Influence of heat treatment conditions of Hardox 500 steel on its resistance to abrasive wear
Categoría del artículo: Research Article
Publicado en línea: 31 mar 2025
Páginas: 173 - 195
Recibido: 23 mar 2025
Aceptado: 28 may 2025
DOI: https://doi.org/10.2478/msp-2025-0015
Palabras clave
© 2025 Martyna Zemlik, published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
Among steels intended for mass application, metallic materials with a homogeneous martensitic microstructure or those designed for quenching in the stamping process – often referred to as boron steels for heat treatment – exhibit the highest possible tensile strength (
A common characteristic of low-alloy martensitic steels is the presence of a microalloying addition of boron, which significantly increases the hardenability. Comparatively, its content in steel at a level of 0.001–0.003% by weight provides a hardening intensity equivalent to 0.6% Mn, 0.7% Cr, 0.5% Mo, or 1.5% Ni by weight [4]. Therefore, it can be concluded that an increase in hardenability occurs at boron concentrations that are considered trace levels for other alloying elements [5,6,7,8]. The production of a family of steels characterized by the aforementioned mechanical properties is justified by their high hardenability, which promotes deformation. Moreover, Hardox 500 steel, which exhibits a tensile strength (
However, it should be noted that an increase in steel hardenability entails the risk of technological challenges. The amount of quenching-induced stresses is determined by the type of cooling medium used during the quenching process. The difference in cooling rates between the core and the surface of the object affects the extent of deformation, particularly in large-scale components with complex shapes. For example, the heat treatment of boron-alloyed martensitic steels is performed on profiled structural components such as plowshares or cultivator coulters. The critical cooling rate depends on the chemical composition of the material and increases as hardenability (most commonly defined by the carbon content) decreases. The optimal cooling rate minimizes the occurrence of potential deformations and cracks in the treated material, which is crucial for maintaining the required dimensions and shapes of finished products.
Water remains the most commonly used quenching medium. However, as the hardenability of the material increases, it is recommended to use synthetic or mineral oil for cooling. According to Rudnik [11], the cooling rate in mineral oil is four times lower than that in water, averaging 150°C/s within the temperature range of 650–550°C. A milder cooling medium is also provided by compressed air blast cooling.
In the study by Luo and Bai [12], it was demonstrated that air-cooled, medium-carbon, low-alloy MnCrB cast steel with a chromium content of 0.6% by weight exhibits a tensile strength (
For the study on the influence of cooling methods after austenitization on abrasive wear resistance, Hardox 500 steel was selected. The choice was motivated not only by its widespread industrial application but also by findings from previous field investigations [21,22], which indicated a tendency for accelerated abrasive wear in the vicinity of its welded joints [21]. Namely, field data have repeatedly shown that the heat-affected zones suffer from accelerated material loss under abrasive conditions, compromising component durability. For this reason, we aimed to reproduce microstructural variations – similar to those occurring within the heat-affected zone of welded joints – by applying different cooling rates after austenitization. By doing so, we can systematically induce and characterize the same microstructural heterogeneities. Unlike higher-grade steels such as Hardox 600 and Extreme [23,24], Hardox 500 is classified as bendable and weldable, which enhances its potential for industrial applications [25]. Hardox 500 is used in products such as liners, wear-resistant bars, cutting edges, and excavator buckets [26,27,28,29]. Its resistance to abrasive wear in soil environments may be comparable to that of Hardox Extreme steel [30]. According to Szala et al. [31], Hardox 500 also exhibits the lowest mass loss compared to S355JR, S355J2, and AISI304 steels in tribological tests involving garnet and silicon carbide (carborundum). Its properties may also be more favorable than those of 38GSA steel (hardness of 548 HBW), which is commonly used in Poland for plowshares [9,32]. Furthermore, the wear intensity of Hardox 500 is 12% lower than that of carburized 20MnCr5 steel [33].
The study utilized 10 mm thick sheets of Hardox 500 steel, supplied by the authorized distributor, STAL-HURT. The chemical composition analysis was performed using a spectral method with a Leco GDS500A glow discharge emission spectrometer. The following parameters were applied to ionize the inert gas:
The CCT diagram was obtained through computer simulations carried out using JmatPro software. All heat treatment operations were performed in gas-tight chamber furnaces (FCF 12SHM/R) manufactured by Czylok, using a protective atmosphere of 99.95% argon. The parameters of the heat treatment procedures are presented in detail in Table 1.
