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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 656
Design Chassis For Onion Harvesters
Vaibhav Dhikale1, Rushikash Dhikale 2, Rahul Ghuge3
1Trainee Engineer, Mechanical Engineering Department, MCOEARC Odha Nashik ,Maharashtra, India
2Trainee Engineer, Mechanical Engineering Department, MCOEARC Odha Nashik ,Maharashtra, India
3Trainee Engineer, Mechanical Engineering Department ,MCOEARC Odha Nashik ,Maharashtra, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - The chassis for any vehicle is the most
important part as it becomes a structural backbone for
the support of different systems attached to it and
carries out the load of and also loads experienced by the
chassis is also an important aspect. Produce vehicle
chassis to mount all the systems required for harvesting
and propelling the harvester. Produce chassis to sustain
in all conditions. It should sustain all forces generated
during the harvesting of the farm which is due to soil
resistance. Making a lightweight chassis to reduce dead
weight on the vehicles without any compromise for the
safety of the driver. Making a lightweight chassis by
considering various rules and regulations given in the
SAE TIFAN rulebook while designing the chassis and also
understanding various specific cross sections for the
chassis fabrication is very important. In this various
software like Creo, Catia, and ANSYS have been used for
the process of doing modeling and Analysis of the chassis
frame.
Key Words: Chassis, TIFAN, Creo, Catia, ANSYS
1. INTRODUCTION
TIFAN is a national-level event that is held under
the banner of SAE International All undergraduate
students from all around the nation participate in
making the aesthetic, ergonomic, and safe chassis, for
the purpose of the competition. For this competition,
the teams strive to make the most well-designed
Harvester frame with all parameters considered.
Designing the chassis is the most important part for
any team, due to the fact that it supports all the
various departments of the whole vehicle. The design
should be made in such a way that it should not
compromise the driver's safety in any condition. The
design should not fail at any cost, it should have the
minimum required stiffness, strength, and torsional
rigidity, and it should be highly reliable and safe.
2. Analyses of Chassis and Calculation
Fig chassis sheet
3. Calculation of Chassis
Material of chassis selection = AISI 4130
• Chemical composition
Element Content
Iron 97.03-98.22%
Chromium 0.80-1.10%
Manganese 0.40-0.60%
Carbon 0.28-0.33%
Silicon 0.15-0.33%
Molybdenum 0.15-0.25%
Sulfur 0.04%
Phosphorous 0.035 %
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 657
• Mechanical properties
• Vehicle Dimensions
Parameter value
Length 2450 mm
Width 870 mm
Height 1500 mm
Ground clearance 270mm
• Cross section of chassis Hollow
Diameter of chassis (D) = 25mm
Thickness of chassis (t) = 3mm
1. Calculations of Bending Strength for The Chassis
Cross Section Formula for bending
Bending strength = Sy*I/C
Where
Syt = Yield Strength
I = Moment of Inertia
C = Extreme Fiber Distance
Given: Syt = 460 MPa = 460*106 N/m2 ,
C = D/2 = 0.025/2 = 0.0125 m
D = 0.025 m, d = 0.019 m
I = ᴫ/64 (D4-d4)
= ᴫ/64 (0.01254- 0.0194)
= 1.277*10-8 mm4
Bending strength = Syt*I/C
= (460*106) (1.277*10-8)/(0.0125)
Bending strength = 469.936 N-m
2. Loading Diagram
2.1 Load at point P1=10Kg
2.2 Load at point P2=10Kg
2.3 Load at point P3=23Kg
2.4 Load at point P4=26Kg
2.5 Load at point P5=40Kg
2.6 Load at point P6=23Kg
2.7 Load at point P7=63kg
2.8 Load at point P8=25Kg
2.9 Load at point P9=105Kg
2.10 Load at point P10=25Kg
2.11 Load at point P11=35Kg
2.12 Load at point P12=4.5Kg
2.13 Load at point P13=4.5Kg
System Point load
Steering system P1,P2
Setting arrangement P3,P6
Digging system P4
