Research Article  Open Access
A Model of Surface Residual Stress Distribution of Cold Rolling Spline
Abstract
Residual stress is an important parameter in the evaluation of the performance of a cold rolling spline surface. However, research on cold rolling spline is rare. To improve the surface property of a spline, an involute spline is selected as the object of this study. The contour method for determining cold rollbeating residual stress involves measuring the force spatial distribution, performing a statistical analysis of the experimental results, establishing the parameters for the tooth profile for different positions (dedendum, pitch, and addendum) of residual stress, and determining the effect of pressure on the relationship between stress and the depth of the cold rollbeating. A response surface method is used to establish the spline tooth profile of the dedendum, pitch, and addendum of the residual stress and different depths of the stress layer to obtain the parameters of a multiple regression model and perform a comparative analysis of the experimental and prediction results. Research indicates that the prediction results have high reliability. The establishment of this model has important guiding significance to control the residual stress in the cold rollbeating forming process, optimize the cold rollbeating processing parameters, and improve the surface properties of cold rolling spline.
1. Introduction
Cold rollbeating technology is a new type of chipless nearnet forming technology that enables environmental protection and energy savings with high efficiency, a high material utilization rate, and an extensive application value in the automobile industry and the aerospace sector and for major strategic equipment manufacturing processes. Highspeed cold roll forming is a progressive forming process during nonuniform thermal mechanical coupling. The forming process of a workpiece surface will inevitably produce residual stress. Residual stress can reduce the surface microcrack expansion of a workpiece and increase its fatigue strength, which will affect the stability of the workpiece size [1–5]. Residual stress is an important parameter for the surface performance of a workpiece, and its type and peak size and depth of the working layer are important factors that affect the surface properties of coldrolled workpieces. However, various questions arise during the actual production process. How do different cold rollbeating process parameters affect the workpiece residual stress state and its distribution? What method can be employed to predict the surface residual stress of a cold rollbeating workpiece when setting the cold rolling process parameters? What method can be employed to optimize the cold rollbeating process parameters according to the stress state of the workpiece application? Research on the spatial distribution and prediction model of the residual stresses in cold rollbeating during nonuniform thermal mechanical coupling is necessary. Providing accurate control of residual stress during cold rollbeating and optimization of the cold rollbeating processing parameters improve the surface performance of cold rollbeating workpiece forming and have theoretical significance and high engineering application value.
In recent years, domestic scientists have investigated the cold rollbeating plastic forming process using modern numerical simulation. Cui [6] employed a rigid plastic numerical simulation method for a cold rolling forming spline shaft finite element analysis and provided a preliminary description of the cold rollbeating process. The spline shaft in the forming process was determined to be prone to collapse in front of defects, and the causes for collapse were determined from an angle of deformation force analysis of mechanics. Cui [7] analyzed the highspeed cold rollbeating of an involute spline by studying the relationship between cold rollbeating and workpiece forming motion using a mathematical model of the forming process of the dynamic response and stress wave. The cold rollbeating process of metal flow law and deformation mechanism were determined from a macro perspective. Quan et al. [8] employed an explicit central difference algorithm and the finite element software ANSYS/LSDYNA; the numerical simulation of an involute spline shaft’s cold rolling forming was realized according to the calculated results. The metal flowing law, the von Mises stress, and the formed outer diameter of an involute spline were forecasted; the errors between the simulation results and the dentiform object of the involute spline were analyzed. Cui et al. [9–11] employed a forming method to design and manufacture rollers without an inaccurate outline and constructed a math model of rollers outline design, in which the experimental method was applied to correct the theoretical outline of rollers. They developed a simulation system of rollers, verified the correctness of the design and manufacture of rollers, and performed a series of process experiments of an actual spline shaft, which caused the formation of coldbeating to attain higher machining precision. Li et al. [12] determined the parameters of the JohnsonCook dynamic constitutive equation for 40Cr using experimental methods, predicted flow stress based on the constitutive equations, and compared the real stress with the experimental data. Based on the comparisons, the true stress calculated based on the model and the predicted flow stress are both consistent with the experimental data, which conclude that the presented dynamic constitutive model can effectively predict the plastic flow stress for 40Cr quenched and