In a piston internal combustion engine, as part of the movement of the piston in the cylinder sleeve, there is a variable instantaneous speed of the moving kinematic pairs. This is due to the reciprocating movement of the piston. The ring pack moves stochastically in the piston grooves. Therefore, it is difficult to determine the mutual position of the moving planes of the piston and piston rings relative to the cylinder surface. Nevertheless, it is possible to determine their mutual position with high probability, depending on the dynamic viscosity of the lubricant, the geometry of all elements of the main engine mechanism, the rotational speed of the crankshaft and the thermodynamic conditions in the combustion chamber. The distribution of the thickness of the oil film between the piston rings and the cylinder wall is affected by a number of engine operating parameters [42]. On the basis of simulation and experimental data, it is possible to determine the approximate thickness of the oil film between the given engine components. The smallest film thickness occurs between the upper piston ring and the cylinder wall. On average, it ranges from 0.1 to 15 µm, depending on the engine stroke, shaft speed and other parameters characterizing the engine load conditions. As is well known, oil parameters play a very important role here and affect the value of hydrodynamic pressure and the possibility of mixed friction or boundary friction conditions.
In the tests, the measurement of the thickness of the lubricating film was performed. Different loads were assumed for selected slider sets with applied coatings and lubricating fluid. The angle of inclination was constant during the test run. The name of the slider comes from the name of the coating. During the interferometric test, the number of fringes at different speeds is read and analyzed. In the test, the same number of evenly arranged fringes shifted on given interferograms with different speeds means that the slider inclination was unchanged at the time of the test and no elastic deformation of the contact surface of the kinematic pairs was observed. All tests were carried out in the conditions of hydrodynamic lubrication, reflecting the conditions of fluid friction between engine components. Experiments with 65% by weight of glycerol were performed using various sliders with a constant load of 5 N and a constant slope of 1:1875. As with the inclination of the plane ring relative to the cylinder face for symmetrical and asymmetric parabolic shapes.
Table 2
Properties of lubricants used in the tests
Lubricant | Refractive index | Dynamic viscosity (22°C, mPas) |
Oil | 1.46 | 840 |
99% Glycerol | 1.47 | 704 |
65% Glycerol | 1.45 | 14 |
Table 3
contact angle and contact angle hysteresis surface materials and lubricants
Lubricating liquids | Zipper surface material | Contact angle CA (°) | Contact angle hysteresis CAH (°) |
65% Glycerol | Steel X90CrMoV18 | \({39.2}_{-5.4}^{+7.8}\) | \({46.5}_{-3.2}^{+2.3}\) |
65% Glycerol | AlTiN/CrN/Cr/…/CrN/Cr | \({32.1}_{-5.8}^{+6.4}\) | \({\text{48,7}}_{-2.1}^{+2.2}\) |
65% Glycerol | AlN/CrN/…/AlN/CrN | \({38.5}_{-4.6}^{+5.5}\) | \({\text{45,2}}_{-2.4}^{+2.3}\) |
65% Glycerol | CrN/AlN/…/CrN/AlN | \({61.7}_{-4.8}^{+54}\) | \({\text{24,5}}_{-1.4}^{+1.4}\) |
65% Glycerol | SiO2 | \({53.1}_{-7.7}^{+8.4}\) | \({35.1}_{-2.9}^{+2.6}\) |
65% Glycerol | Cr | \({66.8}_{-5.4}^{+5.1}\) | \({34.9}_{-2.4}^{+1.7}\) |
99% Glycerol | Steel X90CrMoV18 | \({46.3}_{-4.6}^{+4.8}\) | \({47.4}_{-1.1}^{+1.1}\) |
99% Glycerol | AlTiN/CrN/Cr/…CrN/Cr | \({42.7}_{-3.2}^{+4.1}\) | \({45.2}_{-1.3}^{+1.5}\) |
