Numerical Simulation and Experimental Study on Sealing Performance and Frictional Property of Rotary Lip Seal

,e hydrodynamic theoretical lubrication model of the friction pair between the rotary shaft and the lip seal under the state of full film lubrication was established in this paper. ,e Reynolds equation was solved by using the finite difference method, and the influence of the viscosity-temperature characteristics of the lubricant was taken into account in the solution process. ,e distribution of the film thickness and the hydrodynamic pressure in the sealing area was obtained. At the same time, the bench test was carried out and the correctness of the model was verified by comparing the simulation results and test results of reverse pumping rate and friction torque under different rotational speed of the shaft. ,e microasperity of the lip surface is a necessary condition for achieving the sealing effect. ,erefore, the influences of the contact load of the seal and the root mean square deviation of the lip surface on the sealing performance and frictional property were analyzed by using the theoretical model. ,e analysis results show that the sealing performance and frictional property can be changed by changing the contact load and surface roughness of the lip, but a single increase in the influence of a certain factor cannot achieve good results, and comprehensive consideration is required in product design.


Introduction
Rotary lip seal is an indispensable form of sealing for media seal of transmission shaft, and its sealing performance is related to whether the machine can operate normally. Compared with other sealing methods, the rotary lip seal has the advantages of simple and compact structure, reliable performance, and excellent follow-up [1]. It is widely used in petrochemical machinery, vehicles and ships, aerospace, mining machinery, and agricultural machinery. It is one of the most common seals used at present [2].
Rotary lip seal realizes the sealing of lubricant through its reverse pumping effect. e reverse pumping effect is a unique phenomenon of the lip seal, which prevents the oil from leaking to the air side by sucking the oil back to the oil side.
e reverse pumping mechanism believes that the hydrodynamic lubrication film will be formed between the lip of the lip seal and the surface of the shaft within the contact zone when the shaft rotates steadily. It is closely related to the microasperity of the lip surface. e shear stress of the oil film and the friction between the microasperity and the shaft when the shaft is rotating will cause shear deformation of the microasperity of the lip surface, coupling with the asymmetrical distribution of the contact pressure made by the asymmetric macrostructure of the lip seal, so that the microasperity of the lip surface will pump the lubricant from the air side back to the oil side like a screw pump, thereby realizing zero leakage [3][4][5]. e capacity of reverse pumping directly affects the sealing performance of the rotary lip seal.
As the working conditions of modern machinery develop in the direction of high temperature, high speed, and high pressure, rotary lip seals are facing more stringent performance requirements such as zero leakage, low friction, and long life. erefore, continuous research on the lubrication and sealing performance of rotary lip seals is of great significance and has attracted widespread attention from scholars at home and abroad. With the development of computing technology, numerical simulation has gradually become an important research method. Scholars have established numerical models or carried out experiments to study the formation of the film between the two surfaces of lip seal and shaft [6][7][8][9][10] and study the influence of morphology of the asperities on the surface of the lip [11][12][13][14][15][16], the surface morphology of the shaft [17][18][19], the structural parameters of the lip seal [20], and the misalignment of the lip seal and shaft [21] on the sealing performance. Some scholars have also carried out experimental studies to explore the changing laws of the sealing performance under different operating conditions [22], the microstructure of shaft surface [23][24][25], and other factors. Studies have shown that there are two main aspects to evaluate the sealing performance of a lip seal: reverse pumping rate and friction torque. e reverse pumping rate is the key to the realization of zero leakage of the lip seal, and the friction torque reflects the degree of wear of the lip seal, which is two important factors for evaluating the performance of the lip seal.
ere are many factors that affect the performance of the lip seal, but the final factor can be attributed to the distribution of the fluid pressure in the sealing area.
erefore, reasonable distribution of the flow field is very important to the sealing performance of the seal. Taking the friction pair of the rotary shaft and lip seal as the research object, a hydrodynamic lubrication model was established where the microasperities of the lip surface were simulated as cosine function and the influence of the viscosity-temperature characteristics of the lubricant was considered, and the distributions of film thickness and the hydrodynamic pressure in the sealing area were obtained by a numerical solution in this paper. At the same time, a bench test was carried out to verify the model. e correctness of the numerical model was verified by comparing the calculation results and test results of reverse pumping rate and friction torque at different speeds. en, the influences of different contact forces of the lip seal and the surface roughness of the lip on the reverse pumping rate and friction torque were calculated and analyzed through the numerical model, which have important theoretical guidance for the prediction of the performance and service life and structural design of the lip seal.

