N.

TiC in-situ strengthening mechanism and crack initiation mechanism of SiC/TC4 composite coatings by laser cladding

SiC/TC4 composite coatings were fabricated successfully on the TC4 surface by varying the laser power, and the effect of TiC in-situ strengthening on the microhardness and wear resistance of coatings was investigated. The results show that SiC is continuously decomposed to generate TiC in situ, and α martensite in the coating is refined at 1000 W, with less TiCm. α martensite in the coating is roughened at 1900 W, with the highest content of TiC dominated by dendritic TiCd and petal-like TiCf, longitudinal cracks emerged from the bonding zone and penetrating through the coating. While the appropriate laser power well balanced the relationship between α-martensite and in situ precipitated phases. The C16 coating has the best performance, with an average microhardness 2.1 times higher than that of the substrate (351.8 HV0.2) and a wear rate of 38.1 % of the substrate, respectively. The wear mechanism of the substrate is abrasive, oxidative and fatigue wear, and the wear mechanism of C16 is mainly abrasive wear. The change of the mechanism is due to the fact that TiC particles play the role of skeleton and support in the coating, which are uniformly distributed around α-martensite, thus inhibiting the plastic deformation of the coating.

Study on the fretting wear performance of oxide layer and Cr coating on zirconium alloy in high-temperature water

Grid-to-rod fretting wear is an important factor causing the fuel failure in nuclear power plants. Accident tolerant fuel (ATF) Cr coating and oxide ceramic coating have been developed to improve the fretting wear performance. In this research, two different oxide layers and Cr coating were prepared on zirconium (Zr) alloy, and the fretting wear performance were studied. The morphology, microstructure, tribo-corrosion reaction, and wear characteristics were analyzed. The oxide layer formed at high-temperature pressurized water (HTPW) has the lowest wear rate of 0.11×103 μm3/Nm due to the high hardness and compact structure, which leads to the corresponding friction pairs presenting the highest wear rate of 8.42×103 μm3/Nm. The wear depth of oxide layer formed at HTPW is about 5 times lower than that of as-received Zr alloy, and it is also less than the thickness of oxide layer. The oxide layer formed at HTPW after fretting has a larger thickness than the initial state because the plastic deformation layer caused by shear stress can quickly oxidize to zirconia in high-temperature water, and the wear rate of oxide layer is lower than the formation rate of oxide layer. The wear mechanism of two different oxide layers is delamination and abrasive wear, and that of Cr coating is abrasive wear and fatigue wear.

Impact of Heat Treatment Conditions and Cold Plastic Deformation on Secondary Hardening and Performance of Cold Work Tool Steel X160CrMoV12

In this study, the effect of the cold plastic deformation of a Bridgman anvil at room temperature on the hardness and wear resistance of X160CrMoV12 steel was investigated by utilizing the hardness test, X-ray diffraction (XRD), abrasive emery wear (AEMW) test, optical examination, and scanning electron microscopy (SEM). Three batches of samples were prepared for the experiment: I—as-hardened, II—after hardening with subsequent tempering at 600 °C for 1.5 h, and III— after hardening with subsequent plastic deformation. The hardening of the samples was performed at three temperatures: 1100 °C, 1150 °C, and 1200 °C. The highest content of retained austenite, as much as 69.02%, was observed during hardening at 1200 °C, while 17.36% and 38.14% were formed at lower temperatures, respectively. After tempering (Batch II), the content of residual austenite decreased proportionally by a factor of about seven for each hardening temperature. The effect of plastic deformation (Batch III) is observed, analyzing the hardness of the samples from the surface to the depth, reaching an average hardened depth of 0.08 mm. To evaluate the wear resistance, the surfaces of the three test batches were subjected to an abrasive emery wear test under a 5 N load. Hardened and plastically deformed samples showed higher wear resistance than hardened and tempered samples. The results confirmed that the optimal hardening temperature to achieve the maximum wear resistance of this steel is 1100 °C.