99% Glycerol | AlN/CrN/…/AlN/CrN | \({45.2}_{-3.7}^{+2.4}\) | \({47.4}_{-1.0}^{+1.4}\) |
99% Glycerol | CrN/AlN/…/CrN/AlN | \({69.8}_{-3.4}^{+2.8}\) | \({35.2}_{-1.1}^{+1.2}\) |
99% Glycerol | SiO2 | \({62.3}_{-4.3}^{+3.8}\) | \({33.8}_{-1.3}^{+1.6}\) |
99% Glycerol | Cr | \({74.6}_{-3.6}^{+4.2}\) | \({47.4}_{-1.9}^{+1.1}\) |
Oil | Steel X90CrMoV18 | \({26.1}_{-5.9}^{+5.8}\) | \({31.2}_{-1.8}^{+1.6}\) |
Oil | AlTiN/CrN/Cr/…CrN/Cr | \({12.4}_{-2.2}^{+3.4}\) | \({28.8}_{-1.4}^{+1.2}\) |
Oil | AlN/CrN/…/AlN/CrN | \({20.6}_{-1.5}^{+1.8}\) | \({30.9}_{-1.2}^{+1.7}\) |
Oil | CrN/AlN/…/CrN/AlN | \({54.6}_{-1.6}^{+2.1}\) | \({18.7}_{-1.9}^{+1.6}\) |
Oil | SiO2 | \({46.7}_{-1.1}^{+2.1}\) | \({26.6}_{-1.1}^{+1.3}\) |
Oil | Cr | \({56.2}_{-2.7}^{+1.5}\) | \({25.1}_{-1.2}^{+1.2}\) |
Figure 1 shows the variation of film thickness versus speed for the 65 wt% test. glycerol solution. In order to better understand the issues of hydrophilicity and hydrophobicity, two theoretical layer thickness-velocity curves were additionally plotted on the film thickness. In the study, also for the purpose of systematizing the results, the theoretical Reynolds equations were calculated on the basis of a full two-dimensional solution of finite differences for surfaces covered with a lubricating film. The plotted theoretical curve read in the absence of slippage is equivalent to the classical Reynolds equation. (1). Theoretical results for full slip conditions were calculated using the extended Reynolds equation model with boundary conditions corresponding to full slip as in the case of equation. (2) [43]. Eq. (2) uses the critical stress slip model. In this model, stresses of this type are assumed to be zero. Comparing the terms of the equation on the right side of both equations, including one with boundary conditions for full slip (Eq. 2) was found to be only half of that with boundary conditions without slip. As a consequence of these findings and assumptions, it can be assumed that the theoretical thickness of the layer under the boundary conditions of full slip is smaller. The results of this are shown in Fig. 1.
$$\frac{\partial }{\partial \text{x}}\left({h}^{3}\frac{\partial \text{p}}{\partial \text{x}}\right)+\frac{\partial }{\partial \text{y}}\left({h}^{3}\frac{\partial \text{p}}{\partial \text{y}}\right)=6u\eta \frac{dh}{dx}$$
1
$$\frac{\partial }{\partial \text{x}}\left({h}^{3}\frac{\partial \text{p}}{\partial \text{x}}\right)+\frac{\partial }{\partial \text{y}}\left({h}^{3}\frac{\partial \text{p}}{\partial \text{y}}\right)=3u\eta \frac{dh}{dx}$$
2
The sliders of the device made of steel X90CrMoV18 and AlN/CrN/…/AlN/CrN provided a high layer thickness, which coincided with the classic theory of non-slip hydrodynamic lubrication. The highest layer thickness results were also obtained for the AlTiN/CrN/Cr/…/CrN/Cr coating. It is an innovative highly complex multi-layer coating created by the author in such a combination based on theoretical assumptions in order to obtain special wetting properties. The thickness of the lubricating film created by the SiO2 and Cr sliders was almost the same and slightly smaller than that of the AlTiN/CrN/Cr/…/CrN/Cr, AlN/CrN/…/AlN/CrN and steel X90CrMoV18 sliders. The thickness of the lubricating film created by the CrN/AlN/…/CrN/AlN coated slider was the lowest. In this case, its change with speed is perfectly correlated with the theory of hydrodynamic lubrication for full slip conditions. This shows that the molecular bonds of CrN/AlN/…/CrN/AlN and the lubricant are weak. The difference in the test conditions was the surface roughness. Other parameters for all test trials, such as slider inclination, liquid parameters are the same.