Hydrodynamic Lubrication Model
A hydrodynamic lubrication model of the rotary lip seal is proposed based on the following basic assumptions: (1) e two surfaces are fully film lubricated due to the effect of hydrodynamic pressure during the stable operation and do not consider contact. (2) e shaft is regarded as completely rigid and has no axial movement; the lip seal is completely centered and completely elastic and has a uniform temperature. (3) e lubricant is a Newtonian fluid and the flow is laminar. It can be considered that the density and viscosity of the lubricant remain unchanged in the thickness direction of the oil film because the film thickness is very thin. (4) Do not consider changes of hydrodynamic pressure p along the direction of the film thickness. e film thickness is much smaller than the radius of curvature of the lip seal and the shaft, so the effect of the curvature of the friction pair is not considered.
e schematic diagram of the contact area model of the lip seal at any position in the circumferential direction is presented in Figure 1, where x represents the circumferential coordinate and y represents the axial coordinate. e microasperity topography of the lip surface is simulated by a two-dimensional cosine form of periodic distribution. e calculation area is taken as the contact width L in the axial direction and the period length B in the circumferential direction and divided into 51 × 51 grids, and the external loads on each grid are assumed to be equal.

Reynolds Equation.
A stable film is formed in the sealing area between the shaft surface and the lip surface when the lip seal is in a stable operation. e hydrodynamic lubrication control equation of the film in the contact area is the Reynolds equation and can be written as [6] in which Φ x and Φ y are pressure flow factors, and their physical meaning is the degree of obstruction of asperities to the fluid in flow driven by the pressure difference. For isotropic surfaces, Φ x � Φ y . Φ s is shear flow factor; its physical meaning is the influence of additional flow generated when rough surfaces slide relative to each other. ey can be obtained by the empirical formulas of Patir and Cheng [6], as shown in where H represents the dimensionless film thickness, defined as H � h/σ, σ represents comprehensive roughness of the two surfaces, defined as σ � ������ σ 2 1 + σ 2 2 , σ 1 and σ 2 represent the root mean square deviation of the surface roughness of the lip and the shaft, respectively.

Film ickness Equation.
e surface topography of the shaft is negligible compared with that of the lip. e film thickness between the lip seal and the shaft is superimposed by the initial microasperity f 1 (x, y) of the lip surface, the axial curvature of the lip f 2 (y), and the average film thickness h avg (t). e film thickness expression is given by (4) e periodic two-dimensional cosine form is considered to define the initial microasperity of lip surface, which is defined by the following expression: where h 1 is the wave amplitude of the lip seal surface, N x and N y are the number of periods of the lip surface in the x and y directions, and d x (y) is the circumferential shear deformation of lip surface, defined by d x (y) � D 1 cos − y − y min y min cos −1 (Δy) , 0 ≤ y ≤ y min , D 1 cos π 2 1 − y min y − y min , y min ≤ y ≤ L, where Δy is the tangential deformation of the oil side relative to the maximum tangential deformation, D 1 is the ratio of the maximum tangential deformation to the undulation period in the x direction, and y min is the axial position where the initial average film thickness is the smallest. e axial curvature of the lip is defined in the form of cosine, as in where h 2 is the maximum film thickness in the axial direction.