High-temperature tribological evaluation of cobalt-based laser cladded disc for automotive brake systems

This study investigates the high-temperature wear behavior of laser-cladded (LC) cobalt-based Stellite 6 alloy coatings and compares the wear resistance of the cladding layer to the grey cast iron (GCI) substrate material at three different elevated temperatures: 150 °C, 250 °C, and 350 °C. Wear mechanisms at elevated temperatures were analyzed using SEM-EDS and Raman Spectroscopy to understand the material removal processes and degradation for the discs and counterpart composite friction material pins, respectively.The results indicated a significant improvement in wear resistance for cobalt-based alloy cladding at high temperatures. Wear rates were reduced by 5.0 %, 43.0 %, and 16.0 % at 150 °C, 250 °C, and 350 °C, respectively. The LC - brake pin tribo-pair exhibited a continuous increase in friction coefficients (CoF) with an increase in testing temperatures. The wear mechanism for laser-cladded discs exhibited a combination of abrasive and adhesive wear, with abrasive wear prevailing at 150 °C and increased adhesive wear at 250 °C and 350 °C. However, at 350 °C, decomposition of phenolic resin and the adhesive wear mechanism, led to brake pin failure. For GCI discs oxidative wear was identified as the predominant wear mechanism. The improved knowledge of wear mechanisms on LC Stellite 6 against composite brake pins, is set to enhance surface modification of GCI for brake disc applications.

Microstructure and Mechanical Properties of FeCoCrNiAl + WC Composite Coating Formed by Laser Cladding on H13

To enhance high-temperature wear resistance of H13 steel, laser cladding was used to prepare a high-entropy alloy + carbide composite coating. The microstructure and high-temperature wear resistance of the composite coating were systematically analyzed. The results indicate that the FeCoCrNiAl + WC composite coating had a phase structure of BCC + FCC solid solutions, with a small amount of CFe15.1. The microstructure of the composite coating consisted of columnar and equiaxed grains. The microhardness of the FeCoCrNiAl + WC composite coatings was approximately 3.0–3.4 times that of H13. At wear temperatures of 823 K, compared with H13 steel, the wear volumes of composite coatings with different WC contents were reduced by 73.4%–80.2%. Among these, the FeCoCrNiAl + 10% WC composite coating showed the lowest wear volume. Furthermore, when wear temperatures increased from 623 K to 823 K, compared with H13 steel (108.37%), the increase in the wear volume of the FeCoCrNiAl + 10% WC coating was reduced to 90.82%, which indicates the FeCoCrNiAl + 10% WC coating had better high-temperature wear resistance. The wear mechanisms of the composite coating were abrasive and oxidative wear, while H13 steel exhibited abrasive wear, oxidative wear and fatigue wear.

Investigating the microstructure and high-temperature wear resistance of TiAl/WC coating modified via scanning electron beam

In this study, TiAl/WC cladding coatings were modified to improve high-temperature wear resistance by scanning electron beam treatment. Results of the microstructure reveal that the modified coatings are composed of an α2-Ti3Al matrix, with a high density of TiC reinforced phase and Ti3AlC2 MAX phase. At a scanning speed of 6 mm/s, TiAl/WC coating exhibits superior microhardness and high-temperature wear resistance. After the wear test at 800 °C, the minimum wear volume of modified TiAl/WC coating is 0.084 mm3, which is 4.47 times smaller than that of the TC21 substrate. It is mainly attributed to the dense and uniform distribution of hard TiC with a rigid supporting role and Ti3AlC2 MAX phases with a self-lubricating effect. Furthermore, due to the effect of frictional heat, the decomposition of Ti3AlC2 promoted the formation of a dense Al2O3 protective film. The wear mechanism of modified TiAl/WC coatings exhibits a synergistic occurrence of slight adhesive wear, abrasive wear, and oxidative wear. Scanning electron beam technology shows significant potential for extending the service life of the coatings in high-temperature environments.

