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IRJET- Structural, Material and Modal Analysis of Ashok Leyland 2516 Model Truck Chassis using ANSYS 14.0
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IRJET- Structural, Material and Modal Analysis of Ashok Leyland 2516 Model Truck Chassis using ANSYS 14.0
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 226 Structural, Material and Modal Analysis of Ashok Leyland 2516 Model Truck Chassis using ANSYS 14.0 Saumya Rastogi1, Dr. L. P. Singh2 1M. Tech student, Production & Industrial Engg. (Mechanical Engineering Dept.), SHUATS, Allahabad, India 2Associate Professor, Production & Industrial Engg. (Mechanical Engineering Dept.), SHUATS, Allahabad, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract: Chassis acts as a backbone or framework of automobiles which supports power trains, transmission system, braking system etc. It is ofvarioustypessuchasladder, backbone and monocoque. Their strength varies as the design of chassis and material varies. Chassis strength, deformations, load-carrying capacity, stresses generated, vibrations, etc. are many fields that require regular researchtokeepvehiclessafe, to improve vehicles fuel efficiency and also should be cost effective. In present work structural, material and modal analysis is being done to find the rateofdeformation, strength, deformations occurring at differentfrequenciesetc. inorderto find the best material which can fulfil the requirements of truck chassis. Software such asSOLIDWORKS2016and ANSYS 14.0 is used for modelling and analysing Ashok Leyland 2516 model truck. On comparing all the stress, strain, deformations of respective materials we can conclude that among three materials i.e. Structural steel, AISI4340, Carbon fibre which material is well suited to design a chassis frame Key Words: ANSYS 14.0, Ashok Leyland 2516 model truck Chassis, Ladder frame, SOLIDWORKS 2016 1. INTRODUCTION Chassis is a French term which was used to connote the frame parts or the basic Structural of vehicle. The chassis is considered to be one of the most significant structure of an automobile. Chassis supports Power plant, Transmission System, Axles, Wheels and Tyres, Suspension, Controlling Systems like Braking, Steering etc.,andalsoelectrical system parts are mounted on the chassis frame. It not only provides safety to the vehicle but also reduce the noiselevel,vibration etc. There are many types of chassis such as Ladder chassis, Backbone chassis and monocoque chassis chassis. Further classification of chassis is based onlocationofengine,type of drive, type of Structural etc. Different type of chassis is used in different categories of vehicle. From past many years chassis strength and stability is a focused section for researchers. In the present work Chassis of Ashok Leyland 2516 model truck is taken for study. Structural Steel, AISI4340 and Carbon fiber is taken for modeling and analysis of chassis. From the results we can easily conclude that how different materials affects strength and life of chassis .Composite materials are modern materials less in weight and more in strength. This study will clearly shows comparisonbetweentheconventional materialsandmodern materials. 1.1 OBJECTIVE OF PROJECT The main objective of the project is to: 1. Design achassisofAshokLeyland2516modelTruck with the help of SOLIDWORKS Software. 2. Conduct Stress Analysis in different sections of the chassis to findtheloadconditionsanddeformations in the designed chassis 3. Conduct Material and Modal Analysis by using different materials in order to obtain a correct material for the chassis, capable of reducing the weight and increasing the fuel economyand able to bear the payloads up to certain imit. 2. SPECIFICATION OF CHASSIS Table1-Design Parameters S.No. Parameters Dimensions 1. Model ASHOK LEYLAND 2516 2. Length of frame 7162 mm 3. Width of frame 863.6 mm 4. Ground Clearance 260 mm 5. Gross Vehicle Weight 25 tons 6. Kerb weight 6116 kg 7. Payload 15800 kg 8. C-Channel 228.60 x 88.90x 25.40 mm3
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 227 3. MATERIAL AND METHODS 3.1 Material Properties Table 2- Material Properties Properties Structural steel AISI4340 Carbon fiber Density (kg/m3) 7850 7827 1500 Young’s Modulus (Pa) 2 x 1011 1.995 x 1011 1.5x1011 Poisons ratio 0.3 0.32 0.38 Tensile Ultimate Strength (Pa) 2.5 x 108 8.6184 x 108 6 x 108 3.2 Methodology In present work chassis of Ashok Leyland truck is modeled and analyzed by using SOLIDWORKS 2016 and ANSYS 14.0 software respectively. Structural steel, AISI4340 and carbon Fiber are the materials whicharetakenintoconsiderationfor analysis. Steps follow in methodology flowchart shown below: Figure 1: Flowchart of Methodology 3.3 Design of Chassis Frame The designing process requires CAD software like SOLIDWORKS2016.ThechassisofAshokLeylandisdesigned with unique measurements and as per the requirements of the category of vehicles. We have therefore designed