Transmission system P5,P7
Conveyer system P9,P10
Hydraulic system P4,P9
Separating system P11,P12,P13
Fig. Loading Diagram
3. G force calculation
Given:
Assumptions,
Front impact time taken = 0.15
Rear impact time taken = 0.3
Side impact time taken = 0.3
Properties Metric
Tensile strength, ultimate 560 MPa
Tensile strength, yield 460 MPa
Modulus of elasticity 190-210 GPa
Bulk modulus 140 GPa
Shear modulus 80 GPa
Passions ratio 0.27-0.30
Elongation at break 59.6
Hardness, Brinell 217
Hardness. Knoop 240
Hardness, Rockwell 95
Hardness. Vickers 228
Machinability 70
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 658
3.1Calculating G force for front impact
Velocity of vehicle = 5.27 m/s
Mass of vehicle = 394 kg
By using formula
V = U+A*T
=5.27+a*(0.15)
= 35.133 m/s2
We, know
Force = mass*acceleration
= 394*35.133
= 13842.53 N
G Force = force / (mass of vehicle*9.8)
= 13842.53/(394*9.8)
G Force = 3.71
FEA Analysis of frame (front impact) Load = 3.71 G
Fig. Front Impact Diagram
Fig. Front Impact Stress Diagram
3.2 Calculating G force for side impact
Velocity of vehicle = 5.27 m/s
Mass of vehicle = 394 kg By using formula
V = U+A*T
V = 5.27+A(0.3)
= 17.566 m/s2
We, know
Force = mass*acceleration
= 394*17.566
=6921.004 N
G Force = force / (mass of vehicle*9.8)
= 6921.004/(394*9.8)
G Force = 1.85
FEA Analysis of frame (side impact) Load = 1.85 G
Fig. Side Impact Diagram
Fig. Side Impact Stress Diagram
3.3 Calculating G force for rear impact
Velocity of vehicle = 5.27 m/s
Mass of vehicle = 394 kg By using formula
V = U+A*T
= 5.27+A*(0.3)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 659
= 17.566 m/s2
We, know
Force = mass*acceleration
= 394*17.566
=6921.004 N
G Force = force / (mass of vehicle*9.8)
= 6921.004/ (394*9.8)
G Force = 1.85
FEA Analysis of frame (rear impact) Load = 1.85 G
Fig. Rear Impact Diagram
Fig. Rear Impact Stress Diagram
3.4Factor of safety calculation
1) Factor of safety front impact
Maximum stress induces at front section = 396.6 MPa
Yield strength of material = 460 MPa
F.O.S =460/396.63 = 1.1
2) Factor of safety side impact
Maximum stress induces at side section = 269.2MPa
Yield strength of material = 460 MPa
F.O.S =460/269.27 = 1.17
3) Factor of safety rear impact
Maximum stress induces at rear section = 84.2 MPa
Yield strength of material = 460 MPa
F.O.S = 460/84.2 = 5.46
3.5 Mounting Calculation
Properties table
Property’s Metric
Yield strength 250Mpa
Tensile strength 410 Mpa
% Elongation (At gauge length @
5.65 )
23 %
Chemical properties
Element Content `
Carbon 0.23% max
Silicon 0.40% max
Manganese 1.50
Phosphorous 0.045
Sulfur 0.045
Cross section = C - Cross section
Width =40 mm
Height =75 mm
Thickness of web = 3.7 mm
Thickness of flange = 6 mm
Total length = 650 mm
Bending strength = Sy*I/C
Moment of Inertia = Ixx=76 cm4, Iyy = 12.6 cm4
I = Ixx+Iyy = 76 +12.6 = 88.6 *10-8mm4
Bending strength = 250*(88.6*10-8)/ (0.0375)
= 5906 Nm
Fig. C Section Plate Diagram
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 660
Fig. C Section Plate Impact Diagram
Fig. C Section Plate Stress Diagram Max
Deformation = 0.068 mm
Max Stress = 14.283 MPa
FOS = Yield Strength / Max Stress
= 250/14.283 = 17.50
4. Case study
Over all view of analysis
Analysis Load Stress F.O.S
Front Impact 3.71G 396.63 Mpa 1.1
Side Impact 1.85G 269.27 Mpa 1.17
Rear Impact 1.85G 84.2 Mpa 5.46
5. Conclusion
To study chassis design and analysis of chassis for
requires machine. Different machine have different
chassis criteria has per change its formula for design.
We study the how to chassis design and
manufacturing the chassis for onion harvester
Fig. CHHATRAPATI HARVESTER
We have created the final product after completing
the chassis, mounting manufacturing, and all system
fittings. As a Mechanical Engineer, I am proud that the
final product looks great and fully functional.
