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1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 690 Design and Development of All-Terrain Vehicle : Volume 1 Karan Sangaj1, Aditya Suryawanshi2, Sudarshan Shinde3 , Shubham Lad4 1,2,3,4 UG , Department of Mechanical Engineering , KIT's College of Engineering , Kolhapur , India. ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract- The objective of this project is to design and manufacture a racing vehicle-ATV (All-Terrain Vehicle) for participation in competition like BAJA .The vehicle is designed by using mathematical modeling and computer-aided design and simulation by using a ANSYS software to make vehicle able to run and perform efficiently on different terrains like rocky, muddy, lose gravel .the important parameter to select for chassis are material, its shape and cross section area. This optimized parameter made the vehicle light weight, stable, efficient with having high strengthanddurability. Inthisstudy we deal with manufacturing and development of frame/chassis of vehicle by using steps like Material Selection, Cross-section Selection, and Frame design parameters, Analysis Parameters, Iterations, Analysis and Simulation. So vehicle can be manufactured with compact design, maximum performance as well as safety. Key Words: ATV, Roll Cage, Chassis, Material Selection, Cross-section Selection, Frame Design, Analysis, ANSYS. 1. INTRODUCTION The vehicle chassis includes the suspension and steering systems, frames ,tires, brakes, axles, and wheels [1] .ATV (All-Terrain Vehicle) is designed to operate in difficult and circuitous terrains. ATV consists of three main parts. These are chassis, drive train and suspension. In this study wedeal with developing a unit of ATV called chassis/frame. The chassis is considered to be one of important parts of an automobile. Various important parts like the engine and the drive train, the axle assemblies, the suspension system, the brakes, the steering system, etc., are bolted on chassis. It provides the strength, rigidity required to support the different components. By designing the chassis with optimized parameter the level of noise and vibrations from different components is greatly reduced. To achieve this, Chassis should be rigid, so it can withstanddifferentstresses and shocks (bending and torsional moments). So, strength and stiffness are two important factors considered while designing. Before manufacturing; Finite Element Analysis (FEA) is done to ensure designed chassis can withstand the loads and stresses acing on it. 2. MATERIAL AND CROSS-SECTION SELECTION The AISI grade is considered for the frame design due to its mechanical properties and chemical composition. The AISI grade contains high carbon percentage as well as high yield strength and ultimate tensile strength. it isalsocosteffective as well as easily available. Property AISI 1018 AISI 4130 Carbon Content (%) 0.14-0.20 0.28-0.33 Density (g/cc) 7.87 7.85 Elongation at Break (%) 15 25.5 Modulus of Elasticity(GPa) 200 205 Ultimate strength (MPa) 440 670 Yield Strength (MPa) 370 435 Table 1: Material Comparison From above table it is seen that yield strength and ultimate strength of the AISI 4130 is much higher compared to AISI 1018. Another factor is density, density of AISI 4130 is less than AISI 1018 therefore the material chosen is AISI 4130. AISI 4130 provides better safety and islessbulk framesothe total vehicle weight is reduced. Outer Dia. (mm) 25.4 31.75 Wall Thickness (mm) 3 1.6 Moment of Inertia (mm4) 8073.32 9320.12 Bending Moment (N-m) 229.77 265.26 Bending Stiffness (N-m2) 1655.03 1910.62 Table 2: Cross-section for AISI 1018 Outer Dia. (mm) 25.4 31.75 Wall Thickness (mm) 3 1.6 Moment of Inertia (mm4) 8073.32 9320.12 Bending Moment (N-m) 270.15 311.86 Bending Stiffness (N-m2) 1655.03 1910.62 Table 3: Cross-section for AISI 4130 For the cross-section it was decided to create the frame using 25.4mm OD and 3mm wall thickness, AISI-4130 Steel
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 691 series has higher strength than AISI-1018 [3]. Also another factor for the cross-section selection was the market availability which is important criteria if we want to make this frame feasible for manufacturing. Moment of Inertia (I) is calculated by using equation I = (π/64)*(O.D4 - I.D4) Bending stiffness is calculated by using equation Bending Strength = σy*I/C Bending Strength is calculated by using equation Bending Stiffness = E*I 3. FRAME DESIGN CONSIDERATIONS Frame is designed by keeping in mind the driver’s safety, a minimum clearance is given to the entire roll-cage member from drivers’ body. Frame is also designed giving priority to those parameters which are essential for driver’s safety and vehicle stability. Another consideration is to keep driver in comfort therefore ergonomics considerationisanimportant priority. Driver’s position is kept as comfortable as possible by trying different sitting positions possible. The back angle is kept slightly slant to back at an angle of 5-10 degree from vertical position. Figure 1: 3D RENDERED CATIA MODEL OF CHASSIS Other parameters like weight, durability, and cost, simple and aesthetically appealing design were taken into considerations. By considering the other subsystem assemblies like engine, transmission, steering, suspensions and brakes, frame is so designed that all the subassemblies could be connected to the frame. 