tempered steel. According to the principle of an involute spline cold rollbeating, Cui et al. [13] established the contact model between the rollers and the spline shaft blank in the process of cold rollbeating forming via FEM simulation. They investigated the formation mechanism of the involute spline tooth profile in the cold rollbeating forming process and analyzed the node flow tracks of the deformation area. Experimental research on the metal flow of a cold rollbeating spline is conducted; the results conclude that the particle flow directions of the deformable bodies in a cold rollbeating deformation area are determined by the minimum moving resistance. Cui and others [14] established a finite element model for cold rollbeating simulation based on the thermal effect in different roller speeds. Based on the simulation results, the change in equivalent stress due to the thermalmechanical mechanism was analyzed, and its influence on work hardening was determined. Zhang and others [15] amended the analytical equation based on the principal stress method of cold rolling processing deformation force analysis solution via a simulation analysis. In the field of residual stress, Valiorgu et al. [16] developed a new methodology to predict residual stresses induced in the finish turning of an AISI304L stainless steel. Navas et al. [17] measured the surface residual stresses in AISI 4340 steel bars that were subjected to turning tests via Xray diffraction using different cutting speeds and cutting feeds and cutting tools with different nose radii and surface states. They determined not only the magnitude but also the orientation of the principal residual stresses. Jiang et al. [18] established a finite element model using elasticplastic theory and discussed the effect of the original hardness of the workpiece, the geometry of the cutting tool, and the cutting conditions on the spatial distribution of the residual stress on the formed surface. Sun et al. [19] established a threedimensional finite element model of machining and obtained the variation of surface residual stress with the process parameters via the cutting process parameter design. They discussed the impact of first cutting and second cutting on residual stress formation based on the simulation of different processing procedures. They also performed a cutting experiment to verify the accuracy of the finite element simulation. Capello [20] established an empirical relationship between the residual stress and the machining parameters using experimental data. Ulutan et al. [21] established a prediction model of residual stress during thermomechanical coupling based on an analysis of existing models. Lazoglu et al. [22] employed elasticplastic mechanics theory to establish a prediction model of residual stress based on the consideration of the comprehensive thermal and mechanical effect on the workpiece surface and the stress relaxation problem. Guo [23] employed a numerical simulation method to study the residual stress distribution of different materials. Ding [24] simulated an ultraprecise cutting process, proposed an algorithm that is suitable for measuring the residual stress on the cutting surface, processed the simulation data on the MATLAB platform, and employed a statistical method to establish a model for predicting the residual stress amplitude and depth.
Many scholars have performed considerable research on theoretical models of residual stress, finite element simulations, and residual stress prediction models. Although the forming process, metal flow, and forming mechanism of cold rollbeating have been investigated, few studies have focused on the residual stress in cold rollbeating; in particular, research on the residual stress distribution prediction model of cold rollbeating has not been reported. Therefore, this study investigates the distribution of residual stress with different cold rolling parameters and establishes a prediction model. The results are expected to provide accurate control of the residual stress in the coldforming process and enable the optimization of the process parameters, which improve the surface properties of the workpiece after the cold rollbeating process.
2. Experimental Study of the Residual Stress of Cold RollBeating of an Involute Spline
2.1. Experimental Principle
The principle of the experiment to determine the distribution of residual stress on the cold rollbeating workpiece using the contour method for measurement is shown in Figure 1 [25–27]. The presence of an unknown residual stress inside the specimen is assumed. As shown in Figure 1(a), the specimen is cut in half along the section to be analyzed and evaluated for the residual stresses. As the residual stress is released, the cutting surface contour deforms, as shown in Figure 1(b). According to the superposition principle of elasticplastic mechanics, if an external force is applied, then the cutting surface recovers to the plane that it occupied before it was cut. The obtained stress state is equivalent to the initial residual stress on the plane prior to cutting, as shown in Figure 1(c).
(a)
(b)
(c)
2.2. Experimental Materials and Parameters
Experiments were performed with the same batch of normalizing grade 20 steel, the main chemical composition of which is shown in Table 1. The modulus of the cold rollbeating involute spline is 2.5, the number of teeth is 14, the pressure angle is 30°, the addendum coefficient is 0.5, and the dedendum coefficient is 0.75. The cold rollbeating parameters are as follows: the rotational speeds are 1,428, 1,581, 1,806, 2,032, and 2,258 r/min, and the feed speeds are 21, 28, 35, and 42 mm/min.

