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DESIGN AND DEVELOPMENT OF A CHASSIS FRAME FOR MINI- HARVESTING MACHINERY
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 246 DESIGN AND DEVELOPMENT OF A CHASSIS FRAME FOR MINI- HARVESTING MACHINERY Darwish Jahangir1, Adithyan Pradeep2, Anal Raj3, Adwaith Prasannan4 1,2,3,4 B.Tech Student, Department of Mechanical Engineering, Rajadhani Institute of Engineering and Technology, Trivandrum, Kerala 695102 ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - The purpose of this thesis is to design and create a chassis frame for a harvesting automobile's harvesting mechanism. The focus of this research is on the viability of simple manufacturing at the lowest possible cost. The present industries have identified many types of chassis for forming equipment, particularly harvesting equipment. Those chassis are being investigated. Different harvesting equipment load scenarios are also investigated. Anewchassis designiscreated based on the findings of the investigation using Solidworks 2020. The harvesting part assemblies that were previously designed are assembled on the chassis using various bolts and plate connections to connect the various assembly parts. As previously stated, the Chassis is designed, developed, and verified for a variety of load scenariosusingAnsysWorkbench. Key Words: Chassis frame, Harvesting Automobile, Harvesting Mechanism, Solidworks, Assembly, Ansys, Load Scenarios. 1. INTRODUCTION Farming is one of the most important occupations for generating food and food productsall overthe world.Indiais one of the world's largest producers of rice, wheat, and vegetables. Farmers cultivate crops in a systematic manner at various times throughout the year. Every crop production requires a great deal of manual labor and physical effort. Engineers are working on a variety of semi-automated and mechanical machinery to aid in the growing of formals. We are developing a chassis frame for a tiny harvestingmachine in this thesis. Every automobile's chassis frame isa critical component.It's the foundation on which the vehicle's components are mounted. The vehicle's body is constructed on top of the chassis frame. When compared to a standard automobile chassis, the chassis frame of a harvesting machine carries a variety of loads. A vehicle chassis is designed and engineered to withstand loads resulting from various flat road conditions. However, harvesting machines work in fields with extremely uneven topography, putting extraordinary pressures on their chassis. A chassis in common bears all of the mechanical parts and the vehicle body, ensuring that the vehicle isbalancedonthe road or terrain. A chassis structure for the aforementioned micro harvester is designed in thisbachelorthesis.Theloads and load cases for the chassis to function is analyzed and verified for its durability. 1.1 CHASSIS Chassis is a French word that refers to the vehicle's frame components or primary structure. It is often referred to as a carrying unit. A chassis is the framework upon which a vehicle is constructed. It also supports numerous components that are installedonitwhilecarryingtheweight as well as permits smooth run over varying roadsurface.Itis comprised of steel and serves as the vehicle's backbone. All major units required to drive the vehicle, give it motion, and stop it is equipped on the chassis itself. 1.2 FUNCTIONS OF CHASSIS The following are the functions of the Chassis. It: Supports or bears the vehicle's body load. Provide space and a mounting position for various vehicle components. Supports the weight of the vehicle's different systems, such as the engine and transmission. Supports the weight of passenger and such varying loads. Withstands the strains caused by poor road conditions. Sustains vehicle stresses during braking and acceleration. 1.3TYPEOFLOADSACTINGUPONCHASSISFRAMES The loads operating on the chassis frame are as follows: Stationary loads refer to loads that are permanently attached to the vehicle, such as the chassis and body. Loads caused by unexpected events, such as head-on collisions. Loads resulting from vehicle irregularities and overloading. Short-duration loads: the vehicle load when turning or braking. Momentary loads, which are applied to the vehicle during rapid acceleration, sharp braking, and so on.