Boundary Conditions.
Reynolds boundary conditions are used as follows: 2.4. Load Capacity of Film. e load capacity of film and external load keep balance under the condition of hydrodynamic lubrication. e load capacity is equal to the integral of the pressure p in the entire range of film, which can be obtained by 2.5. Reverse Pumping Rate. Once the distribution of the fluid pressure is determined, the reverse pumping rate can be calculated by equation (10). If Q is a negative value, it indicates that the oil leaks from the oil side to the air side; if Q is a positive value, it indicates that the oil is pumped from the air side to the oil side.
2.6. Friction Torque. e friction torque is defined as the product of the fluid friction and the radius of the lip seal within the contact width. e friction torque determines the service life of the lip seal. It can be calculated by formula (11):

Numerical Solution.
e Reynolds equation is solved numerically using the finite difference method in this study. First, the Reynolds equation (1) is nondimensionalized and then discretized to obtain a linear equation system. A uniform grid is used, and the grid size is 51 × 51. e relaxation iteration method is used for loop iteration which has better convergence and faster convergence speed, and the iteration expression is obtained as equation (12). e relaxation factor is selected as ω′ � 0.7 based on calculation experience. e calculation process is shown in Figure 2. where

Test Equipment.
e bench test was carried out on a selfmade lip seal testing machine, and its main structure is shown in Figure 3. e main technical parameters of the testing machine are ① the speed range of the spindle: Advances in Materials Science and Engineering 3 300∼8000 r/min; ② the maximum output torque of the motor: 20 Nm; ③ the radial runout of the spindle: less than 0.003 mm. e main function of the test equipment is to test the performance of the rotary lip seal during operation, including the friction torque, pressure of oil chamber, temperature of oil chamber, leakage, and other parameters of different specifications of lip seals, which are used to study the frictional property and sealing performance of the lip seal. e main composition and working principle of the testing machine: the testing machine is mainly composed of a main engine, an electric control cabinet, a lubricant source for the main shaft, a computer, and a lubricant source for the oil chamber. e motor can achieve stepless speed change from 300 to 8000 r/min through the frequency change of the frequency converter. e oil chamber is welded with stainless steel, and it is equipped with an oil inlet valve, a bleed valve, an oil return valve, and two temperature sensors, a pressure sensor and a torque sensor. Two temperature sensors are used to measure the temperature of the lip seal and the temperature of the oil chamber, respectively, the pressure sensor is used to measure the pressure in the oil chamber, and the torque sensor is used to measure the friction torque between the lip seal and the rotary shaft specimen. e lubricant source for the oil chamber is composed of an oil tank, an oil pump motor unit, a directacting relief valve, a high-temperature needle valve, and so on. e hydraulic oil pumped by the oil pump enters the oil chamber through the valve block and the oil inlet valve, and it indicates that the oil is full when the oil overflows through the bleed needle valve and then closes the bleed needle valve. e direct-acting relief valve can be adjusted from low to high to the required test pressure. e bleed needle valve should be opened and the oil pump motor should be stopped when the pressure test is not needed. e flow rate of the hydraulic oil is 2.5 L/min, and the pressure is 0-1 MPa. e electric control cabinet is mainly used to control the opening and closing of the frequency converter, the frequency conversion speed regulating motor, the lubricant pump of the main shaft, and the oil supply pump of the oil chamber, whose signal line is connected with the computer to realize the automatic control of the experimental process, data display and processing, and overlimit protection function in the experiment process. e test software matched with the hardware system of the testing machine can realize the functions of experimental parameter setting, parameter testing, display of dynamic data and graphics, and export of experimental results.