The surface roughness of the CrN/AlN/…/CrN/AlN slider is higher than for the other coatings (Table 1). Nevertheless, the roughness of this coating is almost an order of magnitude less than the measured minimum layer thickness. Slightly lower roughness was obtained for the Steel X90CrMoV18, AlTiN/CrN/Cr/…/CrN/Cr and AlN/CrN/…/AlN/CrN coatings. Cr and SiO2 coatings had the lowest roughness. Nevertheless, this parameter did not significantly affect the thickness of the oil film in relation to coatings steel X90CrMoV18, AlTiN/CrN/Cr/…/CrN/Cr and AlN/CrN/…/AlN/CrN.
Assuming these surface properties, it can be said that the small thickness of the lubricating film layer obtained with the CrN/AlN/…/CrN/AlN slider cannot result from high surface roughness. Otherwise, a higher roughness of the applied coating would increase the hydrodynamic effect leading to increased coating thickness. In this arrangement, the thickness of the lubricating film layer generated on the slider surface depends on interfacial and surface effects.
The relationship between the thickness of the lubricating film and the contact angle and CAH is shown in Fig. 2. According to the accompanying figures, it can be concluded that the film thickness decreases significantly with the increase of the contact angle. For the materials adopted, it can be concluded that they coincide with the general conceptual assumption, with the exception of Cr and SiO2. For this coating, the contact angle is the second largest among all the adopted variants of sliders, but it produces a considerable thickness of the lubricating film.
Based on Fig. 3, it can be assumed that the correlation of the thickness of the lubricating film layer and CAH is much better than in the case of CA. It performs much better in the predictability of the lubricating film for individual materials. CAH shows a more stable and rectilinear nature of the waveform. In the case of Fig. 3, slight deviations of SiO2, Cr and CrN/AlN/…/CrN/AlN from the approximation waveform can be noticed. An additional approximation of CA was performed using a sixth-order polynomial and in the case of CAH using a fourth-order polynomial.
Differences between the CrN/AlN/…/CrN/AlN sliders and the AlTiN/CrN/Cr/…/CrN/Cr sliders, which represent the two extreme abilities of forming a lubricating film, are shown in Fig. 4. They were verified by carrying out tests with 99 wt. glycerin. The introduction of glycerol from 65 to 99% by weight allowed to increase the viscosity. The test was performed for 5 and 10 N. The slope was 1:1650. The results of two different loads are shown in Figs. 4 and 5 for the same coatings. The measurement results including the AlTiN/CrN/Cr/…/CrN/Cr coating thickness of the slider are well correlated with the theoretical anti-slip curves in the specified speed range for two loads. However, the film thickness generated by the CrN/AlN/…/CrN/AlN slider is much smaller. Due to the large measurement errors of the interference images of the CrN/AlN/…/CrN/AlN slider at low speeds, Figs. 4 and 5 show only the thickness of the lubricating film layer measured at higher speeds starting from 5 mm/s. The minimum coating thickness shown in Figs. 4 and 5 is still about five times greater than the roughness of the CrN/AlN/…/CrN/AlN slider given in Table 1. It is therefore assumed that there is no direct contact between the two cooperating surfaces of the selected kinematic pairs.
A significant reduction in the thickness of the lubricating film for the CrN/AlN/…/CrN/AlN coating on the slider surface can be attributed to the hydrophobic properties of this coating and the intensification of the repulsion of lubricant particles at low feed speeds. Hysteresis of the surface contact angle of CrN/AlN/…/CrN/AlN and AlTiN/CrN/Cr/…/CrN/Cr with 99% by weight glycerol is 35.2° and 45.2°, respectively, as shown in Table 3. It is assumed that the higher the value of the CAH parameter, the greater the thickness of the lubricating film. Figures 4 and 5 show an interesting phenomenon where the resultant thickness of the lubricating layer obtained by the slider with the CrN/AlN/…/CrN/AlN coating is smaller than the theoretical full slip curves. Therefore, the test was repeated for the Olalphaolefin oil. This oil has approximately the same dynamic viscosity value as 99% by weight. glycerol. However, these substances have different polarity values. Olalphaolefin oil is a non-polar oil while glycerin is polar. This will extend the range more comparison and will allow to assess the possibility of influencing the thickness of the oil film in the operating conditions of a piston oil engine.