2.3. Experimental Program
In order to obtain the yield limit of grade 20 steel, the compression experiment is adopted in the same material under the same heat treatment process. This is due to the fact that the material compression is the main process in the cold rollbeating process. The sample shape is cylinder, the size is Φ8 mm × 6 mm, and the end faces parallelism of the sample is 0.002. The sample manufacturing process is as follows: turning, slow feeding linear cutting, grinding, and polishing. The MTS universal testing machine (shown in Figure 2) was used in the grade 20 steel quasistatic compression experiment.
Based on the parameters of the cold rollbeating spline, the material is machined to a cold rollbeating blank. The following process is employed: the rolling wheel rotates clockwise as the workpiece is pulled out. The rolling wheel strikes each tooth one time as the workpiece rotates in a circle. Involute spline processing of different cold rolling forming parameters was performed on a ZRMe9 rolling machine. The spline of cold rollbeating was shown in Figure 3 and the spline sample was shown in Figure 4. In the SereinCMM type FUNCTION1000 wire cutting machine and using a 0.5 mm molybdenum wire with a feed speed of 2 mm/min, a tooth was cut under the cold rollbeating spline; part of the spline tooth was cut along the tooth curve and involved a cutting of the specimen along the symmetrical surface, as shown by the shading in Figure 5, where mm, mm, and mm.
One of the sections of the spline tooth specimen is annealed; next, the two samples are bonded by cutting, with the cutting section position (the removed volume should be sufficiently large to ensure that the release of stress can cause a sufficient amount of deformation), as shown in Figure 6.
The point coordinates of the cutting plane of Figure 6 were measured using a SereinCMM FUNCTION 1000 threecoordinate measuring machine (to reduce the error, both surfaces produced by cutting must be measured, and a total of four surfaces must be measured). The measurement was performed at 0.01 × 0.01 mm intervals using the reciprocating measurement method (a single measurement track along the direction parallel to the cutting line is required to cover the two surfaces). The measured data that correspond to the two planes are subtracted to obtain the measured point change amount (vector deformation), which is the amount of deformation caused by the release of the residual stress. A cubic spline curve fitting algorithm is employed to fit the variation (the subtracted data) of each measurement point to a surface. The surface is applied to a finite element model with the same size as the annealed specimen using Abaqus software as a boundary condition. To avoid rigid body displacement during the model analysis, an additional constraint that does not affect the free deformation of the profile is imposed. Next, the finite element calculation is conducted. The stress on the cut surface is equivalent to the residual stress at the same position prior to cutting the sample.
2.4. Experimental Results and Discussion
The stressstrain curve of grade 20 steel quasistatic compression experiment is shown in Figure 7. Figure 7 shows that the true stress grows linearly with the increase of true strain reaching the strengthening stage firstly; as the crosssectional area of the sample increases, the true stress changes slowly as the true strain increases. Grade 20 steel in the compression process has no obvious yield stage, taking 213 MPa as the yield stress which corresponds to the true strain 0.0035. Because of the plastic deformation of the workpiece and the severe friction between the rolling wheel and the workpiece, the thermal effect is formed during the cold rollbeating process and part of the energy is released in the form of heat; according to the law of conservation of energy, the residual stress is less than 213 MPa.
The residual stress curve of the dedendum, pitch, and addendum in three positions in a cold rolling spline with different rotational speeds and different feed rates is shown in Figures 8–12.
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
Figures 8–12 show that the tooth superficial coat of the cold rolling spline is composed of the residual compressive stress, and the residual compressive stress on the surface of the tooth superficial coat is small. This is due to the fact that the residual compressive stress of the spline tooth surface has a certain release after cold rollbeating. The residual compressive stress increases with the change in the layer depth; when the layer depth is equal to the depth of the subsurface, the residual compressive stress attains its maximum. The residual compressive stress decreases with an increase in layer depth; when the depth of the layers increases to a certain depth, the residual compressive stress is 0, and the residual stress changes from compressive stress to tensile stress. The residual tensile stress increases with an increase in layer depth, and the residual tensile stress slowly decreases. The gradient of the residual compressive stress in the subsurface layer is larger than the subsurface layer. After a certain layer depth, the increased gradient of the residual tensile stress is larger than the reduction in residual tensile stress. The variation law of the residual stress with the increase of the depth of the layer with different rotational speeds and different feed rates is consistent. The residual compressive stress in the spline formed at the dedendum is larger than the compressive stress formed at the pitch. The minimum value of the residual compressive stress is attained at the addendum. The deep layer of the residual compressive stress at the spline dedendum is larger than the deep layer at the pitch. The deep layer of residual compressive stress at the addendum is the minimum value.