Parameters of the applied heat treatment procedures.
No | Heat treatment parameters |
---|---|
1 | As-delivered condition from the steel mill |
2 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 880°C, 20 min and cooling in H2O (∼270°C/s) | |
Tempering: 100°C, 120 min, and air cooling | |
3 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C, 20 min and cooling in transformer oil (∼25°C/s) | |
Tempering: 100°C, 120 min, and air cooling | |
4 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C, 20 min and cooling in Durixol W72 (∼100°C/s) | |
Tempering: 100°C, 120 min, and air cooling | |
5 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C, 20 min, and cooling with 5 bar air blast (∼5°C/s) | |
Tempering: 100°C, 120 min, and air cooling | |
6 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C, 20 min, and cooling with 3 bar air blast (∼3°C/s) | |
Tempering: 100°C, 120 min, and air cooling | |
7 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C and 20 min cooling with 1 bar air blast (∼1°C/s) | |
Tempering: 100°C, 120 min, and air cooling | |
8 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C, 20 min, and air cooling (∼0.1°C/s) | |
9 | Normalization: 880°C, 30 min, and air cooling (∼0.1°C/s) |
Quenching: austenitization at 900°C, 20 min, and furnace cooling (∼0.01°C/s) |
For microscopic examination, light microscopy (LM) was performed using a Nikon Eclipse MA200 light microscope. The samples were etched with a 5% HNO3 solution, in accordance with ASTM E407. A Nikon DS-Fi2 digital camera, coupled with the microscope, and NIS Elements software from Nikon were utilized for recording and analyzing the captured images. Additional microstructure and worn surface images of the samples were conducted using a Phenom XL scanning electron microscope, employing secondary electron imaging or backscattered electron imaging at an accelerating voltage of 15 keV.
Hardness measurements of the base material were performed using a Zwick/Roell ZHU 187.5 universal hardness tester, applying the Brinell method, in accordance with ISO 6506-1:2014. A 2.5 mm diameter carbide ball was used under a load of 187.5 kgf (1838.7469 N), applied for 15 s.
Laboratory tests of abrasive wear resistance were carried out using a T-07 abrasive wear resistance tester in the presence of loose abrasive media, in accordance with GOST 23.208-79, a standard analogous to ASTM G65. The primary difference between the T-07 tester and the device described in ASTM standard G65 is that in the T-07 device, the tested material is positioned horizontally rather than vertically. The T-07 tribotester consists of a steel roller with a rubber ring of 50 mm (+0.2 mm) diameter and 15 mm (−0.1 mm) width, an abrasive feeder that allows for regulating the abrasive flow, and a lever with weights, which generates a vertical force pressing the sample against the roller. The hardness of the rubber coating on the roller is within the range of 78–85 ShA. The tests were conducted under a constant load of
The reference sample was Hardox 500 steel, used in the as-delivered condition. Figure 1 presents the schematic diagram of the T-07 device, along with the positioning of the tested material sample.

Schematic diagram of the T-07 tribotester. 1 – sample, 2 – rubber-rimmed steel wheel, 3 – abrasive, 4 – load, and P1, P2, and P3 – regions of samples subjected to surface topography evaluation.
For the quantitative evaluation of sample surfaces, a HITACHI TM-3000, the second scanning electron microscope was used along with specific graphic-analytical software. Before roughness evaluation, the sample surfaces were cleaned with dry compressed air, inspected for mechanical damage, and marked at three locations: P1, P2, and P3 (Figure 1), where surface evaluation procedures were to be performed. All surface evaluation procedures were conducted at the same magnification, maintaining ten times the elementary segment length lr = 198.03 µm, i.e., 1980.26 µm, and with identical electron beam settings of 15 kV, ensuring precise observation and recording of surface details of steel samples. Before testing, a working distance (WD) calibration procedure was carried out using a roughness standard with a predefined profile.