REFERENCES
[1] Smita, C. Saddu, Modeling and analysis of composite as
an alternative material for leaf spring, volume 11,
Issue IV (Mayjune 2014) , PP 39-44..
[2] J. William Fitch, “Motor Truck Engineering
HandbookFourth edition” SAE Inc, Warrendale, U.S.A,
1993.
[3] AutarK.Kaw. Mechanics of Composite Materials. 2e.
Taylor and Francis Group, LLc , 2006..
[4] N V Dhandapani, G Mohan kumar, K K Debnath, “Static
analysis of Off-High way vehicle Chassis structure for
the effect of various stress distributions”, Journal of
Mechanical Science and Technology, Vol.1, No 6, 2012.
[5] Ojo Kurdi, Roslan Abdul Rahman, “Finite Element
Analysis of Road Roughness Effect on Stress
Distribution of Heavy Duty TruckChassis”,
International Journal of Technology, Vol.1, PP 57-64,
2010.
[6] Cicek Karaoglu, N. Sefa Kuralay, “Stress analysis of a
truck chassis with riveted joints”, Finite Elements in
Analysis and Design, Vol.38, PP 1115–1130, 2002.
[7] ]. Haval Kamal Asker1 and Arkan Fawzi, “Stress
Analysis of Standard Truck Chassis During Ramping
On Block Using Finite Element Method”, JUNE 2012.
[8] B. Subhramanyam, Mahesh Kolati, Vishal, K Praveen
Kumar, “Analysis of Formula Student Race Car”,
International Journal of Engineering Research &
Technology (IJERT) ISSN: 2278-0181, Vol. 5 Issue 10,
October-2016
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 661
[9] Surve Aditya, Naik Vishal, Naikar Aditya, Mohd. Raees,
“ANALYSIS OF FSAE CHASSIS”, International Journal
of Scientific & Engineering Research Volume 9, Issue
3, March-2018 40 ISSN 2229-5518.
BIOGRAPHIES
Mr. Dhikale Vaibhav B.
Mechanical Engineer
Mathoshri College Of Engineering
Nashik, Maharashtra
Mr. Dhikale Rushikash
Mechanical Engineer
Mathoshri College Of Engineering
Nashik, Maharashtra
Mr. Ghuge Rahul
Mechanical Engineer
Mathoshri College Of Engineering
Nashik, Maharashtra

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Design Chassis For Onion Harvesters

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 656 Design Chassis For Onion Harvesters Vaibhav Dhikale1, Rushikash Dhikale 2, Rahul Ghuge3 1Trainee Engineer, Mechanical Engineering Department, MCOEARC Odha Nashik ,Maharashtra, India 2Trainee Engineer, Mechanical Engineering Department, MCOEARC Odha Nashik ,Maharashtra, India 3Trainee Engineer, Mechanical Engineering Department ,MCOEARC Odha Nashik ,Maharashtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - The chassis for any vehicle is the most important part as it becomes a structural backbone for the support of different systems attached to it and carries out the load of and also loads experienced by the chassis is also an important aspect. Produce vehicle chassis to mount all the systems required for harvesting and propelling the harvester. Produce chassis to sustain in all conditions. It should sustain all forces generated during the harvesting of the farm which is due to soil resistance. Making a lightweight chassis to reduce dead weight on the vehicles without any compromise for the safety of the driver. Making a lightweight chassis by considering various rules and regulations given in the SAE TIFAN rulebook while designing the chassis and also understanding various specific cross sections for the chassis fabrication is very important. In this various software like Creo, Catia, and ANSYS have been used for the process of doing modeling and Analysis of the chassis frame. Key Words: Chassis, TIFAN, Creo, Catia, ANSYS 1. INTRODUCTION TIFAN is a national-level event that is held under the banner of SAE International All undergraduate students from all around the nation participate in making the aesthetic, ergonomic, and safe chassis, for the purpose of the competition. For this competition, the teams strive to make the most well-designed Harvester frame with all parameters considered. Designing