Figures 6 and 7 show the change in the thickness of the lubricating film layer for oliphaolefin oil in relation to the speed of movement at an inclination (slope: 1:1820) for loads of 5 and 10 N. In this case, all accepted materials were used. Sliders with the material steel X90CrMoV18, AlTiN/CrN/Cr/…CrN/Cr, AlN/CrN/…/AlN/CrN and CrN/AlN/…/CrN/AlN were tested for the same measurement conditions. In these coatings, there is a large variation in the contact angle CA, respectively: 26.1°; 12.4°, 20.6°, 54.6°. In the case of CAH, these values are respectively 31.2°; 28.2°; 30.9°; 18.7°. The first three shells have divergent CAs but have very similar CAH values. Therefore, it is necessary to carefully analyze which of the parameters more closely reflects the theoretical prediction of CA or CAH thickness. The courses of the film thickness distribution for CAH correspond well to the classical theory of non-slip hydrodynamic lubrication. The difference in the contact angle between the material CrN/AlN/…/CrN/AlN and AlTiN/CrN/Cr/…/CrN/Cr is CA = 35.2°. In the case of sliders made of steel X90CrMoV18 and AlN/CrN/…/AlN/CrN, the difference is CA = 5.5°. The Cr coating has a CA = 56.2° and a CAH of 25.1°. The SiO2 coating has a CA lower by 7.9° than the CrN/AlN/…/CrN/AlN coating.
The thickness of the lubricating film layer for the oil produced by selected sliders: at different speeds is shown in Figs. 8 and 9. The presented results prove that the CAH more closely reflects the relationship of the kinematic node for the effect of hydrodynamic lubrication produced by various sliding surfaces. This proves that CAH allows better establishment of hydrodynamic lubrication conditions between two surfaces. In this arrangement, CA is worse. In assessing the credibility of introducing the results of experimental research into mathematical models related to hydrodynamic lubrication, in assessing hydrophobic and hydrophilic properties, it is very important. Therefore, CAH gives a greater chance of credibility of changes in the oil film thickness in the elements of the cooperating kinematic pairs of the engine. As CA gives greater deviations from the values of theoretical models and approximation functions.
The results of sliders coated with steel X90CrMoV18, AlTiN/CrN/Cr/…CrN/Cr and AlN/CrN/…/AlN/CrN correlate very well with the classical theory of non-slip hydrodynamics for both 1 and 2 N loads. of the CrN/AlN/…/CrN/AlN slider is, however, significantly lower than for all sliders. The values of the film thickness in relation to the speed are characterized by a significant dispersion of values and non-uniformity of the course. This coating has hydrophobic properties, while 3 coatings have hydrophilic properties. Between them there are oil film thickness distributions for Cr and SiO2. However, they have a more even distribution of film thickness values relative to the speed of the slider. The difference in the thickness of these layers resulting from different surfaces. In this case, it corresponds well with their CAH, but not with the contact angle CA. In the author's opinion, this is the answer which parameter is more important in improving the model of the hydrodynamic theory lubrication. In addition, the results shown in Fig. 4.5, 8 and 9 indicate an unexplained phenomenon where the thickness of the film produced by the CrN/AlN/.../CrN/AlN slider with 99% wt. glycerol or oil is much lower than the theoretical full slip values. It is difficult to explain this phenomenon of stochastic course of values for hydrophobic coatings.
In the work [43], a detailed analysis of the influence of the non-wetted, stationary surface of the sliding object on the hydrodynamic properties was carried out using the model of critical shear stresses. In this work, the conditions of boundary slip were defined: full slip (τc = 0), one-way slip (finite-valued constant τc applied to the entire static surface of the slider) and directional slip (slip or no slip and slip direction depended on the local pressure gradient at the boundary). The tests were carried out on the basis of one-dimensional flow. Studies of this type on two-dimensional flows are presented in [44]. They describe changes in the dimensionless load capacity W* where (\({Wh }_{0}^{2}\)/(Uη\({B}^{2}\)L) with respect to the dimensionless critical value of the shear stress τc* (h0 τc /Uη) for different inclinations of the rubbing pairs.
