International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) Continuously Variable Transmission using the Inner Surface of a Spherical Rotor and Conceptual Design for the Automotive Transmission Hyoungwoo Lee1, Kibong Han2 1,2 Department of Mechatronics Engineering, Jungwon University, South Korea A half-toroidal type of CVT has been applied since 1999 by Nissan Corporation. But many problems have occurred such as spin loss, low torque capacity, severe rotor wear because of a small contact area, large size of CVT, etc. ISCVT overcomes these problems. The shape of the ISCVT contact area is always circular compared to the elliptical area in TCVT. [2-7] Therefore, ISCVT improves both the power transmissibility and the contact pressure. A new ISCVT is designed for automobiles with 110 kW and maximum torque (194 Nm / 4500 RPM). The size of the ISCVT is 220 mm × 150 mm in the overall diameter and width. This ISCVT is compared with a toroidal CVT in terms of the transmission efficiency, maximum shear stress, and life time; it is shown to be more excellent than TCVT. Abstract—A new, continuously variable transmission (ISCVT) that contacts with the inner and outer surfaces of a spherical rotor is introduced. ISCVT consists of four units, a pair of driving/driven rotors, a pair of pressure devices, four traction ball assemblies, and a ratio changer. The four traction balls are situated between the driving and the driven rotors. The ratio changer is located inside one pair of rotors and rotates with a helical groove. The traction ball connector moves through the groove in the ratio changer and varies the traction ball angle, which can change the speed of the driven rotor. The speed ratio of ISCVT is derived by kinematic analysis and determined by the height of the point of contact. We applied the moment equation in order to find the transmission efficiency. ISCVT was applied to a 110 kW passenger car. We evaluated its applicability to automobile usage through a numerical investigation. The maximum shear stresses are formulated by Hertzian contact theory. The lifetime is calculated by the Lundberg-Palmgren method. Simulation results show that ISCVT with four traction ball assemblies is very compact with a high power density and high transmission efficiency. Based on this simulation, we have designed ISCVT and performed stress analysis to find shortcomings in ISCVT. The associated transmission performance is compared with that of toroidal CVT (TCVT) and shown to be excellent. We also applied ISCVT with higher capacity for a construction vehicle and truck. II. BASIC INNER SPHERICAL TRACTION DRIVER CVT MODEL A. Layout The ISCVT is illustrated in Figure 1. The dimension and geometry of the ISCVT are defined by the following design parameters. The curvature of the driving rotor is r1. The traction ball radius is r . n10 , n20 , and n are the direction vectors of the driving/driven rotors and the traction ball, respectively. 1 and 2 are the angle between the rotor axis and the contact point, respectively. is the tilting angle of the traction ball. The radius of the driven rotor is r2 . h1 , h2 , Keywords—CVT, Inner spherical continuously variable transmission (ISCVT), transmission performance, OSR, transmission efficiency, power density, gradability, life-time. h3 , and h4 are the lengths between the driving rotors, driven rotors, traction ball axis, and center of the contact area, respectively. I. INTRODUCTION Existing geared vehicle transmissions use a clutch that isolates the engine power. Geared transmissions result in shifting shock because the speed is changed during high speeds of about 3000~6000 RPM. But a continuously variable transmission (CVT) can continuously transfer power from low to high speeds. CVT has no shifting shocks, which makes it quiet and reduces transmission vibration. Given the continually increasing global concern of consumers with environmental issues, users demand higher efficiency. CVT has already achieved a 10 percent improvement in fuel economy.[1] B. Operating Principle The ISCVT consists of four units, a pair of driving/driven rotors, a pair of pressure devices, four traction ball assemblies, and a ratio changer. The power is generated from the engine or motor and transmitted to the driving rotor. The driving and driven rotors are connected with a pressure device, as shown in Figure 2. 