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 247 The weights applied when crossing terrains with irregular or uneven surfaces. 1.4 CLASSIFICATION OF CHASSIS FRAMES Chassis frames are classified into: Conventional Chassis or frame-full chassis This type of chassis comprises of two long members and suitable number of cross members to make a ladder form. It is usually seen in commercial vehicles such as trucks and busses and some SUVs. Some passenger vehicles still use this frame due to its high load capacity and strength anditspractical feasibilityof easy manufacturing. The major disadvantageisthatthe body tends to vibrate easily and the vehicle dynamics are drastically compromised when compared to the other types. Non-Conventional or Frameless Chassis It's also known as a uni-body chassis or a frameless chassis. This chassis does not have a ladder frame; instead, the body serves as a frame. It also supports all of the vehicle's elements and components. These are commonly utilized on most modern vehicles in the same way that traditional chassis are. 2. METHODOLOGY Following the research, extensiveexpertiseofconceptdesign with presumptive parameters, hand calculations, 3D modelling, material selections, and harvester operation systems with consideration of the target and objectives is gained. The design's outcomes were assessed and debated.A thorough conclusion is then reached in light of all the findings. Fig -1: Methodology 3. MODEL DESCRIPTION As illustrated in the diagram, the chassis geometry is put together with the following parts. The long-members,cross- members, and C-clamp are all part of the chassis frame geometry. Because these parts are identical, they can be mounted together appropriately to form a whole chassis assembly. Two of these long-members, three of these cross- members, and six of these C-clamps were utilized for the chassis sub-assembly alone. Fig -2: Cross-section dimension of the long member The chassis dimensional parameters were compared to information in reference journals and validated with Indian Standards (ISO) for practicality. Because this thesis is primarily concerned with cost reduction, all of the parts designed and used here will be manufacturedofsheetmetal, which is easily available and inexpensive. All of the planned pieces were tested for production viability using conventional sheet metal forming techniques like curling, punching, and blanking. The chassis structure was madeout of AISI 1045 Mild Steel, which is ideal for our application. AISI 1045 is a medium tensile low hardenability carbon steel generally with a typical tensilestrength range570-700 Mpa and Brinell hardness range 170 - 210. This type of steel exhibits medium tensile strength, good weldability and machinability, and high strength. Typically used in machinery parts, die forging, hot upsetting, gears, crankshafts, shafts, axles, bolts, studs, pinions, casters, and support plates. It approximatelyconstitutesof98.5%ofIron,
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 248 0.45% of Carbon, 0.74% of Manganese and less than 0.04% of Phosphorous. Fig -3: Lateral dimension of the long member Similar to that illustrated in the figures 2 and3,forthecross- members, the cross-sectional dimensionsweregiven26mm, 54mm and a thickness of 4mm respectively whereas the lateral dimensions were given the value of 790mm all witha tolerance of 0.5mm. Fig -4: Dimensions of the C-Clamp 3.2 HARVESTING EQUIPMENT Fig -5: Pre-designed outlook of the harvesting machinery Figure 5 depicts the pre-designed assembly of harvesting machinery components. For preliminary loadestimates,this equipment is considered to be made of alloy steel. Each portion of this apparatus is built in such a way that it may be made entirely of sheet metal, dramatically lowering the manufacturing costs. It was made a point throughout the design process to avoid using fillet or curves that would be incompatible with sheet metal forming methods. Fig -6: The internal parts and connections of the harvesting equipment on the chassis frame All of these parts were designed and developed in consideration with the present days existing outlook of the mini and conventional harvesting equipment.