The following roughness parameters were analyzed:
Statistical analyses were performed using Statistica version 13. The key assumptions required for ANOVA are normality of distribution and homogeneity of variance (Table 2). In cases where these assumptions were not met, this did not necessarily prevent the use of parametric tests, as Lindman [35,36] demonstrated that the F statistic is robust to violations of variance homogeneity. Levene’s test was used to assess the homogeneity of variance, while Shapiro–Wilk’s test was applied to evaluate the normality of distributions. All datasets satisfied the normality assumption except those obtained after 5 bar air cooling. To determine which means differed significantly, Duncan’s
Results of Levene’s test for homogeneity of variance.
Effect SS | Effect df | Effect MS | Error SS | Error df | Error MS |
|
|
|
---|---|---|---|---|---|---|---|---|
Mass wear per 1 m of sliding distance | 0.002684 | 8 | 0.000335 | 0.003295 | 31 | 0.000106 | 3.156335 | 0.00987 |
Based on the results, Hardox 500 steel can be classified as a medium-carbon steel (
Chemical composition of Hardox 500 steel (in % by weight).
C | Mn | Si | P | S | Cr | Ni | Mo | V | Cu | Al | Ti | Nb | B |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
0.29 | 0.74 | 0.28 | 0.007 | 0.001 | 0.61 | 0.06 | 0.018 | 0.012 | 0.010 | 0.054 | 0.003 | — | 0.0009 |
Figure 2 presents a CCT diagram for Hardox 500 steel, obtained through computer simulations. The assigned transformation temperatures for individual phases and structural constituents are as follows: ferrite – 795°C, pearlite – 736°C, bainite – 576°C, martensite start –

Time–temperature graph for Hardox 500 steel. Assigned temperatures for individual transformations, phases, and components of the structure: pearlite – 736°C, ferrite – 795°C, bainite – 576°C, martensite (50%) – 331°C, martensite (90%) – 252°C, and
The hardness measurements of Hardox 500 steel (Figure 3) showed that in the as-delivered condition, it exhibited an average hardness of 440 HBW. Considering the data provided by the manufacturer (470–530 HBW) and the experimentally determined mechanical parameters of the tested steel, it can be observed that the obtained hardness index corresponds to only 77–95% of the hardness declared by the manufacturer. To evaluate the effect of cooling rate on mechanical properties, the steel was first normalized, aiming to refine the microstructure and eliminate the influence of multiple recrystallizations and phase strain in steel sheets obtained through thermomechanical rolling. The study results indicate that the highest hardness levels were achieved after quenching in synthetic oil Durixol W72 (493 HBW), water (487 HBW), and transformer oil (479 HBW) (corresponding heat treatment process parameters are presented in Table 1, entries 4, 2, and 3). In all three cases, the hardness exceeded 470 HBW, which is the minimum value specified by the manufacturer. The use of a higher austenitization temperature before oil quenching is justified by the slower cooling rate of this medium. It is also worth noting that achieving high strength parameters in heat-treated samples under the described conditions requires performing normalizing annealing in a slightly lower temperature range than the hardening process. A gradual decrease in hardness was observed with a reduction in the cooling rate, achieved by using compressed air at progressively lower pressures, ultimately reaching 253 HBW. The lowest hardness value (135 HBW) was recorded after furnace cooling. Interestingly, this value was lower than the expected hardness based on carbon content (0.29% by weight), which should be approximately 156 HBW. This places it between the hardness of normalized and fully annealed samples examined in this experiment. Further discussion will focus on the analysis of microstructural properties.

Hardness measurement results of Hardox 500 steel under different heat treatment conditions.