685 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) The driving rotor rotates the traction ball by the pressure device due to rolling contact without slip between the driving rotor and the traction ball. The speed of rotation of the driven rotor is changed by tilting the traction ball. The pressure device shown in Figure 3 consists of an inclined guide and three balls. The balls are set between the input guide and the driving rotor guide. The pressure device generates normal forces that create transmitted torques. The input torque results in tangential and normal forces. The tangential force pushes each rotor and generate contact pressure. The thrust forces are generated by the inclined guide, which generates the normal force proportionally. And are the tangential and thrust components of the resulting force. The tangential and thrust forces are defined as follows. Ti . ri Ft Fth Ft T /r i i . tan tan N1 Fth T1 / r1 . cos1 tan cos1 (3) In the above, Ft and Fth are the tangential force and the thrust force that are applied at the traction ball, respectively, and is the cam lead angle. In the expression above, N1 is proportioned to the torque, T1 This type of pressure device results in high efficiency across a range of speed ratios. Since the angle of inclination, , is related to the efficiency, it is obtained by an optimal process. Figure 4 shows the average efficiency vs. the inclined angle. The efficiency is maximum in the neighborhood of 30°. The assembly of the traction ball consists of four traction balls. Each traction ball has two bearings on the traction ball shaft and the bearing housing. The traction ball is fixed by the traction ball jig. The speed of the driven rotor is changed by varying the tilting angle of the traction ball shaft. The traction ball rotates according to the pivot point, O , which is located at the spherical center of the traction (1) (2) ball. Figure 5 shows a free body diagram of the traction ball. The work that is applied to the ratio changer when the ratio is changed from the lowest speed ratio to the highest value is calculated from the normal forces and the distance moved. FIGURE 1 STRUCTURE OF SWASH PLATE PISTON PUMP BASED AUTOMATIC LUBRICATION SYSTEM FOR COMMERCIAL TRUCKS. FIGURE 3 PRESSURE DEVICE IN THE DRIVING ROTOR Wrc max ( N1 N2 )r (max min ) . (4) In the above, N1 and N 2 are the contact loads at the driving rotor and the traction ball, while max and min are the maximum and minimum static traction coefficients. FIGURE 2 ASSEMBLY OF THE ISCVT (NEUTRAL POSITION). 686 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) max and min are the maximum and minimum phase angles of the traction ball, respectively. The tilted shape of the ratio changer is shown in Figure 6. The ratio changer enables continuously variable transmission (CVT) for the driven rotor. The traction ball connector moves through the helical groove shown in Figure 6. The height of the point of contact changes according to the movement of the connector. V1 1 r1 1 (n r1 ) . (7) Assuming that the driving rotor and the traction ball have no slip, we can apply the velocity constraint on the driving rotor and the traction ball. The rotational speeds of the driving rotor and the traction ball can be written as follows. V1 V1 , 1 1 (n10 r1 ) . (8) (n r1 ) III. KINEMATIC AND KINETIC ANALYSIS Similar to Eqs. (5)~(8), the driven rotor speed can be expressed as: A. Kinematic Analysis In order to find the speed ratio of ISCVT, we have formulated the driving rotor speed, traction ball speed, and driven rotor speed, respectively. The driving/driven rotor speeds and the traction ball speed are as follows. 2 2 (n20 r2 ) . (9) (n 2 r 2 ) The traction balls in the assembly are connected to each other; hence, the speeds of the traction balls are the same. Thus, we rearrange Eqs. (8) and (9) as follows. 1 2 , 1 (n10 r1 ) 2 (n20 r2 ) . (n r1 ) (10) (n 2 r 2 ) The angular velocities of the driving rotor and the driven rotor are related by: FIGURE 4 EFFICIENCY VS. THE INCLINED ANGLE. FIGURE 6 OPERATION OF THE RATIO CHANGER. 2 n40 (n10 r1 ) n40 (n 2 r 2 ) . 1 n40 (n20 r2 ) n40 (n r1 ) (11) Here, r1 is defined in terms of the angle subtended by the contact point and the radius of the rotor as follows. FIGURE 5 THE PRINCIPLE OF SPEED CHANGE. r1 r1 cos1 (n20 ) r1 sin 1 (n30 ) . (12) (13) V1 1 r1 1 (n10 r1 ) . (5) n10 r1 r1s in 1 n40 h1 n40 . V2 2 r2 2 (n20 r2 ) . (6) Similar to Eq. (13), we find all the components of the speed ratio. 