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 249 Fig-7: Rear isometric view of the internal parts and connections of the harvesting equipment on the chassis frame 3.3 MATERIAL PROPERTIES Table -1: CHEMICAL COMPOSITION Table -2: MECHANICAL PROPERTIES Mechanical Properties Metric Imperial Hardness, Brinell 163 163 Hardness, Knoop (Converted from Brinell hardness) 184 184 Hardness, Rockwell B (Converted from Brinell hardness) 84 84 Hardness, Vickers (Converted from Brinell hardness) 170 170 Tensile Strength, Ultimate 565 MPa 81900 psi Tensile Strength, Yield 310 45000 psi MPa Elongation at Break (in 50 mm) 16.0 % 16.0 % Reduction of Area 40.0 % 40.0 % Modulus of Elasticity (Typical for steel) 200 GPa 29000 ksi Bulk Modulus (Typical for steel) 140 GPa 20300 ksi Poissons Ratio (Typical For Steel) 0.290 0.290 Shear Modulus (Typical for steel) 80 GPa 11600 ksi Table -3: PHYSICAL PROPERTIES Physical Properties Metric Imperial Density 7.87 g/cc 0.284 lb/in3 4. ANALYSIS OVERVIEW The analysis is done using Ansys Workbench 2022 R1. For the most ease and simplicity for an efficient analysis, from various reference journals and practical inferences,thetotal load consideration along by including a factor of safety of 3 which is the usual amount for factor of safety considered for steel, we came into the conclusion that 6000N is being applied on the chassis frame totally. From relevant journals which focuses on the load cases acting upon the chassis frames shows us that the cross-members of the structures are the weakest part of the chassis were most amount of deformation due to the applicationsofloadoccurs.Alsofrom engineering theories, we know thatifthecritical pointonthe structure withstands the total amount of load, then it is definite that the entire structure as a whole also withstands the load. Critical point is defined as the virtual point on any structure where when a load is applied is concentrated at maximum deformation is found. For our chassis frame, due to the above-mentioned highlights we can assume that the critical points is in the middle span of the cross- members. Element Content Carbon, C 0.420 - 0.50 % Iron, Fe 98.51 - 98.98 % Manganese, Mn 0.60 - 0.90 % Phosphorous, P ≤ 0.040 % Sulfur, S ≤ 0.050 %
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 250 Fig -8: The chassis assembly for analysis 4.1 SUPPORTS FOR LONG MEMBERS Fig –9: Red marking shows where the support reactions are applied at the bottom of the chassis frame On the observation that as thatofeverycommonvehicle,this would also take the use of four-wheels mechanism for the purpose of motion. Thesefourwheelsprovidesupportsfrom 4 corner regions. On assuming the supports by the four- wheel mechanism as foursupportreactions,wehaveapplied four-point loads at the places marked in red in the above given figure. This assumption was also made into consideration from various reference journals and practical observations. 4.2 SUPPORTS FOR CROSS-MEMBERS From the design we can see that the cross-members are attached to the long-members in a way that both the ends of the cross-members are fixed on the long-member with a C- clamp. On relating this to the engineering theories, we can significantly consider it as a beam with two ends fixed. For any beam with both ends fixed with have both horizontal and vertical reaction forces at both ends. Since we consider only vertical forces being applied for now, which also the major force here, the horizontal forces are neglected for the analysis, hence the horizontal support reactions are also neglected. 4.3 COORDINATE SYSTEMS Fig -10: Side view of the coordinates in the geometry As we can see in the diagram there are two coordinates for the geometry, in which one of them corresponds with the coordinate system for the chassis frame assembly and the other coordinate system withitsoriginhappeningtobefrom the centre of gravity of the entire machinery which includes both the harvesting equipment, the chassis and the parts connecting them. On detailed studies, for a particular load condition for our analysis when the machinery is moving along a 30-degree inclined path, the same load is to be applied with 30-degree inclination with respect to the vertical axis (y axis). For the same reason one more axis is created with 30 degrees of inclination with the vertical axis as like the above given figure demonstrates. 4.4 CONNECTIONS On defining the connections for the analysis of the imported geometry, the input was given that all the components are connected to each other as per the given constraints and the coincident faces. 4.5 MESHING ATTRIBUTES The above shown mesh in the diagram is generated with an element size of 1.e-002 m (1.094x10-2m)whichwasgiven by the adaptive sizing function available. The elements of mesh for the long members were considered triangle and for the Cross-members were considered rectangle. That is also taken into consideration for generating meshes from reference journals of such analysis.FortheC-clampsalsothe elements were considered triangles. Fromthedetailedmesh report available in the software, we can see that the total number of nodes are 78776 and the total number of elements present in this geometry is 21852.
6.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 251 Fig -10: View of mesh for the analysis 5. RESULT FOR DIFFERENT LOAD CASSES APPLIED 5.1 00 STATIC LOAD As per the analysis considerations previously mentioned in this thesis, for the practical case where only the dead load of the harvesting machinery is acting upon it when the machinery is static or kept stationery, the deformation for this scenario is obtained. Fig -11: Deformation for 0-degree load From the image we can see that the maximum deformation happening here is 0.0026375m which is visible to be happening at the previously assumedcritical point region on the cross-member. Fig -12: Isometric view of the deformation due to 0- degree static load 5.2 STATIC LOAD AT 300 INCLINATION Fig -13: Deformation for 30-degree static load On considering the practical application where the harvesting machinery taking its path of motion along a 30- degree inclined terrain, the static load due to the gravitational force would act in a way that it is acting inclined as much with respect to the inclination of the terrain. For that case study, we have inclined the load applied at an angle of 30 degrees with respect to the vertical axis (y axis) of the coordinate system employed for analysis. The deformation for such a case is thus obtained. From the analysis, we can see that the total magnitude of deformation occurred is 0.0030191m which also located near the critical point region of the cross-memberasstudied earlier.