Figures 4–12 present the microstructures of Hardox 500 steel in the as-delivered condition and those obtained after cooling at different rates. In the as-delivered state (Figure 4a and b), Hardox 500 steel exhibits a lath martensite microstructure, characterized by a three-level structural hierarchy, organized into laths, blocks, and packets. The martensite laths within a single block share the same crystallographic orientation, meaning they represent the same martensite variant. In turn, packets consist of blocks with an identical habit plane, corresponding to the {111} plane of the prior austenite [39–41]. A distinguishing feature is the presence of tempered martensite regions, where coalescence occurs due to the steel’s lower tendency for spontaneous tempering processes. Coalescence results from the fact that martensite blocks sharing the same habit plane and having similar crystallographic orientations relative to the prior austenite tend to merge without the involvement of intermediate phases, leading to the formation of thicker structures [42–46]. Additionally, some areas exhibit higher etching susceptibility, suggesting the presence of fine-dispersed phases such as lower bainite or tempered martensite. The fine-lath microstructure is distinguished by the presence of brighter bands, an effect of the thermomechanical processing performed by the manufacturer. Similar morphological features are observed in the microstructures of Hardox 500 in the as-delivered condition after cooling in water, mineral oil, and synthetic oil (Figures 5–7). SEM analysis revealed that in the case of synthetic oil-quenched Hardox 500, a limited number of martensitic regions undergoing coalescence were likely observed, as indicated by the presence of thickened lath areas. For microstructures obtained after compressed air cooling, it was found that with decreasing air pressure, the proportion of other structures, such as very fine pearlite, increased, while the fraction of martensitic regions decreased (Figures 8–10). Additionally, the presence of large bainitic ferrite (upper bainite) and acicular ferrite plates was noted. However, it should be emphasized that microstructures formed after compressed air cooling exhibit significantly higher tempering resistance than conventional hardened microstructures. Furthermore, the presence of very few regions with acicular structural features indicates that substantial undercooling was still present. After normalization (Figure 11a and b), the microstructure mainly consists of nonequilibrium polygonal ferrite grains and pearlite (quasi-pearlite). Essentially, martensite is no longer observed. After furnace cooling, a banded ferritic-pearlitic microstructure was obtained (Figure 12a and b). The banded structure results from the initial hot rolling stage. Unlike steels produced by conventional methods, this rolling is carried out at relatively high temperatures. Consequently, Hardox steels often exhibit carbon segregation (dendritic segregation), which is not eliminated during subsequent processing stages. This ferritic–pearlitic microstructure is typical for low- and medium-strength steels that have undergone controlled furnace cooling, allowing for the gradual phase transformation of austenite into ferrite and pearlite.

Microstructure of Hardox 500 in the as-delivered condition and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after water cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after mineral oil cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after synthetic oil cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after air at 5 bar pressure cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after air at 3 bar pressure cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after air at 1 bar pressure cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after air cooling and etched with 5% HNO3: (a) LM and (b) SEM.

Microstructure of Hardox 500 after furnace cooling and etched with 5% HNO3: (a) LM and (b) SEM.
Abrasive wear resistance tests (Figure 13) conducted in the presence of loose abrasive media revealed that Hardox 500 steel quenched in water exhibited the highest tribological resistance, with a relative wear resistance coefficient of

Relative abrasive wear resistance coefficient
Results of variance analysis.
Effect SS | Effect df | Effect MS | Error SS | Error df | Error MS |
|
|
|
---|---|---|---|---|---|---|---|---|
Mass wear per meter of sliding distance | 0.5748 | 8 | 0.0718 | 0.0157 | 31 | 0.0005 | 141.9316 | 0.0000 |
Results of Duncan’s test.
State of heat treatment | {1} |
{2} |
{3} |
{4} |
{5} |
{6} |
{7} |
{8} |
{9} |
---|---|---|---|---|---|---|---|---|---|
1 | 0.9867 | 0.0595 | 0.0075 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | |
2 | 0.9867 | 0.0499 | 0.0064 | 0.0001 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | |
3 | 0.0595 | 0.0499 | 0.3235 | 0.0008 | 0.0001 | 0.0000 | 0.0000 | 0.0000 | |
4 | 0.0075 | 0.0064 | 0.3235 | 0.0074 | 0.0002 | 0.0001 | 0.0000 | 0.0000 | |
5 | 0.0000 | 0.0001 | 0.0008 | 0.0074 | 0.1088 | 0.0001 | 0.0001 | 0.0000 | |
6 | 0.0000 | 0.0000 | 0.0001 | 0.0002 | 0.1088 | 0.0001 | 0.0001 | 0.0001 | |
7 | 0.0000 | 0.0000 | 0.0000 | 0.0001 | 0.0001 | 0.0001 | 0.3292 | 0.0001 | |
8 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | 0.0001 | 0.0001 | 0.3292 | 0.0001 | |
9 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | 0.0001 | 0.0001 | 0.0001 |
The results for the reference condition (as-delivered state) did not differ statistically from those obtained after quenching in water or mineral oil. However, for other heat treatment conditions, significant differences in wear resistance coefficients were observed. Notably, when considering only cooling methods that resulted in a hardened microstructure (water and oil quenching), Duncan’s test did not show significant differences in wear resistance. Similarly, no significant differences were observed between samples cooled in synthetic oil and those cooled with compressed air at 5 bar, between samples cooled with compressed air at 5 and 3 bar, and between samples cooled with compressed air at 1 bar and normalized samples. For furnace-cooled samples, which exhibited the lowest wear resistance,
Figure 14 illustrates the dependence of mass loss on material hardness (HBW). Linear regression of the experimental dataset yielded a coefficient of determination (

Effect of hardness on the mass loss of Hardox 500 steel under different heat treatment conditions.
