3.1. Tribological Characterization
Tribological testing of sintered steels is a critical step in verifying their functional reliability in automotive applications. For components such as a crankshaft gear or a sensor flange, the coefficient of friction and the intensity of wear are the dominant factors determining the service life of the entire mechanism. The test is performed in order to simulate real operating conditions of sliding contact and to quantify the influence of surface treatments (steam oxidation, nitriding) and matrix chemistry (especially unique systems with high Ti and V content) on resistance to surface degradation. Tribological properties were determined by the non-destructive ball-on-disc method in accordance with the international standard ASTM G99-17. The essence of the test consists of pressing a stationary counter-body (steel ball) against a rotating sample with a defined normal force. During the test, the frictional force is recorded in real time, from which the software calculates the coefficient of friction. After the completion of the test, the volume loss of the material and the depth of penetration into the surface layer are evaluated using optical profilometry [
29,
30].
Tribological characterization was carried out in order to simulate real operating conditions of sliding contact in automotive applications such as gears and sensor hubs. Tribological properties were determined using the Anton Paar TRB tribometer in a ball-on-disc configuration. The choice of a normal load of 5.00 N was chosen to achieve measurement stability without creating dynamic instability that could distort the friction coefficient. The use of a counter-body made of 100Cr6 steel with a hardness of approximately 60 HRC is the standard for verifying the abrasion resistance of sintered steels, as it allows us to monitor the mechanisms of micro-cutting and plastic deformation of the sintered die, temperature 23.9–26.3 °C and relative humidity 16.1–25.3% [
31,
32,
33]. The test was conducted in an uncontrolled laboratory environment while maintaining a record of temperature and humidity, which is consistent with the protocol for comparative studies of new material systems [
31,
32,
33]. The test parameters are listed in
Table 2.
Figure 2a presents the dependence of the coefficient of friction on the number of cycles for Sample 1 (Ni-Mo-Ti) and Sample 2 (C-Cu-Ti). The graph documents the aggressive onset of friction in a high-carbon system compared to a more stable course Ni-alloys.
Figure 2b: Comparison of penetration depth over time. A threefold difference in the depth of penetration of the counter-body is visible (11.46 μm vs. 34.67 μm), which indicates higher plasticity and better fixation of the hard phases in Sample 1.
On the left, the morphology of the surface of Sample 1 (Ni-Mo-Ti system) is captured with a vertical color scale of height levels in the range of 0–80 μm (
Figure 3). On the right, the topography of Sample 2 (C-Cu-Ti system) is shown with the color gamut adjusted in the range of 0–100 μm (
Figure 3). The color gradient on both maps represents local changes in profile height in accordance with ISO 25178 [
34]. The blue spectrum (negative values relative to the reference plane) defines the geometry and depth of the wear groove formed by contact with the 100Cr6 counter-body. The orange-red areas represent the original relief of the surface of the components with a characteristic roughness after steam oxidation and nitriding. The mapped area for each sample has nominal dimensions of 4.5 × 2.3 mm.
The part on the left shows (
Figure 4) the spatial morphology of the Sample 1 friction trail (Ni-Mo-Ti system). The vertical axis (Z) captures the relief in the range from −59.55 μm (foot bottom) to +29.09 μm (tops of the original surface). The right part (2) documents the condition of Sample 2 (C-Cu-Ti system), where the vertical range is more pronounced, from −63.29 μm to +44.30 μm. The color scale (right) assigned to each map indicates local height differences in micrometers in accordance with ISO 25178 [
34,
35,
36]. Both visualizations cover an area measuring approximately 4.5 × 2.3 mm. Sample 1 shows a regular, symmetrical groove cross-section with a maximum measured steady-state penetration depth of 11.46 μm. In Sample 2, the profile indicates a wider and geometrically more rugged wear area, which correlates with a dynamically measured penetration depth of 34.67 μm.