687 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) n20 r2 r2 s in 2 n40 h4 n40 . (14) n rc 2 r2 s in 2 n40 h3 n40 . (15) n rc1 r1s in 1 n40 h2 n40 . (16) By substituting (13), (14), (15), and (16) in (11), the overall speed ratio (OSR) between the driving rotor and the driven rotor is seen to be related to the height of the contact point. The speed ratio of ISCVT is represented as follows. h1 h3 . h2 h4 (17) In the above, is the OSR. B. Kinetic Analysis A simple contact model based on Hertzian contact theory [2] is applied in this study. The maximum shear stress in the traction rotor is proportional to the 2/3rd order of the geometric factor, which is defined by the sums of the inverse of the radii of curvature. The traction coefficient for the fluid used, SANTOTRACK50, is obtained from the results of the experiment. The referenced property of traction fluids is shown in Figure 7. The power that is supplied from the driving rotor at A1 rotates the traction ball shown in Figure 8 and is transmitted to the driven rotor through A2 . The velocity differences between the traction ball and the driven rotor generate the traction slip, which generates 2 . In order to FIGURE 7 THE CHARACTERISTIC CURVE OF THE TRANSMISSION FLUID, SANTOTRACK50. find 2 , the traction ball speed must be calculated to (A) DRIVING ROTOR. ascertain the transmission efficiency. The normal force is distributed over the contact area. In order to supply normal force to the driving rotor, pressure is applied by the pressure device. Shear force is generated at the same time regarding the fluid, SANTOTRACK50. This shear force results from the difference in velocity between the driving rotor and the traction ball. This sliding velocity results in power loss. We found the power loss by searching for the traction ball velocity, . To find , we FIGURE 8 THE PRINCIPLE OF SPEED CHANGE. In the above, T1 is the input torque and A1 is the contact area between the driving rotor and the traction ball. O1P1 is the direction vector from the center of curvature to the center of the contact area. PQ 1 1 is the direction vector from the center of the contact area to the center of an infinitesimal area. The shear stress, 1 , is defined in Eq. (19) assuming that apply the moment equation of the driving axis. T1 n10 A1 (O1 P1 PQ 1 1 ) 1dA1 0 . (B) CONTACT AREA. the 1 direction is the same direction as that of the sliding (18) velocity. We define 1 as follows. 688 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) 1 p IV. CONCEPTUAL DESIGN AND PERFORMANCE ANALYSIS Vsd . (19) A. Design procedure of ISCVT To show practicability in automobile usage, a 2000 cc passenger car is considered for numerical investigation. The main design specifications are the input speed, input torque, and overall speed ratio. The design specifications are listed in Table 1. Vsd In the above, 1 is the shear stress vector at the infinitesimal area, is the traction coefficient, p is the pressure at the contact area, and Vsd is the sliding velocity. The friction factor is a function of the normal force and the creep rate: ( p, Cr ) . The creep rate, Cr , is defined as follows. Cr Vsd TABLE I DESIGN SPECIFICATIONS OF ISCVT FOR 110 KW ▪ Displacement ▪ Max. power . (20) ▪ Max. torque V1 ▪ Input speed range ▪ Input torque range ▪ Overall speed ratio ▪ Driving / driven rotor diameter range ▪ Range of the radius of traction ball ▪ Range of the height of the traction ball pivot ▪ Range of the preloaded thrust forces ▪ Range of the cam lead angle Through this process, is derived. T2 is calculated from the free body diagram of the driven rotor, which is shown in Figure 9. The equation is: T2 n20 A2 (O2 P2 P2Q2 ) 2 dA2 0 . (21) The total efficiency of ISCVT is defined as follows. T 2 2 . T11 (A) THE DRIVEN ROTOR. (22) 2000 cc 110kW / 6,000 RPM 194N·m / 4,500RPM 0.1~8000 RPM 0.1~250 Nm 0.09~0.37 100 ~ 200 mm 10~50 mm 50 ~ 100 mm 0.1 ~ 500 N 0.1 ~ 50° The simulation is performed by the following procedure. Firstly, we input the design parameters and mechanical properties. The design variables are the speed ratio of the gear reducer, the radius of the traction ball, the height of the pivot for fixing the traction ball assembly, the radius of the inner driving/driven rotors, the cam lead angles of the pressure devices, and the preloaded thrust forces. Secondly, we set the design constraints: the maximum shear stresses should not exceed 800 MPa; the average efficiency must exceed 60%; the overall diameter of ISCVT is less than 510 mm; and the height of the traction ball assembly must not exceed 65 mm. After determining the geometry of ISCVT, the simulation finds the maximum transmission efficiency through the overall range of the speed ratio. The optimal process is a direct search method through parametric study. Figure 10 depicts a flowchart of the simulation. (B) CONTACT AREA. FIGURE 9 FREE BODY DIAGRAM OF THE DRIVEN ROTOR. 