Sample Preparation.
Studies have shown that if the surface of the shaft is too rough or too smooth, the lip seal will fail. e American Rubber Manufacturers Association, German standard DIN3760/3761, and international standard ISO6194/1 have stipulated the range of roughness of shaft surface. e ISO6194/1 requires that the seal contact surface of a ground shaft shall be finished to a surface roughness, measured in the axial direction of between Ra 0.2 μm and Ra 0.5 μm and between Rz 1.2 μm and Rz 3.0 μm [26]. erefore, the outer surface of the rotary shaft sample was designed to be ground with a roughness Ra of about 0.4 μm and Rz of less than 3.0 μm. e hardness of the shaft surface reaches HRC 55-60 after high-frequency quenching, which was measured on the HBRVU-187.5 optical hardness tester. e base material of the test rotary shaft is 45# steel, and its size is Φ50 mm × 35 mm, as shown in Figure 4(a). e surface roughness of the shaft was measured by the HT-SURF 10000 surface profiler. Figure 4(b) shows the twodimensional profile curve of the shaft surface. e two-dimensional roughness values of the shaft surface are Ra � 0.345 μm and Rz � 2.798 μm obtained by multiple measurements and taking the average value, which meet the standard requirements. e material of the lip seal sample is NBR (nitrile rubber), the specification is TC50 mm × 72 mm × 8 mm 4 Advances in Materials Science and Engineering (inner diameter × outer diameter × width), and the range of applicable temperature is −40∼120°C. e lubricant is L-HL46 hydraulic oil, whose kinematic viscosity is 45.2 mm 2 /s at 40°C and 6.5 mm 2 /s at 100°C. e density is about 0.87 g/cm 3 .

Test Process.
In order to fully consider the influence of the speed, the speed of the spindle was selected as r � 1000 r/min, 1500 r/min, 2000 r/min, 2500 r/min, 3000 r/min, 3500 r/min, and 4000 r/min. Since the testing machine has no heating function, the initial temperature of all tests is the ambient temperature of 25 ± 2°C. e surface of the rotary shaft sleeve sample was matched with the surface of the lip seal, and the test was carried out at different speeds for 120 minutes. e friction torque, temperature rise, and reverse pumping capacity of the friction pair corresponding to different speeds were measured, and the reverse pumping rate was calculated.   Advances in Materials Science and Engineering e detailed experimental steps are as follows: (1) Mounting the sample: the lip seal was installed in reverse on the sample holder which can limit it in the axial and radial direction, and the sample holder is installed on the end face of the oil chamber by bolts after alignment. en the rotary shaft sleeve specimen was installed on the main shaft and tightened with a nut for axial fixation. e oil chamber was moved to the left by turning the handle to the designated position where the lip seal was in contact with the surface of the rotary shaft sleeve specimen, and the locking screw was tightened to lock the moving table to prevent the position from changing during the experiment. (2) Power on: power on the electric control cabinet, turn on the computer, and enter the software interface to check whether the data displayed by each sensor were normal and whether there was an alarm signal. (3) Oil filling: open the oil inlet needle valve and the bleed needle valve, close the oil return needle valve, adjust the direct-acting relief valve to the lowest pressure, and press the "experimental oil pump on" button, and then the system starts to inject oil into the experiment chamber. It indicated that the oil in the cavity was full when it was found that there was oil flowing out of the oil pipe of the bleed needle valve, and the oil pump was turned off at this time. e level of the hydraulic oil in each test is consistent, which is subject to the filling of the oil chamber. (4) Setting the parameters and starting the experiment: set the information of the experiment, such as the alarm parameters, the duration of the experiment, the speed of the spindle, and the control mode, and then perform the experiment.