Effect of laser remelting on microstructure evolution and high-temperature fretting wear resistance in a laser-cladding self-lubricating composite coating on titanium alloy substrate

TC21 titanium alloy possesses the advantage including high strength, low density, and great resistance to damage. Combining it with surface modification technology, it is expected to improve the performance of aviation structural components. This work applied laser remelting technology to realize surface modification, and the hardness and fretting wear properties of the coating were investigated. This research has found that laser remelting technology can effectively refine grain size and improve the performance of coatings. By exploring different laser remelting powers (600 W, 900 W, 1200 W) and the different diameters of laser beam (3 mm, 6 mm), the optimal laser process was obtained with laser power and spot diameter of 600 W and 6 mm, respectively. The average grain size is 2.1 μm. The laser remelting coating has an average microhardness about 980 HV0.2, and it is 2.5 times and 1.3 times higher than the substrate and laser cladding hardness, respectively. A minimum coefficient of friction (COF) about 0.5 was obtained by the laser remelting coating, and the wear rate reaches the lowest of 1.87 × 10−6 mm3/(N·m) at fretting temperature with 500 °C. The abrasive wear and adhesive wear were the main wear mechanisms, and accompanied by oxidative wear. This study provides important reference for improving the performance of high-strength titanium alloy to obtain low defect, high-performance coatings with stable quality.

Effect of heat treatment on wear resistance of cold-sprayed Ti-diamond composite coating

In order to enhance the wear resistance of cold-sprayed Ti coatings, Ti-diamond (Ti-MD) composite coatings were fabricated, followed by heat treatment at different temperatures. The effects of heat treatment temperature on the wear resistance of the composite coatings were assessed using X-ray diffraction (XRD), scanning electron microscopy (SEM), transmission electron microscopy (TEM), microhardness testing, and wear resistance experiments. The results show that the composite coating undergo no phase transformation after heat treatment, and exhibits higher microhardness and improved wear resistance. The porosity results showed that the porosity of the coating decreased as the heat treatment temperature increases. TEM results showed that stable TiC (about 10 nm) was formed at the interface between the titanium and diamond particles after heat treatment at 800 °C, and nanoindentation results showed that the heat-treated coating had higher deformation resistance. Specifically, when the heat-treated temperature rose to 800 °C, the composite coating exhibits an 80 % reduction in wear rate, primarily attributable to the decreased porosity of the coating and the enhanced adhesion between Ti and diamond particles. The wear mechanisms of the heat-treated coatings are predominantly reduced oxidative and abrasive wear.

The investigation of support effect from hard substrate to soft coating of PI/EP-PTFE under different coating thicknesses and frictional contacts

Engine bearings on ships can experience rapid failure under extreme conditions, such as when seawater infiltrates the engine compartment due to collisions with reefs or missile attacks. To enhance the self-lubrication and wear resistance of these bearings, a composite coating consisting of ZrO2-PI/EP-PTFE has been designed. This coating was applied using liquid spraying technology onto the surfaces of A370 aluminum alloy, CuPb22Sn2.5 copper alloy, and 15# carbon steel. Three different coating thicknesses—20 μm, 30 μm, and 40 μm—were applied to each substrate. The tribological properties of these coatings on the three substrates were investigated under both dry sliding wear and seawater corrosion conditions. The results indicated that the tribological performance of the coatings is influenced by factors such as the coating hardness, frictional contacts, and the supporting effect of the substrate. The hardness and elastic modulus of the coatings decreased as the coating thickness increased. A thicker coating results in reduced support from the substrate. The adhesive wear of these coatings under dry sliding wear conditions on the different substrates is also presented. The coefficients of friction (CoFs) of these coatings increased with coating thickness on all three substrates. In contrast, the wear rates decreased as the coating thickness increased. The hardness of the coating was influenced by the support effect of the substrate. The primary factors governing the tribological performance of the coating under dry sliding conditions are the pinch action of the hard grinding ball against the soft coating on the hard substrate and the contact pressure. Abrasive wear, spalling wear, plough grooves, and spalling pits were observed under seawater corrosion conditions. These findings suggest that increased coating thickness is associated with lower coefficients of friction (CoFs) and wear rates. The main contributing factors are seawater corrosion and the scouring effect of high-frequency reciprocating friction.