the chassis is the most important part for any team, due to the fact that it supports all the various departments of the whole vehicle. The design should be made in such a way that it should not compromise the driver's safety in any condition. The design should not fail at any cost, it should have the minimum required stiffness, strength, and torsional rigidity, and it should be highly reliable and safe. 2. Analyses of Chassis and Calculation Fig chassis sheet 3. Calculation of Chassis Material of chassis selection = AISI 4130 • Chemical composition Element Content Iron 97.03-98.22% Chromium 0.80-1.10% Manganese 0.40-0.60% Carbon 0.28-0.33% Silicon 0.15-0.33% Molybdenum 0.15-0.25% Sulfur 0.04% Phosphorous 0.035 %
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 657 • Mechanical properties • Vehicle Dimensions Parameter value Length 2450 mm Width 870 mm Height 1500 mm Ground clearance 270mm • Cross section of chassis Hollow Diameter of chassis (D) = 25mm Thickness of chassis (t) = 3mm 1. Calculations of Bending Strength for The Chassis Cross Section Formula for bending Bending strength = Sy*I/C Where Syt = Yield Strength I = Moment of Inertia C = Extreme Fiber Distance Given: Syt = 460 MPa = 460*106 N/m2 , C = D/2 = 0.025/2 = 0.0125 m D = 0.025 m, d = 0.019 m I = ᴫ/64 (D4-d4) = ᴫ/64 (0.01254- 0.0194) = 1.277*10-8 mm4 Bending strength = Syt*I/C = (460*106) (1.277*10-8)/(0.0125) Bending strength = 469.936 N-m 2. Loading Diagram 2.1 Load at point P1=10Kg 2.2 Load at point P2=10Kg 2.3 Load at point P3=23Kg 2.4 Load at point P4=26Kg 2.5 Load at point P5=40Kg 2.6 Load at point P6=23Kg 2.7 Load at point P7=63kg 2.8 Load at point P8=25Kg 2.9 Load at point P9=105Kg 2.10 Load at point P10=25Kg 2.11 Load at point P11=35Kg 2.12 Load at point P12=4.5Kg 2.13 Load at point P13=4.5Kg System Point load Steering system P1,P2 Setting arrangement P3,P6 Digging system P4 Transmission system P5,P7 Conveyer system P9,P10 Hydraulic system P4,P9 Separating system P11,P12,P13 Fig. Loading Diagram 3. G force calculation Given: Assumptions, Front impact time taken = 0.15 Rear impact time taken = 0.3 Side impact time taken = 0.3 Properties Metric Tensile strength, ultimate 560 MPa Tensile strength, yield 460 MPa Modulus of elasticity 190-210 GPa Bulk modulus 140 GPa Shear modulus 80 GPa Passions ratio 0.27-0.30 Elongation at break 59.6 Hardness, Brinell 217 Hardness. Knoop 240 Hardness, Rockwell 95 Hardness. Vickers 228 Machinability 70
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 658 3.1Calculating G force for front impact Velocity of vehicle = 5.27 m/s Mass of vehicle = 394 kg By using formula V = U+A*T =5.27+a*(0.15) = 35.133 m/s2 We, know Force = mass*acceleration = 394*35.133 = 13842.53 N G Force = force / (mass of vehicle*9.8) = 13842.53/(394*9.8) G Force = 3.71 FEA Analysis of frame (front impact) Load = 3.71 G Fig. Front Impact Diagram Fig. Front Impact Stress Diagram 3.2 Calculating G force for side impact Velocity of vehicle = 5.27 m/s Mass of vehicle = 394 kg By using formula V = U+A*T V = 5.27+A(0.3) = 17.566 m/s2 We, know Force = mass*acceleration = 394*17.566 =6921.004 N G Force = force / (mass of vehicle*9.8) = 6921.004/(394*9.8) G Force = 1.85 FEA Analysis of frame (side impact) Load = 1.85 G Fig. Side Impact Diagram Fig. Side Impact Stress Diagram 3.3 Calculating G force for rear impact Velocity of vehicle = 5.27 m/s Mass of vehicle = 394 kg By using formula V = U+A*T = 5.27+A*(0.3)