Measurement of the Temperature of the Seal Contact
Area. It is difficult to directly measure the temperature of the contact area between the lip seal and shaft because there is relative movement between them, the contact width is only a few tenths of a millimeter, and the thickness of the film is as low as micrometers. Many scholars have adopted different measurement methods, such as perforating and burying a thermocouple in the lip near the contact area, using the oil temperature in the oil chamber to approximate the temperature of the contact area, using an infrared thermal imager to measure the temperature, and using the temperature of the shaft end to represent the temperature of the contact area. ere are two temperature sensors on the testing machine in this study: one is installed on the oil chamber to measure the temperature of the oil chamber and the other is installed near the lip seal to measure the temperature of the oil seal. e measurement results of the temperature will be dynamically displayed on the interface of the supporting software during the experiment. e test results show that the temperature of the oil in the oil chamber is lower than the temperature of the lip seal, so it is more reasonable to regard the measured temperature of the lip seal as the temperature of the contact area, but there may be some errors in the temperature of the real contact area.

Measurement of Friction Torque.
Friction torque is one of the key parameters for evaluating the sealing performance of rotary lip seal. e measurement of friction torque is mainly completed by the torque sensor of the testing machine and the test software. e torque sensor is connected to the computer, so the friction torque is displayed in real time during the whole operation. e initial temperature of the test is the ambient temperature of 25 ± 2°C. e friction torque and lubricant temperature change dynamically as the machine runs. e change rule of the friction torque with time contains the influence of the temperature change. It must be explained that the value of the friction torque discussed below is the value when its change is steady, and the lubricant bath temperature is the temperature corresponding to the time when the torque change is steady.

Measurement of Reverse Pumping Rate.
Generally speaking, there are two main methods for measuring the reverse pumping rate which are the weighing method and the oil drop method. e lubricant is continuously supplied and almost the same conditions of oil supply are achieved in all tests in the former, while the injection of oil droplets is more error-prone and the result may be affected by the operator's operation in the oil drop method. erefore, the weighing method was used to measure the reverse pumping rate in this study and the specific test process was as follows: the lip seal was installed in reverse, and the measured leakage was the reverse pumping capacity which can be known from the sealing mechanism described above. e oil sucked by the reverse pumping was collected by a beaker placed under the sample holder, and then the volume was measured with a small-capacity measuring cylinder. e bottom of the lip seal was exposed to the oil side when the lip seal was installed in reverse and the oil chamber was filled with oil, so the continuous supply of lubricant could be realized. e oil pumped could be collected in the beaker after a certain amount of time, and it flowed down the sample holder and dripped into the beaker only when enough oil is pumped. It started timing until the end of the experiment when the reverse pumping phase began and oil was observed to flow out of the sample holder, and the total time was recorded as t. Pour the oil collected in the beaker into a smallcapacity graduated cylinder to measure the total volumetric pumping capacity denoted as m. e volumetric reverse pumping rate is equal to the pumping capacity divided by the total pumping time.

Results and Discussion
It points out in the literature [27] that the film thickness h in the contact area of the rotary lip seal during operation is about 0.1∼1.0 μm and may reach 10 μm under large eccentricity; the contact width of the lip L is generally 0.10∼0.15 mm and increases to 0.2∼0.3 mm after 500∼1000 hours of operation; the contact load of the new seal F is in the range of 0.10∼0.15 N/mm, and experience shows that the residual contact load of 0.05 N/mm can maintain an effective seal [27]. But some scholars have measured a larger magnitude of film thickness; for example, Poll and Gabelli measured film thickness as high as 9.5 μm when the speed is 6 Advances in Materials Science and Engineering 1.4 m/s [9], and Van Leeuwen and Wolfert measured the oil film thickness from 1 μm at 0.035 m/s to 4.5 μm at 0.35 m/s [10]. erefore, the assignment of the initial value of the average film thickness is based on comprehensive consideration of the experiment results of Poll and Van Leeuwen. e parameters of the sealing system studied in this paper are as follows: the diameter of the rotary shaft D � 50 mm; the contact width of the sealing area L � 0.12 mm; the length of the circumferential area B � 0.1 mm; the initial average film thickness h avg � 4 μm; the environmental pressure p a � 0.1 MPa; the sealing pressure p s � 0.1 MPa; the contact load F � 0.05∼0.25 N/mm. e reverse pumping rate and the friction torque are two important factors for evaluating the sealing effect and service life of the lip seal. erefore, the above two parameters were selected as the research object to discuss the influence of viscosity of lubricant, rotational speed, contact load, and the surface roughness of lip surface.