Exploring the potential of coal derived graphite as next generation lubricant additive for multifunctional applications

In the present study, the friction and wear characteristics of steel/steel contact under reciprocating sliding conditions were investigated using composite mixtures made from Polyalphaolefin 4 (PAO4) as base oil lubricant and North Dakota lignite-derived graphite (LG) as high-value carbon additive. The results show that addition of 1 wt% LG to PAO4 led to a reduction in the friction coefficient and wear volume by ∼15 % and ∼13 %, respectively. In addition, the oxidation induction time (OIT) at 160 °C was increased by ∼29 %, which further indicates good stability of the formulated composite lubricant against oxidative degradation. The primary wear mechanism on AISI 52100 steel flat and counter-body was found to be abrasive wear under high-contact stress reciprocating sliding conditions, where tribo-oxide films of 100–200 nm were observed on the wear tracks of 52100 steel surfaces using focused ion beam scanning transmission electron microscopy (FIB-STEM). Furthermore, cross-sectional analysis of the wear track of AISI 52100 steel revealed that 1 wt% of LG additive reduced the thickness of the sub-surface deformation zone by 44 %, which indicates higher load-bearing capacity and improved wear resistance.

Fabrication of high-performance biomedical rare-earth magnesium alloy-based WE43/hydroxyapatite composites through multi-pass friction stir processing

Magnesium-based composites with bioactive ceramic particles addition are promising materials for biomedical implant applications. Nevertheless, the agglomeration of bioactive ceramic particles remains a challenge for fabricating high-performance biomedical magnesium-based composites. Herein, a novel high-performance biomedical rare-earth magnesium alloy-based WE43/hydroxyapatite (HA) composite is successfully fabricated via multi-pass friction stir processing (MP-FSP). Systematic investigations reveal that MP-FSP leads to a uniform distribution of HA particles and efficient elimination of defects. The microstructural analysis shows a significant grain refinement in the WE43 alloy from 49.4 μm to 2.4 μm under triple-passes FSP. The mechanical properties of the composite are enhanced significantly under triple-passes FSP, with yield strength, ultimate tensile strength, and elongation reaching 236.2 MPa, 278.6 MPa, and 14.2% respectively. Corrosion resistance is also improved, with a 30% reduction in the corrosion rate in SBF solution compared to the unprocessed alloy. Moreover, the MP-FSP fabricated composites exhibit superior corrosion-wear resistance, characterized by slight abrasive wear compared to the abrasive wear and severe pitting corrosion observed in the base WE43 alloy. These improvements are attributed to the synergistic effects of grain refinement, dispersion strengthening, enhanced interfacial bonding, and texture modification. Overall, these findings provide significant quantitative insights into the advanced fabrication techniques of magnesium-based composites for biomedical implant applications, highlighting the effectiveness of MP-FSP in enhancing both mechanical and corrosion-related properties.

Evolution of fretting wear behavior of zirconium alloy cladding tube under gross slip regime in simulated primary water of pressurized water reactor

The evolution of fretting wear behavior of zirconium alloy cladding tubes mated with dimples under the gross slip regime (GSR) was investigated. The findings revealed that the primary wear mechanisms under GSR were delamination, surface fatigue wear and abrasive wear, and the fretting damage rate mainly depends on delamination. The cross-sectional microstructure of the worn area could be divided into the third-body layer, tribologically transformed structure layer, and general deformation layer, with their formation mechanisms analyzed. Furthermore, the mechanism of wear-induced grain refinement was identified as dynamic recrystallization (DRX), including both continuous DRX and discontinuous DRX. Additionally, the processes of fretting wear and DRX were discussed.

Study on the friction and wear properties of 7075-T6 aluminum alloy enhanced by milling and ultrasonic impact treatment

This study investigates the effects of milling parameters on the surface friction behavior of 7075-T6 aluminum alloy subjected to ultrasonic impact treatment. A three-dimensional milling and friction-wear model was developed using ABAQUS finite element analysis, examining the influence of milling speed, depth, and feed rate on the coefficient of friction, wear volume, and surface morphology through single-factor experiments. Results indicate that milling parameters affect the friction coefficient in the following order: Vc > f > ap. Specifically, increasing milling speed from 35 m/min to 59 m/min raises the average friction coefficient from 0.305 to 0.387, a 26.88 % increase. At a milling speed of 83 m/min, the friction coefficient and wear volume reach their lowest values of 0.305 and 0.977 mm³, respectively. The wear volume decreases with increasing milling speed and feed rate, while milling depth has a minor effect. The most significant reduction in wear volume, from 5.76 mm³ to 0.977 mm³ (an 83.04 % decrease), occurs as milling speed increases from 35 m/min to 83 m/min. Maximum longitudinal slip during the reciprocating motion primarily occurs at the ends, with both positive and negative peak offsets. Surface damage from 304 stainless steel balls against the 7075-T6 alloy involves adhesive and abrasive wear. At a milling depth of 35 μm, friction-induced compounds in the transfer film mainly consist of Al, C, Fe, Zn, Mg, and Cr.