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 659 = 17.566 m/s2 We, know Force = mass*acceleration = 394*17.566 =6921.004 N G Force = force / (mass of vehicle*9.8) = 6921.004/ (394*9.8) G Force = 1.85 FEA Analysis of frame (rear impact) Load = 1.85 G Fig. Rear Impact Diagram Fig. Rear Impact Stress Diagram 3.4Factor of safety calculation 1) Factor of safety front impact Maximum stress induces at front section = 396.6 MPa Yield strength of material = 460 MPa F.O.S =460/396.63 = 1.1 2) Factor of safety side impact Maximum stress induces at side section = 269.2MPa Yield strength of material = 460 MPa F.O.S =460/269.27 = 1.17 3) Factor of safety rear impact Maximum stress induces at rear section = 84.2 MPa Yield strength of material = 460 MPa F.O.S = 460/84.2 = 5.46 3.5 Mounting Calculation Properties table Property’s Metric Yield strength 250Mpa Tensile strength 410 Mpa % Elongation (At gauge length @ 5.65 ) 23 % Chemical properties Element Content ` Carbon 0.23% max Silicon 0.40% max Manganese 1.50 Phosphorous 0.045 Sulfur 0.045 Cross section = C - Cross section Width =40 mm Height =75 mm Thickness of web = 3.7 mm Thickness of flange = 6 mm Total length = 650 mm Bending strength = Sy*I/C Moment of Inertia = Ixx=76 cm4, Iyy = 12.6 cm4 I = Ixx+Iyy = 76 +12.6 = 88.6 *10-8mm4 Bending strength = 250*(88.6*10-8)/ (0.0375) = 5906 Nm Fig. C Section Plate Diagram
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 660 Fig. C Section Plate Impact Diagram Fig. C Section Plate Stress Diagram Max Deformation = 0.068 mm Max Stress = 14.283 MPa FOS = Yield Strength / Max Stress = 250/14.283 = 17.50 4. Case study Over all view of analysis Analysis Load Stress F.O.S Front Impact 3.71G 396.63 Mpa 1.1 Side Impact 1.85G 269.27 Mpa 1.17 Rear Impact 1.85G 84.2 Mpa 5.46 5. Conclusion To study chassis design and analysis of chassis for requires machine. Different machine have different chassis criteria has per change its formula for design. We study the how to chassis design and manufacturing the chassis for onion harvester Fig. CHHATRAPATI HARVESTER We have created the final product after completing the chassis, mounting manufacturing, and all system fittings. As a Mechanical Engineer, I am proud that the final product looks great and fully functional. REFERENCES [1] Smita, C. Saddu, Modeling and analysis of composite as an alternative material for leaf spring, volume 11, Issue IV (Mayjune 2014) , PP 39-44.. [2] J. William Fitch, “Motor Truck Engineering HandbookFourth edition” SAE Inc, Warrendale, U.S.A, 1993. [3] AutarK.Kaw. Mechanics of Composite Materials. 2e. Taylor and Francis Group, LLc , 2006.. [4] N V Dhandapani, G Mohan kumar, K K Debnath, “Static analysis of Off-High way vehicle Chassis structure for the effect of various stress distributions”, Journal of Mechanical Science and Technology, Vol.1, No 6, 2012. [5] Ojo Kurdi, Roslan Abdul Rahman, “Finite Element Analysis of Road Roughness Effect on Stress Distribution of Heavy Duty TruckChassis”, International Journal of Technology, Vol.1, PP 57-64, 2010. [6] Cicek Karaoglu, N. Sefa Kuralay, “Stress analysis of a truck chassis with riveted joints”, Finite Elements in Analysis and Design, Vol.38, PP 1115–1130, 2002. [7] ]. Haval Kamal Asker1 and Arkan Fawzi, “Stress Analysis of Standard Truck Chassis During Ramping On Block Using Finite Element Method”, JUNE 2012. [8] B. Subhramanyam, Mahesh Kolati, Vishal, K Praveen Kumar, “Analysis of Formula Student Race Car”, International Journal of Engineering Research & Technology (IJERT) ISSN: 2278-0181, Vol. 5 Issue 10, October-2016
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 09 | Sep 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 661 [9] Surve Aditya, Naik Vishal, Naikar Aditya, Mohd. Raees, “ANALYSIS OF FSAE CHASSIS”, International Journal of Scientific & Engineering Research Volume 9, Issue 3, March-2018 40 ISSN 2229-5518. BIOGRAPHIES Mr. Dhikale Vaibhav B. Mechanical Engineer Mathoshri College Of Engineering Nashik, Maharashtra Mr. Dhikale Rushikash Mechanical Engineer Mathoshri College Of Engineering Nashik, Maharashtra Mr. Ghuge Rahul Mechanical Engineer Mathoshri College Of Engineering Nashik, Maharashtra