the Ashok Leyland 2516 model truck chassis with exact measurements such as overall length, wheel base, track width, and other vehicle measurements. Different views are mentioned in order to understand the design easily. Figure 2: SOLIDWORKS MODEL As per the above-mentioned design requirements, the truck chassis designed as follows: Step 1- After collecting all the dimensions a Structural of chassis is being created withthe help ofSOLIDWORKS.While sketching the Structural first of all, the plane i.e front, top or right is chosen. Step 2- Now Longitudinal member is drawn which is C channel whose dimensionis228.60x88.90x25.40mm3.With the help of mirror, extrude etc. options , structure got its exact look. Step 3-Next is to draw the cross members at the fixed distance as it is in actualstructure.Thecrossmembercontain C Section, I section. Step 4-Next is to provide supports to the cross members. The supports are C Section Structural and provide load bearing capacity to the Structural. Step 5-After designing make sure the all the components should not merge in each other. 3.4 Analysis of Chassis The step of analysis is as follows: Step 1-Firstly, after openingthesoftwarewechooseStatic Structural option from the table listed at the left most part of the screen. Step 2- Now as shown in the fig below a chart A appears .Starting from option number 2 Engineering data, here we choose material on which the analysis is performed Step 3- After choosing the material now the CAD modelof the Ashok Leyland 2516 model truck Chassis frame, is imported into this software from SOLIDWORKS 2016 where various inputs are provided to start the analysis process of this design. Step 4-Ater importing contact between the all the members i.e. longitudinal member, cross members and supports is being provided. Here in the present analysis we have given bonded relationship between all the members. Step 5- Now, the CAD model is meshed followed by the fixing of fixed supports. And then different loads are applied and the structural analysis is carried out to obtain the deformation distribution results. All the results of this
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 228 analysis are listed in the ANSYS 14.0 structural analysis report in APENDIX. Step 6- For showing the deformations due to various frequencies we opt modal option from the main ANSYS window and a chart B appears on the screen .Here we solve the modal and get various results. Step 7- Now generate the report. Step 8- Repeat this whole process for n number of materials on which analysis is to be performed and after generating the result compare all the result and choose the best material. Here in the present work I have used three materials – Structural Steel,AISI4340 and Carbon Fibre. Figure 3: ANSYS Window Figure 4: Meshed View (Nodes-288611, Elements- 47199) 1. Structural Steel Analysis-Solution of analysis is mentioned below Fig 5: Equivalent Elastic strain Fig 6: Directional Deformation Fig 7: Equivalent Von –Mises Stress Fig 8: Total Deformation Fig 9: Total Deformation (34.867Hz)
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 229 Fig 10: Total Deformation (78.141Hz) Fig 11: Total Deformation (79.823Hz) Fig 12: Total Deformation (92.701Hz) Fig 13: Total Deformation (100.57Hz) Fig 15: Total Deformation (112.21Hz) 2) AISI4340- Solution of analysis is mentioned below: Fig 16:Equivalent Elastic strain Fig 18: Equivalent Von –Mises Stress Fig 19: Directional Deformation
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 230 Fig 20: Total Deformation Fig 21: Total Deformation (39.943Hz) Fig 22: Total Deformation (78.248Hz) Fig 23: Total Deformation (91.837 Hz) Fig 24: Total Deformation (79.933 Hz) Fig 25: Total Deformation (92.76 Hz.) Fig 26: Total Deformation (106.34 Hz) 3) CarbonFiber-Solutionofanalysisismentionedbelow: Fig 27: Equivalent Elastic strain
6.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 231 Fig 28: Equivalent Von –Mises Stress Fig 29: Total Deformation Fig 30: Directional Deformation Fig 31: Total Deformation (69.32 Hz) Fig 32: Total Deformation (153.96 Hz) Fig 33: Total Deformation (158.18 Hz) Fig 34: Total Deformation (182.25 Hz) Fig 35: Total Deformation (208.55 Hz)
7.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 232 Fig 36: Total Deformation (219.84 Hz) 4. Result & Discussion A- Comparison Chart between materials Table 3: Comparison Chart between Materials Parameters /Materials Structural steel AISI 4340 Carbon Fibre Min. Max. Min. Max. Min. Max. Equivalent Stress (MPa) -5.8175e- 7 252.26 5.5723e- 7 251.17 3.8628e- 6 240.81 Equivalent Strain 6.8678e- 12 0.00127 14 7.3248e- 12 0.00128 12 7.0616e- 11 0.00168 88 Total Deformatio n (mm) 0 1.0106 0 1.0154 0 1.3198 Directional Deformatio n (mm) -0.42125 0.20475 -0.95522 0.0115 -0.56389 0.27345 B-Modal Analysis Comparison Charts A-Structural Steel Table 4: Structural Steel Modal Analysis Frequency(Hz) Deformation (mm) 34.867 1.9727 78.14 3.234 79.823 2.7258 92.701 2.7714 100.57 