In light of this finding, the Archard wear model was subsequently applied to quantitatively predict mass loss as a function of hardness under various heat‐treatment regimes, thereby enabling a comparison between model forecasts and measured wear data. Based on the dataset collected for nine different states of heat treatment – each with known mass loss (converted to volumetric loss assuming a steel density of 7.8 g/cm³), applied normal load (
The calculated wear volumes were compared with the experimentally determined values (obtained from measured mass loss), revealing satisfactory agreement for materials with the highest hardness levels (Table 6). The experimentally measured volumetric wear losses (
Mass consumption and volumetric wear loss determined experimentally and predicted by the Archard model.
State of heat treatment | Actual mass consumption (g) | Actual volumetric wear loss |
Wear coefficient |
Wear coefficient |
Theoretical volumetric wear loss |
Relative difference (%) |
---|---|---|---|---|---|---|
1 | 0.2236 | 2.84841 × 10⁻⁸ | 0.009880 | 0.010272 | 3.00644 × 10⁻⁸ | +5.55 |
2 | 0.218 | 2.77707 × 10⁻⁸ | 0.010666 | 0.010272 | 2.71511 × 10⁻⁸ | −2.23 |
3 | 0.23884 | 2.97898 × 10⁻⁸ | 0.011578 | 0.010272 | 2.76135 × 10⁻⁸ | −7.32 |
4 | 0.23385 | 3.04255 × 10⁻⁸ | 0.011490 | 0.010272 | 2.68310 × 10⁻⁸ | −11.82 |
5 | 0.25272 | 3.21936 × 10⁻⁸ | 0.009238 | 0.010272 | 3.63384 × 10⁻⁸ | +12.87 |
6 | 0.25722 | 3.27669 × 10⁻⁸ | 0.008781 | 0.010272 | 3.89106 × 10⁻⁸ | +18.72 |
7 | 0.29104 | 3.70752 × 10⁻⁸ | 0.007391 | 0.005787 | 2.90297 × 10⁻⁸ | −21.69 |
8 | 0.29543 | 3.76348 × 10⁻⁸ | 0.005400 | 0.005787 | 4.03325 × 10⁻⁸ | +7.17 |
9 | 0.3371 | 4.29427 × 10⁻⁸ | 0.004570 | 0.005787 | 5.43758 × 10⁻⁸ | +26.59 |
The surface analysis of worn samples, conducted using a scanning electron microscope, provided valuable insights into the micromechanisms of abrasive wear in the examined materials (Figures 15 and 16). The surfaces of Hardox 500 steel in the as-delivered condition and after cooling in water and oils exhibited similar morphological features (Figure 15a–d). The dominant wear characteristics included grooves and scratches aligned with the movement direction of the loose abrasive medium. Between the long scratches, only short, fine scratches oriented at different angles to the wear direction were observed, indicating localized variations in the nature of abrasive interactions. At the edges of these grooves, material buildup was evident, resulting from prior plastic deformation. This material, subjected to cyclic interaction of abrasive particles, was gradually detached, further intensifying the wear process. In addition to microplowing, microcutting played a significant role in the wear mechanism, occurring without significant plastic deformation of the material. In some cases, chips were observed at the edges and ends of the grooves, resulting from material shearing by abrasive particles (Figure 15c and f). The identified micromechanisms of wear – microplowing, microcutting, and asperity shearing – acted synergistically, leading to the progressive removal of material from the sample surfaces (Figure 15a−e). Among these mechanisms, microcutting is a more aggressive wear process than microplowing, which initially induces plastic deformation in the surface layer. Material detachment from the top layer may occur only after repeated passes of abrasive particles. Additionally, during the interaction of abrasive grains with the metal, the bottom of the grooves undergoes work hardening, increasing the material’s resistance to further wear. At lower cooling rates, in addition to long parallel grooves and scratches, shorter but deeper scratches appeared, oriented at different angles to the abrasive grain movement direction (Figure 15g−i). These effects led to material spallation, resulting in deep pits and significant mass loss. The spalled material exhibited irregular shapes, likely caused by the abrasive grains penetrating the top metal layer (Figure 15g−i). These grains were subjected to repeated interactions with