689 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) FIGURE 11 CAD ON ISCVT. B. Stress analysis To analyse the shortcomings of the driving rotor and traction ball housing, we performed stress analysis. Figures 12 and 13 show the stress contours of ISCVT parts. The load condition is the maximum torque at 4500 RPM. This means that the simulation is performed under the worst conditions. FIGURE 10 FLOWCHART OF THE SIMULATION. Table 2 shows the results on the layout and performance from simulation at the maximum torque condition. TABLE II SIMULATION RESULTS FOR ISCVT. Layout results ▪ Radii of the driving/driven rotors ▪ Radius of the traction ball ▪ Height of the traction ball pivot 125 mm 43.3 mm 52 mm ▪ Cam lead angle 36° ▪ Preloaded thrust force Performance results ▪ Transmission efficiency ▪ Work for the ratio changer ▪ Life time ▪ Maximum shear stress ▪ Gradability 220 N 93 % 263 Joules 108,000 hour 552 MPa 20°t FIGURE 12 STRESS CONTOURS OF THE DRIVING ROTOR AND A TRACTION BALL. The assembly design is shown in Figure 11 based on the result of simulation. FIGURE 13 STRESS CONTOURS OF THE TRACTION BALL JIG AND HOUSING. 690 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) The results of analysis are listed in Tables 3 and 4. It is reasonable to use normal carbon steel such as SCM440 (AISI4140) with a yield strength of 1,650 MPa. The results show that ISCVT can have lower thickness and weight because of the low stress as compared with the yield strength. TABLE III DRIVING ROTOR AND TRACTION BALLS Jig 4,104 / 12,005 Tetrahedral ▪ Node / element ▪ Element type Housing 1,198 / 3,329 9 ▪ Material property E=200 × 10 Pa, =0.3 ▪ Max disp. 0.02 mm 0.18 mm ▪ Max stress 200 MPa 559 MPa FIGURE 14 THE AVERAGE POWER EFFICIENCY. TABLE IV TRACTION BALL JIG AND HOUSING ▪ Node / element ▪ Element type Driving rotor 4,104 / 12,005 Tetrahedral Traction ball 4,179 / 20,097 9 ▪ Material property E=200 × 10 Pa, =0.3 ▪ Max disp. 0.1mm 0.02mm ▪ Max stress 141MPa 339MPa C. Performance analysis The power efficiency is calculated according to an inputspeed range of 0~8,000 RPM and an input-torque range of 0~250 Nm. These are the operating conditions of automobiles. The efficiency refers to the average value in the region of the speed ratio. In Figure 14, the efficiency over the 90% region is widely distributed The maximum torque of 194 Nm and rated speed of 4,500 RPM are generated by the engine. According to the speed ratio and input torque, the efficiency distribution is shown in Figure 15. As the speed ratio changes from the high-speed mode to the low-speed mode, the efficiency variation is not significant. This means that the efficiency is over 90% in the entire range of operation and the highperformance region is also widely distributed. FIGURE 15 EFFICIENCY AT THE RATED SPEED. The shear stresses are shown in Figures 16 and 17 at the rated speed. The maximum shear stress is within 510~555 MPa in the driving rotor and within 510~630 MPa in the driven rotor at the maximum torque of 193 Nm. Therefore, a typical carbon steel such as SCM440 (AISI4140) is sufficient as material for the traction rotor. Based on the Lundberg-Palmgren method, the life cycle of ISCVT is calculated and shown in Figure 18. The lifetime at the maximum transmitted torque of 193 Nm being the worst condition is 80,300 hours. This means that the ISCVT’s life-time is more than five years at the worst condition. 691 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) The required work to operate the ratio changer over the full speed range is shown in Figure 19. The maximum value is 280 Joules. At this value, a 300 W stepping motor is sufficient for varying the speed ratio. For ISCVT, we define the gradability as the maximum angle of inclination. The gross vehicle weight is 1660 kg and torque is 193 Nm at 4500 RPM in the lowest speed mode the allowable angle of inclination of roads over which the vehicle can drive is approximately obtained as follows. Fthrust sin 1 Wg Ctire air CareaV 2 2Wg . (23) In the above, is the inclined angle, Fthrust is the thrust force due to the rear wheel, W is the gross vehicle weight, Ctire is the tire resistant coefficient, air is the air density, Carea is the projection area of the automobile, and V is the vehicle speed. Figure 21 shows that ISCVT is capable of ascending over an inclination of 20° at the maximum torque condition. FIGURE 16 MAXIMUM SHEAR STRESS IN THE DRIVING ROTOR. FIGURE 17 MAXIMUM SHEAR STRESS IN THE DRIVEN ROTOR. FIGURE 19 WORK FOR THE RATIO CHANGER. FIGURE 20 A MODEL OF GRADABILITY. FIGURE 18 LIFE-TIME OF THE DRIVING ROTOR. 