Changes in Viscosity.
In actual working conditions, the viscosity of the lubricant will drop sharply with the increase in temperature when the machine keeps running, especially at high rotational speeds. e change in viscosity will significantly affect the pressure distribution of the oil film, resulting in different reverse pumping rates and friction torque. In order to simulate the real working conditions more accurately, the temperature change of the lubricant at different rotational speeds was measured, while the machine is running during the test. Figure 5 shows the change law of the temperature of lubricant when running for 120 minutes at 1000 r/min. Figure 6 shows the change law of the temperature of lubricant at different speeds, where the temperature at each speed is the temperature that changes relatively smoothly during a period of operation. Figure 7 shows the variation of the viscosity of the No. 46 lubricant with the rotational speed obtained by using the viscosity-temperature characteristics of the lubricant.

Distribution of the Film ickness and the Hydrodynamic
Pressure. Bringing the above parameters into the numerical model of the hydrodynamic lubrication model shown in Figure 1, the distribution of the film thickness and hydrodynamic pressure is obtained when h avg � 4 μm, r � 1000 r/ min, and F � 0.1 N/mm. Figure 8 shows the distribution of film thickness in the contact zone, and Figure 9 shows the distribution of hydrodynamic pressure in the contact zone. It can be seen that the maximum fluid pressure is located at 0.3 mm in the direction of the contact width, close to the oil side, which is a necessary condition for achieving the reverse pumping effect according to the sealing mechanism of the lip seal. Figure 10 shows the calculation results and test results of the change law of reverse pumping rate of the lip seal in the rotational speed range of 1000 to 4000 r/min. It can be seen that both indicate Advances in Materials Science and Engineering 7 that the reverse pumping rate increases with the increase of rotational speed, and the growth trend is basically linear. A large number of studies have shown that the reverse pumping rate is related to the speed of the shaft, but it is not reflected directly in formula (10). In fact, the influence of the speed is implicit in parameter h. e hydrodynamic pressure effect is enhanced, and the hydrodynamic support increases when the rotational speed of the shaft increases. Large support will create a large gap; therefore, the film thickness increases with the increase of the rotational speed, thereby increasing the reverse pumping rate. e variation of friction torque with rotational speed is shown in Figure 11. Both theoretical calculations and test results show that the friction torque increases as the speed increases within the studied range, and the increase trend of friction torque gradually slows down when the speed exceeds 2500 r/min. It can also be seen from equation (11) that the friction torque is proportional to the product of the viscosity of the lubricant and the speed of the shaft. e influence of the speed plays a major role when the speed is low; however, the viscosity of the lubricant decreases with the increase of the speed when the speed is increased, and the influence of the viscosity on it increases gradually. e correctness of the hydrodynamic model of the lip seal is verified by the bench test. It can be seen that the changing trend of the theoretical values of reverse pumping rate and friction torque at different speeds is consistent with the experimental data generally from Figures 10 and 11, but there are differences in the consistency of specific values. e main reason for these differences is that, on the one hand, the amount of oil reverse pumped during the test is small, and there are certain errors in collection and measurement due to the limitation of the experimental instrument. On the other hand, the calculation results of the theoretical model are subject to the influence of the setting of some initial values of parameters and the idealized assumption of the operating state, and the model need be further optimized later.   e change laws of the average film thickness, reverse pumping rate, and friction torque when the contact force of the lip seal changes from 0.05 to 0.25 N/mm at 1000 r/min of speed are shown in Figures 12-14 separately. It can be seen from Figure 13 that the reverse pumping rate Q decreases as the contact force F increases. e reason is that high contact force leads to increased pressure in the gap of the seal, and fluid particles must overcome higher pressure to reach the air side from the oil side. At the same time, the film thickness in the contact zone decreases with the increase of contact force which can be seen from Figure 12, which leads to a decrease of flow from the air side to the oil side. It can be seen from Figure 14 that the friction torque T increases as the contact force F increases and the magnitude of the increase decreases gradually.