7.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 252 Fig -14: Isometric view of deformation due to 30- degree static load 5.3 WHENONEOFTHESUPPORTREACTIONSFAIL This load condition came into consideration when in a practical scenario when one of its tyres falls into a pitch or breaks so that it fails to providethe support themachineryto rest normally. For this load condition study, we have removed one of its supportreactionsonthelongmemberand the dead load is applied vertically in order to act like the above-mentioned practical case and for this the total deformation is obtained. Fig -15: Deformation when one of the support reactions fail Here it is observed that the total deformation happening here is 0.0062253m for the described case. Fig -16: Side view of the deformation when one of the support reactions fail Fig -16: Isometric view of the deformation when one of the support reaction fails 6. VERIFICATION OF THE RESULTS 6.1 VERIFYING THE DEFORMATION OBTAINED FOR 0-DEGREE LOAD CASE Considering the cross-member as a beam with both ends fixed, but the horizontal support reactions are neglected because only vertical loads are applied, therefore there is no necessity of horizontal support reactions being formed. The total load of 6000N is applied all along the three cross- member, therefore for the calculation of deformation for a single beam, we need to consider only one-third of the total load which is 2000N. For a simply supported beam carrying a point load of2000N eccentrically, From data hand book of K Mahadevan we know, maximum deflection ymax, Where, W = load applied b = distance from point of load applied to the right support a = distance from point of load to the left support
8.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 253 E = Young’s Modulus I = Moment of Inertia for a C Section beam Here, W = 2000N a = 395mm b = 395mm E = 205 GPa (AISI 1045 Steel) a and b are equal as the load is considered as a point load here acting upon the centre of cross-member, but in real life practice the point of load applied may differ, thus the equation for eccentric loading is employed. Moment of Inertia ‘I’ for C section (from K. Mahadevan Data hand book), I = [bd3 – h3(b-t)] / 12 Fig -17: Cross sectional dimension of the cross member is illustrated in this diagram Here, b=26mm d=54mm t=4mm h=50mm For the given values, Moment of Inertia I = 112005.33 kgmm2 Thus, on substituting all the obtained values in the equation for maximum deflection, ymax =2.598mm which is equal to 0.002598m of deflection The obtained result on numerical calculation for deformation is almost similar to the deformation obtained on the computational analysis for the respective load condition. Hence the obtained results are successfully verified. 7. CONCLUSION The difference between the value of the deformation obtained from the numerical calculation and the simulation calculation has a negligible difference of 0.032mm. This implies that the load cases calculations through simulation are sufficiently accurate and can be considered as the result of the study. For both the 0 degree and 30-degree inclined load application it is observed that the maximum deformation is happening at the maximum allowable limit on the application of 6000N. The load of 6000N was considered including a factor of safety of 3 for steel as usual, which also makes it evident that practically this load is safe for the chassis to with stand. Since the aim of this thesis was to study the practical feasibility of manufacturing a chassisframewithsheetmetal, from the above static load conditions it is visible that it is visible that for this application as the chassis for harvesting machinery it is reliable. The primary objective of the design is to reduce the cost of the final product by involving sheet metal to manufacture all of the necessary components for this harvesting machinery and hence found successful in that aspect too. It is found that the chassis fails to withstand the load on the third load case study where one of the support reactionsfail. In that particular point of view, this thesis can be further studied to overcome the failure happening in that instance which makes this concept of using sheet metal for chassis a total success. ACKNOWLEDGEMENT First and foremost, I concede the surviving presenceandthe flourishing refinement of almighty GOD for his concealed hand yet substantial supervision all through the seminar. I extend my sincere gratitude to our Principal Dr.S.SURESH BABU., to his countenance towards the successful accomplishment of the course. I sincerely thank Dr. BINDU S.S., Head of the Department of Mechanical Engineering for valuable support, comments, advice, guidance and constant encouragement that enables me to complete the seminar on time.