2.4.1. Experimental Error Analysis
The experimental error of the contour method is caused by fitting error of the spline tooth and cutting plane slightly moving because of stress relief during the wire cutting progress; these errors are difficult to be synthetically calculated and adopt classical residual stress test XRD compared with the contour method.
ProtoLXRD type X ray stress analyzer was used to test the surface residual stresses of specimens with rotational speed being 1806 r/min and feed rate being 28 mm/min. The peeling of the spline teeth is tested by electrolysis corrosion method, and the residual stress in the deep direction of the spline is obtained by layerbylayer test. The contrast of the residual stress measured by the contour method and the XRD method is shown in Figure 13.
(a) Dedendum
(b) Pitch
(c) Addendum
The surface residual stress of the spline tooth profile measured by the contour method is obviously lower than that measured by the XRD method. This is because the fitting error of the spline tooth and the test error are caused by cutting plane slightly moving because of stress relief during the wire cutting progress. Although the contour method has a certain error, the test result still has the same trends as the XRD test result. As is shown in Figure 13, the residual stress magnitude and trend obtained by the two methods are very close to each other. Because of the XRD test, it is difficult to accurately control the delamination depth, and the ProtoLXRD system has the error of fitting diffraction peaks. Therefore, the contour method can be used to test the internal stress with high accuracy.
2.4.2. Variation Rule of the Residual Compressive Stress Peak
The change curve of the peak value of the residual compressive stress with the cold rollbeating rotational speed is shown in Figure 14.
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
As shown in Figure 14, the peak residual compressive stress of the spline at the dedendum is larger than the peak residual compressive stress at the pitch. The peak residual compressive stress of the addendum is the smallest value. When the rotational speed increased, the peak residual compressive stress curve of the three positions of the tooth profile increases, and the increase of the residual compressive stress of the addendum and the pitch is small. When the feed rate of the cold rolling spline was 21 mm/min or 28 mm/min, the peak value of the residual compressive stress at different rotational speeds at the pitch of spline in cold rollbeating forming ranges from 67.4 MPa to 80.8 MPa. The feed rates of the cold rollbeating spline are 35 mm/min and 42 mm/min. The peak value of the residual compressive stress for different rotational speeds at the pitch of the spline in cold rollbeating forming ranges from 79.4 MPa to 86.8 MPa. The increase of the residual compressive stress at the dedendum is more significant. Because the nonuniformity of the surface metal flow formation of residual stresses is directly related to the formation of residual stresses during spline cold rolling, the increase in the rotational speed of the cold rollbeating increases the nonuniformity of the flow of the spline surface, and the peak residual stress increases, especially the degree of the metal flow unevenness at the dedendum. The peak residual stress increases, especially the unevenness of the metal flow at the dedendum, and a maximum increase in the peak residual stress is attained. At the same feed rate, the increase in the rotational speed of cold rollbeating causes the amount of striking to be reduced in each round of the workpiece. The effect of thermal mechanical coupling on the formation of residual stress increases, and the peak residual stress has a tendency to decrease. Due to an increase in the rotational speed of the cold rollbeating, the increase of the peak residual stress at the pitch is not significant. Because the forming of the spline addendum is gradually formed by the flow of the metal during the cold rollbeating process, the effect of force on the cold rollbeating is small. After the cold rollbeating process, the residual stress is released at this position; thus, the peak residual compressive stress at the addendum of the spline is the minimum value, and the increase of the peak residual compressive stress at the addendum is small as the rotational speed of the cold rollbeating increased.
The variations of the peak compressive residual stress curve with the feed rates of the spline at different rotational speeds are shown in Figure 15.
(a) 1428 r/min
(b) 1581 r/min
(c) 1806 r/min
(d) 2032 r/min
(e) 2258 r/min
As shown in Figure 15, at different rotational speeds, the peak residual compressive stress at the dedendum, pitch, and the addendum of the cold rolling spline increased with an increase in the feed rate. The residual compressive stress at the dedendum exhibited the most significant increase, and the peak residual compressive stress at the pitch and the addendum is small due to an increase in the spline feed rate at the same speed rate. The amount of strike increased in the cold rollbeating process, and the deformation caused by the force of the cold rollbeating increased. The strain increased to the maximum value at the dedendum; thus, the peak residual stress at the dedendum also exhibited the most significant increase. With an increase in the feed rate, the storage range energy in the cold rollbeating process increased; the workpiece surface needs to balance the tensile stress within the depth of the workpiece in an extensive range. As the spline feed rate increased during the cold rolling process, the larger peak residual compressive stress is formed at the spline surface.