Large critical shear stresses τc*>1 correspond to non-slip conditions and the resistance curves approximate Reynolds load values. The size of the ability to transfer the hydrodynamic load, i.e. to create a lubricating film, decreases when the limit slip begins on the stationary surface of the slider covered with any material. The disappearance of the hydrodynamic effect in the initial phase proceeds very quickly with increasing slip, which is indicated by the decrease in τc*. Soon this phenomenon is reduced to a minimum and the lubricating film-forming capacity increases again to further reduce τc*. Such a description is particularly important in the case of correcting the slip values for various materials used for the elements of kinematic pairs of internal combustion engines. This is the basic condition for the planned shaping of the oil film in terms of surface coverage and the thickness of the lubricating film obtained.
Figure 1 shows that the thickness of the lubricating film layer generated by the CrN/AlN/.../CrN/AlN slider with 65% wt. glycerol solution coincides with the theoretical full slip curve (i.e. τc = 0). This means that the critical shear stress of an EGC slider surface lubricated with 65% wt. values that lead to a significant reduction of the hydrodynamic effect, i.e. load support, as shown in Fig. 9. As a result, the thickness of the lubricating film layer formed by the CrN/AlN/.../CrN/AlN slider with 99% wt. glycerol or oil is much less. Under such conditions, the direction of lubricant slip in the pre-surface area of the slider is directed towards the inlet, which results in reduced grease pick-up and leads to a lower thickness of the lubricant film than under full slip conditions. The two glycerol samples have similar chemical properties, but a large difference in dynamic viscosity. In this case, 99% by weight of glycerol has a higher viscosity. Greater Critical Shear Stress 99% weights of glycerol on the surface layer of the CrN/AlN/.../CrN/AlN slider material can be attributed to its higher dynamic viscosity with respect to 65% by weight. glycerol.
The results of the experiment for selected sliders with different surface materials show the influence of surface properties of various materials in terms of CA and CAH on hydrodynamic lubrication. The ability of the hydrodynamic formation of a lubricating film is related to the adhesive force between the liquid and the solid surface. It takes place under conditions of fluid friction in the separation of cylinder walls, piston rings and piston. The conditions of mixed friction and the values of generated forces depending on the operating conditions are not taken into account here. Lubricant particles are able to slide or relative to any surface of the coating applied to the engine component only when these particles overcome the energy barrier. Its value depends on the adhesion of the lubricant particles and the coating. These parameters are determined using CAH and CA. The size of the energy barrier depends on the interfacial properties of the coating and the lubricant.
In paper [45], based on the basic principles of thermodynamics, the energy barrier equation was derived. It is expressed using CA and CAH:
$$E=\frac{R}{{2}^{\frac{7}{3}}}{\left(CAH\right)}^{2}f\left(\theta \right)$$
1
,
Where:
$$f\left(\theta \right)=\frac{{\left(1+cos\theta \right)}^{2}}{{\left(1-cos\theta \right)}^{1/6}{\left(2+cos\theta \right)}^{4/3}}$$
2
Calculations of the energy barrier E can be made using the parameters θ and CAH. However, the value of this parameter does not change significantly for the range from 20° to 140°. The parameter f(θ) practically remains unchanged in this range. To a large extent, the value of the energy barrier is due to the CAH. In the case of materials used in the construction of kinematic elements of internal combustion engines, it is assumed that a contact angle greater than 90° means that the surface of the material is hydrophobic. Therefore, for the operating conditions of combustion engines and the maximum piston speeds achieved, which are temporarily much higher than in the test, the hydrophobic properties of the coatings do not necessarily have to be worse in terms of the formation of a lubricating film than for the hydrophilic coatings.
Based on the formula (1), it is established that the smaller the CAH, the lower the barrier value. The main reason for this condition is the molecular interaction between the lubricating liquid and the surface layer of the coating. Limit slip occurs only above CA 140°. Slip length increases also occur above this value. A number of works on the methodology of research to assess the validity of the use of CA and CAH are given in [47–52]. According to the author, the research methodology adopted and the results obtained prove the significant potential of the theory of material selection in terms of CA and CAH in industrial use in internal combustion engines in order not only to obtain durability of these assemblies and low wear, but also to significantly reduce hydrodynamic friction losses occurring between main components of internal combustion piston engines.