Enhanced wear resistance, corrosion behavior, and thermal management in magnesium alloys with PEO coatings

The harsh conditions encountered in aerospace applications, such as high operational temperatures, abrasive wear, and corrosive substances, present significant challenges to the performance and longevity of magnesium alloy components. To create a coating with superior wear resistance, corrosion resistance, and high emissivity, this study employs plasma electrolytic oxidation (PEO) technology to develop a nanocomposite coating doped with carbon nanotubes (CNTs) and hexagonal boron nitride (h-BN). The results demonstrate that the MgO-BN/CNTs coating with an emissivity of 0.82 reduces the equilibrium temperature of the 5 W LED junction by nearly 10 °C compared to the magnesium alloy substrate, showing improved radiative heat dissipation performance. Due to the ability of the porous structure to accommodate abrasive particles, coupled with the lubricating effect of h-BN and CNTs, the friction coefficient of the MgO-BN/CNTs coating is 0.57, which is 21 % lower than that of the MgO coating. Additionally, the coating exhibits excellent corrosion protection, attributed to the dense microstructure and chemical inertness of h-BN. The findings demonstrate that the strategic incorporation of h-BN and CNTs into PEO coatings effectively improves the wear resistance, corrosion resistance, and thermal management performance of magnesium alloys.

Microstructure and wear behavior of WC-reinforced AlCoCrFeNiSi high entropy alloy coatings prepared by high-velocity arc spraying

In this study, AlCoCrFeNiSi/WC (WC from 0 to 40 wt%) high entropy alloys (HEAs) coatings were deposited on Q235 steel substrates using high-velocity arc spraying technique. The coatings' phases, microstructure, microhardness, nano-hardness, wear properties, and the mechanisms of wear were examined. The results have shown that the WC reinforced HEA had faced-centered cubic, body-centered cubic solid solution and carbide phases, while faced-centered cubic solution and Cr3Si, Al2O3 phase were observed in AlCoCrFeNiSi coating. The coatings possess a dense, lamellar structure and strong adhesion to the substrates. With the addition of reinforced particles, the porosity of the coatings initially decreases and then increases. The average microhardness of the coatings is significantly improved as WC content increased, reaching a maximum of 530 HV0.1. The ratio of nano-hardness to reduced elastic modulus rises as more WC is introduced. The coatings with the WC particles exhibit good wear resistance with the optimum wear rate at WC content of 40 wt%. Under the same conditions, the coating with 40 wt% of WC displayed the lowest wear rate, which decreased by 60.5 % compared to the AlCoCrFeNiSi coating. The AlCoCrFeNiSi coating experienced a mix of adhesive, abrasive, oxidative, and fatigue wear mechanisms. The wear mechanism changed to more abrasive, adhesive, and oxidative in the reinforced coatings. The load-bearing capacity and secondary phase strengthening effects of WC reduce the wear rate of the coatings.

Strengthening of mechanical and tribological properties in CrFeCuMnNi high entropy alloy through dispersion of TiO2 reinforcement via powder metallurgy processes

The present study reports the effect of TiO2 reinforcement on the phase, microstructure, mechanical and tribological properties of CrFeCuMnNi/TiO2 high entropy alloy composites (HEACs) processed by powder metallurgy. The results reveal the formation of single-phase face-centered cubic (FCC) structure after 30 h of milling in the original HEA, while TiO2 peaks in the HEACs indicate uniform distribution. After sintering, multiple phases including FCC, Cr-rich, Cr2O3 were observed. The hardness of HEAs increased from 330±10 to 440±10 HV and compressive yield strength increased from 480 to 760 MPa while scarifying the strain from 43.5 to 21 % with TiO2 content. The addition of TiO2 content slightly reduces the coefficient of friction and specific wear rate decreased by 45.16 % due to increased hardness and formation of stable oxide layer on the worn surface inhibits plastic deformation. The addition of TiO2 reduces the dominance of abrasive and adhesive wear and enhances the strength of HEACs.