2.4.3. Variation in the Residual Layer Depth
The variation of the residual stress layer depth curve with rotational speeds is shown in Figure 16.
(a) 21 mm/min
(b) 28 mm/min
(c) 35 mm/min
(d) 42 mm/min
As shown in Figure 16, within the range of the cold rollbeating rotational speed and spline feed rate in the experiment, the residual compressive stress layer depth in the superficial spline profile in cold rollbeating indicates that the residual compressive stress layer depth at the dedendum is deeper than the residual compressive stress layer depth at the pitch. The residual compressive stress layer depth at the addendum is the smallest depth. With an increase in the rotational speed of the cold rollbeating, the residual compressive stress layer depth at the dedendum decreases, while the residual compressive stress layer depth at the pitch and addendum slightly decreases. The residual compressive stress layer depth ranges from 0.7 to 0.8 mm at the pitch. When the spline feed rate is large, the residual compressive stress layer depth at the dedendum increases because the increase in the cold rollbeating speed rate causes an increase in the peak residual compressive stress. However, an increase in the cold rollbeating speed rate causes a decrease in the amount of strike. Rolling rounds of a single hit were caused by the corresponding reduction in strain. The strain energy produced by the amount of strike is reduced, especially the spline feed rate, which is large in the cold rollbeating. With an increase in the rotational speed of the cold rollbeating, the amount of strike and the range of the cold rollbeating force decrease; thus, the residual compressive stress layer depth is reduced.
The curves of the relationship between the depth of the residual compressive stress layer and the feed rate of the spline for different cold rollbeating speeds are shown in Figure 17.
(a) 1428 r/min
(b) 1581 r/min
(c) 1806 r/min
(d) 2032 r/min
(e) 2258 r/min
As shown in Figure 17, the residual compressive stress of the surface of the spline tooth profile increases with an increase in the spline feed rate amount during the cold rollbeating process. When the rotational speed of the cold rollbeating is 1428 r/min and 1581 r/min, the residual compressive stress layer depth significantly increases. When the rotational speed of cold rollbeating is 1806 r/min, 2032 r/min, and 2258 r/min, the increase of residual stress layer is not obvious. This is due to the fact that the residual stress is produced by the uneven deformation of the workpiece material. In the high rotational speed, the workpiece material strain rate increased, causing the material flow stress to increase and the workpiece surface of the uneven degree of plastic deformation also increased. But the increase of speed led to the reduction of depth of a single hit; the scope of the impact of rolling force becomes smaller. Therefore, at high rotational speed, the increase gradient of the residual stress layer depth is small, and the gradient of the peak residual compressive stress decreases slowly. When the rotational speed of the cold rollbeating is 1428 r/min and 1581 r/min, the depth of the residual compressive stress layer ranges from 0.84 to 0.98 mm at the pitch with different feed rates. The rotational speed is 1806 r/min and 2032 r/min when the different feed rates of cold rollbeating forming at the pitch of the residual pressure stress layer depth range from 0.71 to 0.73 mm. This finding is due to the increase in the amount of spline feed rate, which causes the roller on the spline of the single shot to increase the amount of strike after an increase in the amount of deformation. The cold rollbearing force eventually produces residual stress in the deeper surface of the spline surface. When the cold rollbeating rotational speed is 2258 r/min with different feed rates of cold rollbeating forming, the pitch circle at the residual compressive stress layer depth ranges from 0.68 to 0.73 mm. This result is due to the increase in the rotational speed of the cold rollbeating, which causes a reduction in the number of hits of the roller to the spline, the effect range of the rollbeating force, and the depth of the residual compressive stress layer.
3. Model of the Surface Residual Stress Distribution of the Spline Shaft Profile
The response surface method has many advantages, such as the ability to rotate, sequential nature, model stability, and reduced test times; the method is often employed to solve practical problems because the response estimation results can approach the real response surface and achieve a satisfactory prediction.
The experimental results reveal that the influence of the rotational speed and feed rate of the spline on the residual stress is not independent, and the relationship between the peak and depth layer of the residual stress curve is nonlinear. Therefore, the secondorder estimation regression equation is employed to establish the surface response model of the residual stress distribution with variations in the cold rollbeating parameters.