The isometric cutouts on the right provide a view of the micro-texture of the bottom of the friction trail, where the directional orientation of the micro-grooves formed by the interaction with the 100Cr6 counter-body is visible.
The profile shape (
Figure 5) of Sample 1 shows a relatively symmetrical, shallow and wide trace. The value of Sq = 19.352 μm expresses the average height deviation of the track. Negative asymmetry Ssk = −1.552 confirms that valleys (pores and grooves) predominate in the track, which serve as micro-reservoirs for the capture of abrasion particles (debris). A lower Sku value = 3.783 indicates a more stable wear pattern with less occurrence of sharp peaks. In Sample 2, the trace is markedly asymmetrical with a deep local indentation (red area). This irregular shape is indicative of the micro-ploughing mechanism. The maximum trace depth reaches up to 70,005 μm, which is significantly higher than in the first sample. The cross-sectional area is 47,576.764 μm
2, which represents the volume of material pulled out under dynamic loading. An overview of key data is provided in the
Table 3.
Figure 6 shows a statistical analysis of the topography of the wear footprint in accordance with ISO 25178. The vertical axis (Y) in both graphs represents the depth/height of the profile in micrometers μm). The horizontal axis (top) expresses the material ratio as a percentage % for the red curve. Graph 1 (left): belongs to Sample 1 (Ni-Mo-Ti). The total analyzed vertical range is from 0.00 to 68.25 μm. The red curve of the material ratio shows a steep decrease in the initial phase (up to approximately 7 μm), which indicates the character of the bearing surface. Graph 2 (right): belongs to Sample 2 (C-Cu-Ti). The vertical range in this case is wider, up to 83,717 μm, which correlates with the deeper penetration found in dynamic measurement.
Table 4 captures a set of quantitative parameters of the height distribution of the surface in accordance with the international standard ISO 25178. These indicators provide a comprehensive view of the roughness and overall morphology of the investigated materials, while serving to mathematically describe the surface texture. The parameters of arithmetic and quadratic deviation define the degree of roughness, while the coefficients of asymmetry and pointiness determine the predominance of peaks over valleys and the steepness of the elevation distribution. Also included are the parameters of maximum heights and depths, which define the overall vertical span of the relief. Overall, these data make it possible to accurately assess the geometric integrity of surface layers before and after tribological loading and to identify the mechanisms of friction-induced structural changes. The mapping was performed on the worn surface (inside the wear track) to characterize the micro-topography of the friction contact area.
Figure 7 and
Figure 8 represent a detailed mapping of a surface measuring 1.2 × 0.161 mm. Sample 1 (Ni-Mo-Ti):
Figure 7 shows 2D elevation maps, where a color gradient in the range of 0–40 μm represents the distribution of local peaks and valleys. The lower 3D model captures a micro-relief with a vertical range of the
Z-axis from −21.32 to +22.95 μm. Sample 2 (C-Cu-Ti): The upper row documents the surface with a color gamut adjusted to 0–25 μm for better resolution of finer textures. The 3D isometric view (bottom) shows a vertical range of Z from −13.61 to +14.95 μm. These measurements are used to accurately quantify the condition of the surface before tribological loading (roughness analysis after nitriding) or to characterize the micro-texture of the bottom of the friction track. They make it possible to identify the presence of open pores and trace grooves after the net-shape molding process.
3.2. Microstructure of SEM/EDX Analysis
Scanning electron microscopy (SEM) in conjunction with energy-dispersive X-ray spectroscopy (EDX) represents the dominant technique for the detailed study of surface morphology and micro-chemical constitution of materials. In the field of powder metallurgy and automotive development, this method is necessary to identify the distribution of alloying elements in a heterogeneous sintered matrix and to characterize secondary phases, such as titanium carbides and vanadium investigated in this work. The main goal of measurements on the Phenom benchtop microscope (Eindhoven, Netherlands) is a comparative analysis of the surface condition before and after the tribological load (base material) and after it (friction trace) [
37,
38].