4. FRAME ANALYSIS PARAMETRS The objective of analysis of frame is to ensure that framehas adequate factor of safety even in worst case scenarios/ impacts/ collisions to ensure driver safety. it also ensures that it has greater torsional stiffness ,less deflection under dynamic loading and static loading, natural frequency of the roll cages does not matches with the engine working range frequency to avoid resonance. The value of force to be applied on the frame could be obtained by using Impulse Method or G-Force Method. G-Force Method is widely used method when prototype testing is not a feasible solution. Mathematically, G = m*g = 250*9.81 = 2452.5 N [2]. Where, M=mass of the vehicle g= acceleration due to gravity Different static analysis or collisions are Front Impact, Rear Impact, Side Impact and Roll over test. The applied forces in different static analysis or collisions are as follows. Front impact 4G Rear impact 3G Side impact 2G Roll over 1.5G Table 4: G-force Applied 5. ANALYSIS Analysis of frame is necessary in order to determine the induced maximum stressesandmaximumdeflection.For the analysis of frame we have used ANSYS 15 software. The impact tests and their deformed shape and stress analysis are as follows. Figure 2: Meshing Of Chassis
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 692 In Figure 2: Meshing Of Chassis, initial settings are Physics Preference is mechanical, Element Size isdefault,Smoothing is Low, Transition is Fast, Span Angle Center is Coarse, Transition Ratio is 0.272, Growth Rate is 1.2, total Nodes are 130745 and total Elements are 69211. Front Impact: For the front impact the rear suspension points are kept fixed. After fixing rear suspension points the force of 4G is applied on the front part of the frame. Figure 3: Total Deformation in front impact Figure 3: Total Deformation in front impact, shows total deformation of chassis when force of 4G (9810N) is actedon front part of chassis. From above figure it is observed that the maximum deflection is 4.8029 mm. Figure 4: Maximum Stress in front impact Figure 4: Maximum Stress in front impact, shows maximum stress occurred in chassis when force of 4G (9810N) is acted on front part of chassis. From above figureitisobservedthat the maximum stress occurred in body is 253.56 Mpa. Rear Impact: For the rear impact the front suspension points are kept fixed. After fixing frontsuspensionpoints the force of 3G is applied on the rear part of the frame. Figure 5: Total Deformation in rear impact Figure 5: Total Deformation in rear impact, shows total deformation of chassis when force of 3G (7357.5N) is acted on rear part of chassis. From above figure it is observed that the maximum deflection is 2.6420 mm. Figure 6: Maximum Stress in rear impact
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 693 Figure 6: Maximum Stress in rear impact, shows maximum stress occurred in chassis when force of 3G (7357.5N) is acted on rear part of chassis. From above figure it is observed that the maximum stress occurred in body is 283.67 Mpa. Side Impact: For the side impact the suspension points of the other side of the side of impact is kept fixed. After fixing suspension points, the part of the side of impact is applied with the force of 2G. Figure 7: Total Deformation in side impact Figure 7: Total Deformation in side impact, shows total deformation of chassis when force of 2G (4905N) is actedon side part of chassis. From above figure it is observedthatthe maximum deflection is 0.5990 mm. Figure 8: Maximum Stress in side impact Figure 8: Maximum Stress in side impact, shows maximum stress occurred in chassis when force of 2G (4905N) is acted on side part of chassis. From above figure it is observed that the maximum stress occurred in body is 179.16 Mpa. Roll Over: For the roll-over condition the bottom suspension points are kept fixed. After fixing bottom suspension points, the point which comes in contact with ground first when roll over occurs is applied with the 1.5G force. Figure 9: Total Deformation in Roll-over Figure 9: Total Deformation in Roll-over, shows total deformation of chassis when force of 1.5G (3678.75N) is acted when roll-over condition is occurred. From above figure it is observed that the maximum deflection is 5.8738mm. Figure 10: Maximum Stress in Roll-over
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 10 | Oct -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 694 Figure 10: Maximum Stress in Roll-over, shows maximum stress occurred in chassis when force of 1.5G (3678.75N) is acted when roll-over condition is occurred. From above figure it is observed that the maximum stress occurred in body is 172.26 Mpa. 6. RESULTS The different test gave us the maximum stresses and deformed shape. As we know value of stresses on frame, we can find the FOS with it, as we know that FOS is the ratio of Yield Strength of material to the Maximum stress occurring on body. Mathematically, FOS = σy / (Max. Stress) The overall Results are tabulated as follows. Impact condition Maximum stress (Mpa) Total Deformation (mm) FOS (calcula ted) Front 253.56 4.8029 1.72 Rear 283.67 2.6420 1.53 Side 179.16 0.5990 2.42 Roll-over 172.26 5.8738 2.52 Table 5: Results 7. CONCLUSION From above results we conclude that FOS is greaterthan 1in all conditions so frame is safe. the maximum deflection occurs in the Roll-over condition, the value of which is 5.8738 mm. in this study we have already discussed that there is clearance between driver’s body and frame, this clearance is more than maximum deflection and therefore we can conclude that even in worst condition there is no harm to driver. 8. REFRENCES 1. Gilles, Tim. “Automotive Chassis: Brakes, Suspension, and Steering” /Tim Gilles. ISBN 1-4018-5630-6. Pg. 3. 2. Nordhoff , Larry S. “Motor Vehicle Collision Injuries: Biomechanics, Diagnosis, and Management”/Lawrence S. Nordhoff, Jr. - Second Edition. Pg. 604 . 3. Karl-Heinrich Grote, Erik K. Antonsson. “Springer Handbook of Mechanical Engineering, Volume 10” / ISBN 978-3-540-49131-6. Pg. 177.
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