The secondorder regression prediction model of the rollbearing rotational speed and feed rate interaction of the two factors is given bywhere is the rotational speed in r/min and is the feed rate in mm/min.
3.1. Model of the Peak Value of the Residual Compressive Stress of Cold RollBeating
The peak value of the residual stress on the surface of the tooth profile is the dependent variable, and the rolling wheel speed and the spline feed rate are the independent variables. Using the experimental data, the rollbeating rotational speeds are 1, 428, 1,581, 1,806, and 2,032 r/min, and the spline feed rates are 21, 28, 35, and 42 mm/min. Fitting for formula (1), establish a relationship model between the peak residual compressive stress and the parameter of cold rollbeating of the three positions in the spline tooth profile at the dedendum, pitch, and addendum.
The model of the peak value of compressive residual stress of the dedendum is expressed as follows:
The model of the peak value of compressive residual stress of the pitch is expressed as follows:
The model of the peak value of the compressive residual stress of the addendum is as follows:
After calculation, the test results from the three models are listed in Table 2.

The test results for the peak residual stress values, which are listed in Table 2, illustrate that the value is substantially larger than , which indicates that the confidence levels of the three models exceed 95% and also indicates high accuracy of the prediction results. The correlation coefficients in the three models are 99.7%, 98.83%, and 98.64%, which indicate that the fitting results are reliable and the correlation between the predicted values and measured values is strong.
According to the model of the residual compressive stress peak of the tooth profile established by formulas (2)–(4), the response surface of the residual stress peak of the tooth profile with the cold rollbeating speed and spline feed rate is shown in Figure 18.
(a) Dedendum
(b) Pitch
(c) Addendum
The response surface shown in Figure 18 illustrates that the peak of the residual stress increases with an increase in the rollbeating speed when the feed rate of cold rollbeating is constant but the amplitude of the increase is not large. When the cold rollbeating’s rotational speed is constant, the increase in the residual stress peak with an increase in the feed rate is large, especially in the dedendum part.
3.2. Establishment of the Depth Model for the Residual Compressive Stress Layer of Cold RollBeating
With the depth of the residual stress layer on the surface of the spline tooth profile as the dependent variable and the rollbeating rotational speed and spline feed rate as the independent variables and using the experimental data, the cold rollbeating rotational speeds are 1,428, 1,581, 1,806, and 2,032 r/min, and the spline feed rates are 21, 28, 35, and 42 mm/min. Fitting for formula (1) establishes a relationship model between the residual compressive stress layer depths and the parameter of cold rollbeating of the three positions in the spline tooth profile at the dedendum,pitch, and addendum. The model of the residual compressive stress layer depth of the dedendum is expressed as follows:
The model of the residual compressive stress layer depth of the pitch is expressed as follows:
The model of the residual compressive stress layer depth of the addendum is expressed as follows:
The significance test and variance analysis were applied to models (5)–(7). The results of the significance test are listed in Table 3.

The significance test results of the residual stress layer depth in Table 3 show that the value is greater than 0.05. In addition, the confidence level of the three models is greater than 95%, which indicates that the prediction results are accurate. The correlation coefficients for the dedendum, pitch, and addendum are 96.76%, 88.25%, and 93.21%, respectively, which indicate that the fitting results are accurate. Thus, a strong correlation between the predicted values and the measured values is observed.
According to the residual stress layer depth model, the residual stress layer depth in the tooth profile with the rotational speed and spline feed rate is shown in Figure 19.
(a) Dedendum
(b) Pitch
(c) Addendum
The response surface in Figure 19 shows that the combined effect of the rollbeating speed and spline feed rate has a significant effect on the residual compressive stress layer depth. When the rotational speed is constant, the depth of the residual compressive stress layer rapidly increases with an increase in the feed rate, and the growth rate gradually increases. When the spline feed rate is constant, the depth of the residual stress layer exhibits a decreasing trend but the rate of the descent gradually decreases (the top part is slightly different). The residual compressive stress depth layer is the same as the residual compressive stress depth layer in the experimental section in terms of the curve trends.