other abrasive particles and were eventually pulled out along with fragments of the material. Around the spallation sites, plastically deformed regions were observed. These phenomena were particularly intense in samples cooled with compressed air at 1 bar, normalized, and fully annealed (Figure 15g–i) and were associated with the presence of soft ferritic phases in the microstructure. In complex microstructures containing phases with significantly different hardness, abrasive wear initiates in the softer phase. This phase gradually wears away, exposing regions containing the harder phase. As wear progresses, the hard phase begins to protrude above the surface, forming a natural protective barrier that partially shields the softer phase from further wear. This process continues until the hard phase protrudes sufficiently for it to be removed by the abrasive particles. For samples cooled at lower rates, the dominant wear mechanisms were material spallation leading to deep pits, grooving combined with plastic deformation, and wear caused by cyclic particle interaction.

SEM analysis under unetched conditions of surfaces of Hardox 500 steel subjected to abrasive wear testing under different heat treatment conditions: (a) as-delivered condition, (b) after water cooling, (c) after mineral oil cooling, (d) after synthetic oil cooling, (e) after air cooling at 5 bar pressure, (f) after air cooling at 3 bar pressure, (g) after air cooling at 1 bar pressure, (h) after air cooling, and (i) after furnace cooling.

3D images obtained by SEM analysis of sample surfaces subjected to wear testing along the longitudinal direction of abrasive movement: (a) as-delivered condition, (b) after water cooling, (c) after mineral oil cooling, (d) after synthetic oil cooling, (e) after air cooling at 5 bar pressure, (f) after air cooling at 3 bar pressure, (g) after air cooling at 1 bar pressure, (h) after air cooling, and (i) after furnace cooling.
Figure 17 presents cross-sections of selected heat treatment conditions, including the as-delivered condition, mineral oil quenching, air cooling at 1 bar pressure, and furnace cooling. On the sample surfaces, pits and groove bottoms of varying sizes are clearly visible (Figure 17a). Only small areas of plastically deformed material were observed around these features. However, the near-surface layer did not exhibit significant signs of plastic deformation. In the sample shown in Figure 17c, which has a complex multiphase microstructure, different structural components (bainite, ferrite, and martensite) wear at a similar rate, with pits distributed uniformly across these phases. In contrast, for the furnace-cooled sample (Figure 17d), deep pits predominantly form within the ferritic phase. This confirms the described wear mechanism of microstructures with components of differing microhardness, where the softer phase undergoes wear more intensively. This process leads to selective material degradation, contributing to localized pits and surface irregularities. Consequently, differences in the microhardness of individual phases significantly influence the service life of working elements made from the tested material (Table 7).

Cross-sectional SEM analysis under unetched conditions of selected samples subjected to abrasive wear: (a) as-delivered condition, (b) after mineral oil cooling, (c) after air cooling at 1 bar pressure, and (d) after furnace cooling.
Results of variance analysis.
Effect SS | Effect df | Effect MS | Error SS | Error df | Error MS |
|
|
|
---|---|---|---|---|---|---|---|---|
|
0.1072 | 8 | 0.0134 | 0.1407 | 18 | 0.0078 | 1.7140 | 0.1629 |
|
0.9911 | 8 | 0.1239 | 4.6533 | 18 | 0.2585 | 0.4792 | 0.8551 |
|
4.4831 | 8 | 0.5604 | 3.9031 | 18 | 0.2168 | 2.5844 | 0.0450 |
Due to significant differences in the surface condition of the worn samples observed depending on the heat treatment state, the following roughness parameters were measured:

Roughness parameters

Profilograms of Hardox 500 steel under different heat treatment conditions subjected to abrasive wear testing.