The image on the left (
Figure 9) documents the initial surface condition of the component. A typical heterogeneous morphology of sintered steel is evident with the presence of open pores (dark irregular areas) and a continuous metal matrix (light areas). The surface shows signs of integrity after the processes of vapor oxidation and plasma nitriding. The image on the right (
Figure 9) captures the detailed morphology of the trace of wear. The surface is characterized by parallel grooves and micro-grooves oriented in the direction of relative motion of the counter-body, which confirms the dominant mechanism of micro-ploughing [
34,
35].
The left image (
Figure 10) shows the initial surface state of the high-carbon system. A dense network of open pores (black irregular formations) in an evenly sintered matrix is visible. The lighter areas correspond to the metal necks, with the surface morphology reflecting the final treatment by steam oxidation and nitriding. The image on the right (
Figure 10) shows the surface of the friction path after the 1000 m friction path. Compared to Sample 1, there is a denser network of parallel grooves and a more pronounced plastic deformation of the edges of the grooves, which indicates an aggressive micro-cutting mechanism.
The upper spectrum (1 no wear,
Figure 11) represents the chemical state of the base material before the test. It is dominated by characteristic iron peaks supplemented by low-intensity copper and oxygen peaks. Spot analysis in this area confirmed the low initial oxidation of the surface after heat treatment. The lower spectrum (1 signs of wear) captures the elemental composition directly in the frictional path after the end of the test. Compared to the basic material, there is a significant increase in the intensity of the oxygen peak. The quantitative evaluation of the point analysis in the wear trace showed an increase in the mass concentration of oxygen up to the level of 31.74%, while in the base material the measured values were significantly lower. This significant increase in oxygen content at the point of contact with the 100Cr6 counter-body is direct evidence of the tribo-oxidative mechanism of wear. The resulting oxide layers in combination with the nickel–molybdenum matrix contribute to the stabilization of friction contact, which correlates with the measured lower coefficient of friction and a minimum penetration depth of 1.46 μm in this sample.
Table 5 provides a quantitative overview of changes in the local chemical composition of Sample 1 (Ni-Mo-Ti) before and after tribological loading. It documents the atomic and mass concentrations of the dominant elements iron, copper and oxygen, capturing the chemical response of the surface. At the point of wear (signs of wear), a slight increase in oxygen and iron content is observed, which indicates the formation of tribo-oxide layers. On the contrary, the mass concentration of copper shows a decrease from the initial 4.28% to 2.12%, which indicates a local transformation of the surface texture. These data, obtained by the spectrometer of the Phenom instrument, are used for accurate statistical verification of wear mechanisms observed on SEM micrographs and complement the results of dynamic tribometry.
The upper record (2 no wear,
Figure 12) represents the chemical profile of the base material of Sample 2. The spectrum shows dominant iron peaks accompanied by copper, molybdenum and silicon peaks. The significant intensity of the oxygen peak in the initial state confirms the presence of a continuous oxide layer (magnetite) formed by the process of vapor oxidation. Quantitative spot analysis in this area identified an initial oxygen content of 5.88%
w/
w. The bottom record (2 signs of wear) captures the elemental composition at the point of the friction path. The spectrum confirms the presence of all alloying elements of the matrix, with an increase in oxygen concentration up to 11.95% by weight recorded at some points. This phenomenon indicates local oxidation of the surface during dynamic contact. Traces of nickel are also visible in the spectrum, which indicates a slight chemical heterogeneity of the sintered structure in this system.
Table 6 summarizes the changes in the local chemical composition of Sample 2 (C-Cu-Ti) before and after tribological loading. The comparison of the values confirms a slight increase in the mass concentration of oxygen from the initial 7.96% to 10.94%, which verifies the course of oxidation processes at the site of dynamic contact with the counter-body. A significant increase in silicon content (from 0.36% to 3.82%) and changes in the proportion of copper and molybdenum in the wear trace indicate local exposure of deeper layers of the die and redistribution of elements due to mechanical ploughing.