9.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 254 I am thankful to my project guide Mr. SREERAJ M P., Assistant Professor and project coordinator Mr. KRISHNAKUMAR K., Assistant Professor in Mechanical Engineering department for his valuablesupportandadvice. I also express my indebt thanks to all the teaching and non- teaching staffs of Mechanical Engineering department. Finally, I am grateful to my parents, family members and my beloved friends for their help, encouragement and moral support given to me during the course of work. REFERENCES [1] D. Kornack and P. Rakic, “Cell Proliferation without Neurogenesis in Adult PrimateNeocortex,”Science,vol. 294, Dec. 2001, pp. 2127-2130, doi:10.1126/science.1065467. Apata, T. G., Linkages between Crude-oil Exploration and Agricultural Development in Nigeria: Implications for relevant qualitative data collectionandanalysis toimprove rural economy., 2010. [2] Olajide, O. T., Akinlabi, B. H., and Tijani,A.A.Agriculture Resource and Economic Growth in Nigeria. 2012. [3] Engineering Export Promotion Council (EEPC), Agricultural Machinery, Parts and Tractors Market in Nigeria., 2013. [4] Talabi, S. O. and Onasanya, O. Agricultural Introduction. 2013 22/09/2014] [5] Faborode, M. O. Strategies for sustainable National Agricultural Infrastructures Development. in Sustainable Engineering Infrastructures development. Port Harcourt: The Nigerian Society of Engineers,2001. [6] Akande, L. O., Empowerment of the Rural People through Agricultural Mechanization,Osun StateCollege of Education, 2006. [7] Lamidi, W. A. and Akande, L. O., A Study of Status, Challenges andProspectsof Agricultural Mechanization in Osun State, Nigeria. 1(1): p. 001 -008, 2013. [8] Takeshima, H. and Salau, S., Agricultural Mechanization and the Smallholder Farmers in Nigeria; Nigeria strategy support program, 2010. [9] Abdulkareem, Y. A., Indigenous Technology, Past, Present and Futures, in Workshop for the Processingof Raw Materials: Raw Materials Research and Development Council, 1992. [10] Adamade, C. A. and Jackson, B. A., Agricultural mechanization: a strategyfor foodsufficiency.Scholarly Journal of Agricultural Science. 4(3): p. 152-156, 2014. [11] Asoegwu, S., Agricultural Field Implements and Mechanization., 1998. [12] André-Michel, E. Despite recovery, Africa needs more jobs, says ECA. 2016. [13] Quick, G. R. and Buchele, W. F., The Grain Harvesters. American society ofagricultural engineers., 1978. [14] Olukunle, O. T., Developments in Grain Harvesting Mechanisation. Journal of Agricultural Engineeringand Technology (JAET). 18(1), 2010. [15] AMRI, Test Report Indian Combine Harvester SWARAJ-8100, Agricultural Mechanization Research Institute (AMRI), Multan Government of the Punjab, Lahore, 2014. [16] Ademosun, O. C., Adewumi, B. A., Olukunle, O. J., and Adesina, A. A., Development ofIndigenousMachinesfor Weeding and Grain Harvesting: FUTA Experience. FUTAJEET 3(2): p. 77-84, 2003. [17] BioSat Agricultural Biomass Sources. 2016. [18] Karande, O., Gauri, S. K., and Chakraborty, Applications of Utility Concept and Desirability Function for Materials Selection. Material and Design Journal 45: p. 349-358, 2012. [19] Shackelford, J. F., Introduction to Materials Science for Engineers. Fifth ed.: Prentice Hall, 2000. [20] Granta, Cambridge Engineering Selector (CES), Granta Design Limited, UK, 2014. [21] Childs, P. R. N., Mechanical Design. Second ed.: Oxford: Butterworth-Heinemann, 2003. [22] Khurmi, R. S. and Gupta, J. K., A Textbook ofMachine Design. Ram Nagar, New Delhi: Eurasia Publishing house, 2005. [23] Pahl, G., Beitz, W., Feldhusen, J., and Grote, K.- H., Engineering Design: A system Approach. Thirded., London: Springer-Verlag 2007. [24] Sapuan, S. M., A knowledge-based system for materials selection in mechanical engineering design. Materials & Design. 22(8): p. 687-695, 2001.
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