e Influence of Rotational Speed.
is is because the average film thickness decreases with the increase of contact force, resulting in an increase in viscous shear friction of fluid.

e Influence of the Surface Roughness of the Lip.
As can be seen from Figures 15 and 16, the numerical calculation results show that, within the range of research, the reverse pumping rate increases, while the friction torque decreases with the increase of the root mean square deviation of the lip surface, indicating that the sealing performance can be changed by changing the surface roughness of the lip. e trend of theoretical calculation is consistent with the results of Horve's test. Horve proved that the seal that has rough wear tracks with abundant microasperities provides better reverse pumping rates and excellent service reliability and  Advances in Materials Science and Engineering the smooth lip surface with no microasperities provides poor reverse pumping rates by experiments [11]. Obviously, the lip surface with abundant microasperities has greater surface roughness, while the smooth lip surface has smaller surface roughness. Reverse pumping ability and service reliability of the lip seal could be improved by artificially roughening the lip surface or changing the elastomeric material to provide the formulations of microasperities. But actual experience tells us that it will significantly increase the wear of the sealing ring and affect its service life if the surface roughness of the lip surface increases too much. erefore, comprehensive consideration is required in product design.

Conclusion
(1) A numerical model for hydrodynamic lubrication of the interface between the rotary shaft and the lip seal was established in which the microasperities of the lip surface were simulated by a periodic two-dimensional cosine form and the influence of the change of lubricant viscosity was considered in the analysis. e distribution of film thickness and hydrodynamic pressure in the contact area was obtained by solving the model numerically.
(2) e reverse pumping rate and friction torque were selected which are the two most important parameters for evaluating the performance of the lip seal as the calculation output, and the correctness of the model was verified by carrying out a bench test. (3) Rotational speed affects the reverse pumping rate indirectly by affecting the film thickness. In the range of research we did, the film thickness increases, and the reverse pumping effect is enhanced as the rotational speed increases. e friction torque increases with the increase of the speed. e friction torque is proportional to the product of the lubricant viscosity and the shaft speed. e influence of the speed plays a leading role at low speed, and the influence of viscosity increases when the speed increases. (4) e contact load of the seal and the root mean square deviation of the lip surface were analyzed by using the theoretical model verified. e analysis results show that the sealing performance can be changed by changing the contact load and surface roughness of the lip, but a single increase in the influence of a certain factor cannot achieve good results, and comprehensive consideration is required in product design.

Nomenclature
x: Radial rectangular coordinates y: Axial rectangular coordinates h: Film thickness p: Fluid pressure t: Time σ: Comprehensive roughness of the two surfaces σ 1 : Root mean square deviation of the surface roughness of the lip σ 2 : Root mean square deviation of the surface roughness of the shaft µ: Dynamic viscosity of fluid U: Linear velocity of shaft

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Advances in Materials Science and Engineering Δy: e tangential deformation of the oil side relative to the maximum tangential deformation D 1 : e ratio of the maximum tangential deformation to the undulation period in the x direction y min : e axial position where the initial average film thickness is the smallest h 2 : e maximum film thickness in the axial direction W: e load capacity of the film Q: Volumetric reverse pumping rate T: Friction torque ω': Relaxation factor k 1 : Iterative times D: Diameter of the rotary shaft r: Rotational speed of the shaft Pa: Environmental pressure Ps: Sealing pressure F: Contact load.

Data Availability
e data used to support the findings of this study are included within the article.

Conflicts of Interest
e authors declare that there are no conflicts of interest regarding the publication of this paper.