17.38 112.21 4.7563 B-AISI4340 Table 5: AISI4340 Modal Analysis Frequency(Hz) Deformation (mm) 34.943 1.9758 78.248 3.276 79.233 2.7142 91.837 13.415 92.76 2.7363 106.34 16.818 C-Carbon Fiber Table 6: Carbon Fiber Modal Analysis Table 7: % Reduction in Mass of Chassis Graph 1: Bar Chart of static Analysis Graph 2: Bar chart of material mass reduction potential From the above mentioned tables the result is clearly visible that maximum equivalent von-misesstressgenerated in Structural steel is more than AISI 4340 and Carbon Fibre. But if we see the total deformation result, then the value of carbon Fiber is more than the other two materials, but if we increase the thickness of the c-channel then the deformation will be become less .In case of directional deformation the maximum value occurs in AISI4340.Fromthemodalanalysis results indicatethat a different deformation value appearsin chart above. On comparing all the value study shows that at maximum frequency i.e. 219.84 Hz of carbon Fibre very less deformation occurs in the chassis. This shows that Carbon Fibre is safeformanufacturing truck chassis and its weightis approximately 80.8 % less than that of steel. This weight reduction also enhances fueleconomyandreducespollution. 5. CONCLUSION Chassis strength anddeformationundersafelimitsisvery crucial parameter while designing and analysing chassis Structural. In this work, three materials i.e. Structural steel, AISI4340 and Carbon Fiber is selected for modelling and analysis and among them carbon Fibre gives best results. Composite material is very costly as compare to other metal used in auto vehicle chassis frame which incur some extra cost on the consumer .If cost is not considered then best alternative forthe automobileandchassisframeiscomposite materials. The results of the modal analysis give a clear indication that the maximum stress induced is in steel and minimum stress induced is in composite material. It reduces Frequency(Hz) Deformation (mm) 69.32 4.5128 153.96 8.8764 158.18 5.5478 182.25 6.323 208.55 41.963 219.84 10.82 S.No. Material Mass (kg) % Difference 1 Structural steel 1263.2 2 AISI4340 1259.5 0.3% 3 Carbon Fiber 241.37 80.8%
8.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 233 weight of the chassis upto great extent which ensures fuel economy of the vehicle. REFERENCES [1] Anurag, Amrendra Kumar Singh, Akash Tripathi, Aditya PratapTiwari,Nitishupadhyay,ShyamBihari Lal ,” Design And Analysis Of Chassis Frame”, Ijre | Vol. 03 No. 04 | April 2016 [2] David J. Andrea and Wesley R. Brown ,Material Selection Processes in the Automotive Industry ,December, 1993, Office for the Study of Automotive Transportation, University of Michigan Transportation Research Institute, Prepared forthe Automotive Plastics Recycling Project Report Number: UMTRI 93-40-5 [3] Hirak Panchal, Khushbu C. Patel, Chetan S. Jadav,”Structural Analysis of Truck Chassis Frame and Design Optimization for Weight Reduction”, International Journal of Engineering and Advanced Technology (IJEAT) ISSN: 2249 – 8958, Volume-2, Issue-4, April 2013. [4] Mohd Azizi Muhammad Nora,, Helmi Rashida, Wan Mohd Faizul Wan Mahyuddin “Stress Analysis of a Low Loader Chassis” Elsevier Ltd. Sci Verse Science Direct Procedia Engineering 41 ( 2012 ) 995 – 1001 [5] M. Ravi Chandra, S. Sreenivasulu,SyedAltafHussain, “Modeling and Structural analysis of heavy vehicle chassis made of polymeric composite material by three different cross sections”, InternationalJournal of Modern Engineering Research (IJMER) Vol.2, Issue.4, July-Aug. 2012 pp-2594-2600 ISSN: 2249- 6645 [6] MonikaS.Agrawal,”FiniteElementAnalysisofTruck Chassis Frame”, International Research Journal of Engineering and Technology (IRJETVolume: 02 Issue: 03 | June-201) e-ISSN: 2395-0056 p-ISSN: 2395-0072 © [7] O. Ahmad Moaaz, Nouby M. Ghazaly“AReviewofthe Fatigue Analysis of Heavy Duty Truck Frames” American Journal of Engineering Research (AJER, Volume-3, Issue-10, pp-01-06, 2014. [8] Patel Vijaykumar V, Prof. R. I. Patel, “Structural Analysis of Automotive Chassis Frame and Design Modification for Weight Reduction”, International Journal of Engineering Research & Technology (IJERT) Vol. 1 Issue 3, May - 2012 ISSN: 2278-0181 [9] Roslan Abd Rahman, Mohd Nasir Tamin, Ojo Kurdi “Stress analysis of heavy duty truck chassis as a preliminary data for its fatigue life prediction using FEM” Jurnal Mekanikal December 2008, No. 26,76– 85. [10]Shaik Neelophar Begum, S.P.Bhanu Murthy, 'MODELLING AND STRUCTURAL ANALYSIS OF VEHICLE CHASSIS FRAME MADE OF POLYMERIC COMPOSITE MATERIAL' International Research Journal of Engineering and Technology (IRJET), Volume: 03 Issue:08|Aug-2016,p-ISSN:2395-0072 AUTHORS Saumya Rastogi, M. Tech Scholar, Production & Industrial Engineering (Mechanical Engineering Department), SHUATS, Allahabad Dr. L.P Singh Associate Professor, Production & Industrial Engineering (Mechanical Engineering Department), SHUATS
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