Effect of Nb and Ti additions on microstructure, hardness and wear properties of AlCoCrFeNi high-entropy alloy

The use of Nb and Ti in the development of high-performance alloys is strategically important for technological advancement. The effect of Nb and Ti additions on the microstructure, hardness and tribological properties of the High Entropy Alloy (HEA) AlCoCrFeNi was evaluated. The addition of 0.6mol of Nb led to the formation of Laves phase, resulting in a B2/Laves type hypoeutectic microstructure. Conversely, increasing Ti concentration led to the formation of a dendritic microstructure, with interdendritic region composed of Cr-rich BCC-A2 and Fe-Ti rich Laves phase. The average hardness values obtained were 790 HV, 597 HV and 731 HV for AlCoCrFeNiNb0.6, AlCoCrFeNiTi0.5 and AlCoCrFeNiTi1.2 HEAs, respectively. The high hardness was attributed to the formation of the Laves phase and Cr-rich phases, in addition to solid solution hardening, as confirmed by the increase in the lattice parameter calculated by Rietveld refinement method for both B2 and BCC-A2 phases. While the three compositions exhibited comparable friction coefficient, the alloy containing Nb showed superior wear behavior. This was evidenced by the lower volume of material loss and the lower wear rate, which can be attributed to the fine and homogeneous hypoeutectic microstructure observed in the ingot’s cross section. The wear mechanisms were studied, characteristics features of abrasion and adhesion wear were observed.

Weathering effect on the wear performance of epoxy powder coatings reinforced with calcium ion-exchanged amorphous silica

Epoxy coatings generally have poor performance when used for exterior applications. After having studied the corrosion benefits obtained with calcium ion-exchanged amorphous silica pigments, the possible weathering advantages they may provide to powder coatings are analyzed in this work for the first time. For that purpose, five epoxy-based powder coatings were studied: the as-received coating (AR), and four epoxy subjected to a hot mixing process with different amounts by weight of silica anticorrosive micropigments (0 %, 1, 2 and 3 %). All epoxy coatings were degraded by ultraviolet radiation with a xenon lamp for 250 h to determine their weathering resistance. The damage suffered by each coating was evaluated quantifying their FTIR spectra, considering the carbonyls and hydroxyls formed during this type of degradation. Subsequently, studies of plastic universal hardness and abrasive and erosive wear were carried out. The results obtained show that these functionalized coatings have better mechanical and wear performance than the commercial coating after xenon light exposure. This is coherent with the fact that the non-reinforced coatings have the greatest degradation both by hydrolysis and photodegradation. After the weathering process carried out, the 3 % coating proves to have the best abrasive and erosive wear performances. Thus, the calcium ion-exchanged silica particles allow the service life of UV exposed epoxy powder coating to be extended, not only because of their anti-corrosive character but also because of their weathering stabilization properties. These findings represent a significant advancement in improving the durability of epoxy powder coatings for exterior applications.

Investigating on the Tribological Behavior of Binderless WC Matrix Composite

The purpose of this study was to investigate the dry friction and wear behavior of WC-4.3wt.%MgO-2wt.%ZrO2 (WM2Z) composite. WM2Z composite prepared by high-energy ball milling and spark plasma sintering (SPS) technology exhibited excellent comprehensive mechanical properties and dense microstructure. Dry friction test results indicated that the increase of sliding speed will lead to the decrease of friction coefficient, while at the same sliding speed, the extension of sliding time has no significant effect on the friction coefficient. The wear volume increased proportionally with the sliding time, while the wear rate stabilized after reaching a certain duration. The wear mechanism was mainly slight abrasive wear. Additionally, some oxidation occurred on both the WM2Z composite and the Si3N4 ball during friction, forming an oxide film that contributed to the reduction of the friction coefficient. The novelty of this study lies in the first systematic investigation of the effects of sliding speed and time on the wear performance of WM2Z composite, and the revelation that in high-speed sliding environments, even with shorter sliding times, the material experiences faster wear. This discovery emphasizes the important role of sliding speed in the wear process and provides new insights into understanding the wear mechanism of materials in practical applications. This study not only enriches the friction and wear theory of binderless WC matrix composites, but also provides important experimental data and theoretical support for the design and application of related materials, laying a solid foundation for wear resistance optimization and industrial applications.