Results of Duncan’s test for the parameter
State of heat treatment | {1} |
{2} |
{3} |
{4} |
{5} |
{6} |
{7} |
{8} |
{9} |
---|---|---|---|---|---|---|---|---|---|
{1} | 0.3384 | 0.1759 | 0.3759 | 0.5651 | 0.1470 | 0.0034 | 0.6780 | 0.7236 | |
{2} | 0.3384 | 0.6295 | 0.9243 | 0.6662 | 0.5640 | 0.0215 | 0.5545 | 0.5109 | |
{3} | 0.1759 | 0.6295 | 0.5860 | 0.3924 | 0.8970 | 0.0488 | 0.3146 | 0.2855 | |
{4} | 0.3759 | 0.9243 | 0.5860 | 0.7171 | 0.5185 | 0.0197 | 0.6028 | 0.5598 | |
{5} | 0.5651 | 0.6662 | 0.3924 | 0.7171 | 0.3405 | 0.0103 | 0.8493 | 0.7944 | |
{6} | 0.1470 | 0.5640 | 0.8970 | 0.5185 | 0.3405 | 0.0516 | 0.2694 | 0.2426 | |
{7} | 0.0034 | 0.0215 | 0.0488 | 0.0197 | 0.0103 | 0.0516 | 0.0075 | 0.0067 | |
{8} | 0.6780 | 0.5545 | 0.3146 | 0.6028 | 0.8493 | 0.2694 | 0.0075 | 0.9312 | |
{9} | 0.7236 | 0.5109 | 0.2855 | 0.5598 | 0.7944 | 0.2426 | 0.0067 | 0.9312 |
The article presents a comprehensive approach to the evaluation of heat-treated steels, with a particular focus on microstructural development aimed at achieving varied responses in terms of tribological resistance. In the course of this study, a broad spectrum of surface roughness parameters was selected for analysis. This decision was motivated, in part, by the absence of clear literature guidelines that would support the selection of a narrower set of parameters. The authors were concerned that limiting the scope might reduce the likelihood of detecting potential microstructural differences arising from distinct heat treatment processes, which could influence wear resistance. Therefore, an extended set of roughness parameters –
In this study, despite conducting a comprehensive analysis of roughness parameters after various heat treatment conditions of Hardox 500 steel, it was observed that traditional roughness parameters do not fully reflect the surface states, which exhibit a high degree of variation. Therefore, the authors decided to address this issue in the discussion. Standard roughness parameters, such as
Explanations for the above observations, as well as valuable supplementation to the experimental studies, are provided by numerical analyses of surface topography evolution, as proposed by Garcia-Suarez et al. [52]. The simulation results indicate that, regardless of the initial surface condition, wear processes gradually “erase” the original topographic features. As a result, the surface tends toward a steady-state roughness, reached after a transitional period during which surface parameters oscillate around an average value. Comparing these results with the Hardox 500 study allows for several conclusions. First, both experimental studies and numerical analyses suggest that global roughness parameters are insufficient for a comprehensive description of surface conditions, especially when local defects play a crucial role. Second, the transitional period observed in simulations, during which the surface “forgets” its initial state, reflects dynamic wear processes that may also occur in steel subjected to different heat treatment variants. Numerical simulations have shown that initially smooth surfaces reach a steady-state roughness more quickly, whereas initially rough surfaces require a longer transitional period. This observation aligns with the findings for Hardox 500, where differences in wear mechanisms visualized through SEM were not fully captured by averaged roughness parameters. This indicates that, under real operating conditions, the influence of roughness on wear may be more complex and dependent on local micromechanical wear mechanisms than suggested by standard parameters. Therefore, integrating experimental studies on Hardox 500 with numerical analyses in future research would enable a more comprehensive understanding of wear mechanisms. Advanced techniques, such as three-dimensional topography analysis, allow for a more precise identification of local defect distribution and their impact on overall surface conditions. Such a holistic methodology could contribute to the optimization of heat treatment processes, leading to increased wear resistance and improved durability of the material under operational conditions.