692 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) The power density based on the volume is defined as the maximum power divided by the overall volume. An ISCVT with an efficiency of 93%, minimum life cycle of 80,300 hours, and maximum shear stress of 600 MPa can be designed to a diameter of 220 mm and width of 150 mm, as shown in Figure 22(a). The ISCVT power density is calculated to be about 19.3 kW / . The comparison between the TCVT and ISCVT are shown in Figures 23~25. In Figure 23, the average through the overall speed ratio of the power efficiencies are about 93 %. Figure 24 shows that the maximum shear stresses in ISCVT are much less than those in TCVT. D. Comparison with the toroidal CVT model To show the superiority of the proposed CVT model, a toroidal model of similar size as that of the designed ISCVT is considered, as shown in Figure 22(b). It has three traction balls that relay motion between the driving and driven rotors. By applying the design specifications in Table 1 to the artificial toroidal model, the overall diameter and width are found to be about 160 mm and 240 mm, respectively. The transmission performance is calculated with respect to input torques of 0.0~250 Nm. FIGURE 23. COMPARISON BETWEEN ISCVT AND TCVT REGARDING THE EFFICIENCY. FIGURE 21 INCLINED ANGLE AT THE LOW-SPEED MODE. FIGURE 24. COMPARISON BETWEEN ISCVT AND TCVT REGARDING THE MAXIMUM SHEAR STRESS. (A) ISCVT. (B) TCVT. FIGURE 22 THE OVERALL SIZE OF ISCVT WITH FOUR BALLS AND TCVT WITH THREE BALLS. FIGURE 25. COMPARISON BETWEEN ISCVT AND TCVT REGARDING THE LIFE-TIME. 693 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) Figure 25 shows differences in the life-time. For input torques in the vicinity of 100 Nm, the ISCVT life-time is twice that of TCVT. Consequently, in comparison with TCVT, ISCVT is expected to be excellent in terms of the transmission performance. In Table 5, the performance of TCVT and ISCVT is summarized. V. CONCLUSION We introduce a new traction drive CVT and apply it to a 110 kW passenger car to evaluate its practicability for automobiles. We have derived the speed ratio of ISCVT by kinematics and the moment equation regarding equilibrium. This paper has presented the conceptual design and performance analysis through numerical investigation of ISCVT by focusing on its basic components. With the proposed mechanism, we can get traction CVT with very high efficiency (over 90%) in the ranges of the maximum speed and the maximum torque. ISCVT has high power density (more than 9.3) even though the material of the traction rotor is carbon steel, such as SCM440 for which the yield strength is 1800 MPa. The expected lifetime is derived by the Lundberg-Palmgren method and the gradability is verified. TABLE V COMPARISON BETWEEN TCVT AND ISCVT ▪ Efficiency ▪ Max. shear stress TCVT 110kW / 6000 RPM 90 % 920 MPa ISCVT 110kW / 6000 RPM 93.4 % 545 MPa ▪ Life time 7,950 hr 80,300 hr ▪ Weight ▪ Work for the ratio changer ▪ Power density 15.7 kg 8.2 kg 571 Joules 246 Joules ▪ Maximum power 8.27 kW / 9.30 kW / E. Analysis of the torque capacity vs. the overall size To analyze higher power capacities and larger sizes, the simulation range is expanded in terms of the overall diameter and input power. The results show that when the rotor is larger than 250 mm, the performance is high (efficiency of over 92%), as shown in Figure 26. The maximum shear stress is considered for largecapacity vehicles. Under 630 MPa, the rotor can be used for small vehicles, as shown in Figure 27. The life-times are compared across the various capacities shown in Figure 28. The simulation result shows that the fatigue life-time is over 40,000 hours. FIGURE 27. SIMULATION RESULTS FOR THE MAXIMUM SHEAR STRESS UNDER HIGH CAPACITIES AND LARGE OVERALL SIZES. FIGURE 28. SIMULATION RESULTS FOR THE FATIGUE LIFE-TIME UNDER HIGH CAPACITIES AND LARGE OVERALL SIZES. FIGURE 26. SIMULATION RESULTS FOR THE EFFICIENCY UNDER HIGH CAPACITIES AND LARGE OVERALL SIZES. 694 International Journal of Emerging Technology and Advanced Engineering Website: www.ijetae.com (ISSN 2250-2459, ISO 9001:2008 Certified Journal, Volume 3, Issue 8, August 2013) [3] The results show that ISCVT can incline over a 20° ramp at the maximum torque. The associated transmission performance is calculated to be excellent in comparison with TCVT; ISCVT also is shown to be practicable for mid-sized automobiles. This study also suggests ISCVT for vehicles with high power capacities such as construction vehicles or trucks. The results show that ISCVT is applicable for all kinds of vehicle. [4] [5] [6] REFERENCES [1] [2] Takashi Imanishi and Shinji Miyata, (2003). 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