In the cold rollbeating forming process, an increase in the spline feed rate not only can increase the residual stress peak and the residual compressive stress layer depth but also can cause an increase in the contact force of the rolling wheel and the spline and system vibrations. As a result, the spline surface quality decreased, and the excessive increase in the residual stress peak value and the residual compressive stress depth layer caused machining deformation of the workpiece. However, an overly small feed rate will affect the processing efficiency. Therefore, the processing conditions should be appropriate with the increased feed rate but the increase should not be excessive. Increasing the rollbeating rotational speed can also increase the peak value of the residual stress of the spline surface but reduces the contact force between the rolling wheel and the spline and the depth of the residual compressive stress layer; therefore, a better spline surface quality can be obtained.
4. Contrast Analysis of the Predicted and Experimental Results of the Established Model
The residual stress peak values and residual compressive stress layer depth were experimentally obtained, and a model for the comparative analysis for a rollbeating rotational speed of 2,258 r/min and spline feed rates of 21, 28, 35, and 42 mm/min was established. The comparative analysis results of the residual stress peak values and residual stress layer depth are shown in Figures 20 and 21.
Figure 20 shows that the curve change tendency of the predicted results for the residual stress peak value at different spline feed rates is consistent with the experimental results. According to the calculation results, the maximum relative error of the residual stress peak value between the predicted results and the experimental results in the dedendum is 2.38%. The maximum relative error of the residual stress peak value between the predicted results and the experimental results in the dedendum is 3.3%. The maximum relative error of the residual stress peak value between the predicted results and the experimental results in the dedendum is 3.14%.
Figure 21 shows that the curve change tendency of the predicted results for the residual stress peak value at different spline feed rates is consistent with the experimental results. According to the calculation results, the maximum relative error of the residual compressive stress layer depth between the predicted results and the experimental results in the dedendum is 6.5%. The maximum relative error of the residual compressive stress layer depth between the predicted results and the experimental results in the pitch is 6.1%. The maximum relative error of the residual compressive stress layer depth between the predicted results and the experimental results in the addendum is 10%.
This analysis indicates that the residual stress peak value and the residual compressive stress layer depth model can be employed to control the residual stress and optimize the parameters of the cold rollbeating process.
5. Conclusions
The residual stress distribution at the surface of the spline tooth profile was measured for cold rollbeating, the measurement data were analyzed, and the influence of different cold rollbeating parameters on the spatial distribution of the residual stress in different parts of the spline tooth profile was clarified. The main conclusions are as follows.
() Cold rollbeating in the spline tooth profile surface causes the formation of residual compressive stress, the residual compressive stress on the spline tooth profile surface is small, the residual compressive stress increases with an increase in the surface layer depth, and the maximum residual compressive stress is attained when the layer depth attains a certain depth. As the depth of the layer increases, the residual compressive stress decreases. When the depth of the spline tooth profile pitch reaches a certain position (0.68–0.98 mm), the residual compressive stress of the spline tooth profile is 0, and the residual tensile stress is formed with an increase in the depth of the layer.
() The residual compressive stress at the dedendum is higher than the residual compressive stress at the pitch and the addendum, and the smallest residual compressive stress is attained at the addendum.
() Increases in the spline feed rate and rotational speed can cause an increase in the residual compressive stress peak value of the tooth surface profile of the cold rollbeating spline shaft. A significant increase in the range of the peak value of the residual compressive stress was observed at the dedendum, and the peak value of the residual compressive stress at the pitch and the addendum did not significantly increase. The peak value of the residual compressive stress at the pitch ranges from 67.4 MPa to 80.8 MPa.
() The depth of the residual compressive stress layer at the dedendum is deeper than the residual compressive stress layer at the pitch, and the depth of the residual compressive stress layer at the addendum is minimal. The increase of the rotational speed of the cold rollbeating decreases the depth of the residual compressive stress layer at the addendum, and the depth of the residual compressive stress layer at the pitch and the addendum slightly decreases. An increase in the spline feed rate will increase the residual compressive stress layer depth.
() In this paper, the secondorder regression surface model of the residual stress distribution of cold rollbeating forming is established with a high degree of credibility due to the maximum relative error of the peak of the residual compressive stress of 3.3%, and the maximum relative error of residual compressive stress layer depth is 6.1% at the pitch. The residual stress distribution and the residual compressive stress layer depth of the superficial spline profile can be predicted for different cold rollbeating parameters. The surface performance of the spline of cold rollbeating forming should be improved, and the forming process parameters should be determined according to the required residual stress state.
Conflicts of Interest
The authors declare that they have no conflicts of interest.
Acknowledgments
The authors are grateful for the financial support received from the National Natural Science Foundation of China (51475146, 51475366, and 51075124).
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