Additionally, analyses conducted by Bigerelle et al. [53] demonstrated that three primary wear mechanisms can be distinguished depending on the size of abrasive grains. For particles larger than 125 µm, wear occurs through microcutting, whereas for grains smaller than 10 µm, adhesion dominates. In the intermediate range, when the abrasive particle size is between 10 and 125 µm, a phenomenon known as the “grain size effect” is observed, where the extreme amplitude of peaks to valleys decreases with increasing abrasive particle size. This indicates the crucial role of grain size distribution in the surface degradation process. Bigerelle et al. also demonstrated that beyond a critical autocorrelation length (approximately 160 µm), the surface loses memory of its initial structure, meaning that its further evolution can be modeled using extreme value theory. Autocorrelation measures how roughness values at different points on the surface are related to one another. If there is a distinct correlation at a certain length, it indicates that the surface maintains an ordered structure on that scale. However, once the critical autocorrelation length (in this case, 160 µm) is exceeded, the surface loses this ordered relationship, and its further evolution becomes more random and independent of its previous state.
An extension of the above studies is provided by the results presented by Szala et al. [31], who investigated the wear mechanisms of S235JR, S355J2, C45, AISI 304, and Hardox 500 steels using three types of abrasives: garnet, corundum, and silicon carbide (carborundum). Their experiments demonstrated that the type of abrasive used has a decisive impact on wear mechanisms and local surface topography. For example, when silicon carbide – which is characterized by very high hardness and fine grain size – was used, the dominant wear mechanism for Hardox 500 steel was microcutting, resulting in lower values of
In conclusion, although traditional roughness parameters provide valuable information about the average surface condition, their limited sensitivity to local topographical variations makes them insufficient for analyzing materials with complex wear structures. Thus, it is essential to expand the research methodology to include techniques that enable a more precise description of local surface features, leading to a better understanding of wear mechanisms and the more effective adjustment of heat treatment parameters and material selection for specific operating conditions.
The obtained results emphasize the importance of selecting appropriate heat treatment parameters for components made from the analyzed material. The statistical analysis of the results confirmed significant differences between the examined heat treatment variants, indicating the material’s sensitivity to changes in cooling intensity, which directly influences microstructure formation. The research, conducted using the described methodology, allowed for the formulation of the following conclusions: The use of high-intensity cooling media, such as water and oils, resulted in the formation of a martensitic microstructure, characterized by high hardness, which directly translated into significantly increased tribological resistance ( The application of the Archard model to describe the volumetric wear of steel with different heat treatment conditions requires adjusting the wear coefficient The dominant wear mechanisms included microplowing, microcutting, and asperity shearing, particularly in high-hardness samples. In samples cooled at lower intensities, the primary wear mechanism was cyclic particle interaction leading to material spallation. In complex microstructures, wear typically initiated in the softer phase, leading to the formation of deep pits, while the harder phase temporarily acted as a protective barrier. However, continued abrasion eventually led to its detachment, accelerating surface degradation. Variance analysis indicated no statistically significant differences between roughness parameters depending on heat treatment conditions ( Given the above findings, in addition to traditional roughness parameters, it is essential to apply more advanced surface analysis methods. Techniques such as three-dimensional topography analysis allow for a more precise assessment of local defect distribution and their influence on the overall surface condition. This holistic approach can contribute to enhancing the material’s wear resistance and improving its durability under operational conditions.
Authors state no funding involved.
Martyna Zemlik: Conceptualization, methodology, validation, formal analysis, investigation, resources, data curation, visualization, writing – original draft preparation, supervision. Beata Bialobrzeska: Conceptualization, methodology, validation, formal analysis, investigation, resources, data curation, visualization, writing – original draft preparation, writing – review and editing, supervision. Mateusz Stachowicz: methodology, validation, formal analysis, investigation, data curation. Lukasz Konat: formal analysis, resources, writing – review and editing.
Authors state no conflict of interest.
Data sharing is not applicable to this article as no datasets were generated or analysed during the current study.