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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 892
MODELLING AND ANALYSIS OF TWO WHEELER SUSPENSION SYSTEM
A. Harshavardhan Reddy1, G. Rajasekhar Reddy2, G. Phanindra3, K. Vijay Kumar4
1 Asst. Professor, Mechanical, Gurunanak Institutions, Telangana, India
2,3,4 Student, Mechanical, Gurunanak Institutions, Telangana, India
---------------------------------------------------------------------***-------------------------------------------------------------------
ABSTRACT - A suspension system or shock absorber is a
mechanical device designed to duty is to absorb or dissipate
energy. In a vehicle, it reduces the effect of travelling over
rough ground, leading to improved ride quality, and
increase in comfort due to substantially reduced amplitude
of disturbances. The design of spring in suspension system is
very important.
In this project a shock absorber is designed a 3D model
software using solid works. The model is also changed by
changing the material and load of the spring.
Structural analysis and is done on the shock absorber by
varying material for spring, magnesium, steel and titanium.
The analysis is done by considering loads, bike weight, single
person and 2 persons. Structural analysis is done to validate
the strength and static structural analysis is done to
determine the total displacements for different loads and
materials. Comparison is done for three materials to verify
best material for Shock absorber.
Key Words: ANSYS, Damp Stock, Kinetic Energy, Ride
Quality, SOLID WORKS.
1. INTRODUCTION TO SUSPENSION SYSTEM
Shock absorbers are important part of vehicle's
suspension- which is fabricated to reduce shock impulse.
Shock absorber minimizes the effect of travelling on a
rough ground. Modern vehicles are designed with strong
shock absorbers to tolerate any type of bouncy conditions.
If supposedly shock absorber is not used then to control
excessive suspension movement- stiffer springs will be
used. The shock absorbers duty is to absorb or dissipate
energy. One design consideration- when designing or
choosing a Shock absorber is where that energy will go. In
most dashpots- energy is converted to heat inside the
viscous fluid.
1.2 Literature Review
For providing the best design of spring coil to the
suspension system of two wheeler vehicles. A lot of
technical papers and reduction processes were studied
before deciding upon the most feasible process for project.
The following list presents a gist of the main papers
referred to, throughout the duration of the project.
1.3 Construction and Working
Construction
Fig. 1 Construction
Components are:
1. Rod
2. The piston with seals.
3. Cylinder.
4. Oil reservoir.
5. Floating piston.
6. Air chamber
2. MODELING OF COMPONENT
Part 1: Lower Shaft
To create go to SOLIDWORKS software and click
on start –and select part design module. In part design
module then go to sketcher tool and select sketcher tool
and select required plane. Then we enter into sketcher
module and go to profile and create a profile structure as
shown in fig.
FIG.2 Sketch for Lower Suspension
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 893
After completing sketcher go to workbench and
select exit work bench. Then we enter into part module
again. In part module, go to HELIX TOOL and select shaft
tool. In shaft definition, select above sketch as sele ction
profile and specify angle as shown in fig
FIG.3 Spring
Now again, in part design module then go to
sketcher tool and select sketcher tool and select required
plane. Then we enter into sketcher module and go to
profile and create a profile structure as shown in fig.
FIG.4 Sketch for Locker
After completing sketcher go to workbench and
select exit work bench. Then we enter into part module
again. In part module, feature tool and select pad tool. In
pad definition, select above sketch as selection profile and
specify length as shown in fig and click on mirrored extent
option.
FIG.5 Pad for Lock
In part modules go to dress up based feature and
select edge fillet tool. In edge fillet definition, Select edge
of developed part and from dress up features select edge
fillet and make fillet with 5mm radius.
FIG.6 Fillet for Support
Part 2: Upper Suspension Shaft
To create go to catia software and click on start –
mechanical design and select part design module. In part
design module then go to sketcher tool and select sketcher
tool and select required plane. Then we enter into
sketcher module and go to profile and create a profile
structure as shown in fig.
FIG.7 Sketch for Upper Suspension
After completing sketcher go to workbench and
select exit work bench. Then we enter into part module
again. In part module, go to sketcher based feature and
select shaft tool. In shaft definition, select above sketch as
selection profile and specify angle as shown in fig
FIG.8 Shaft Definition
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 894
In part design module then go to sketcher tool and
select sketcher tool and select required plane or surface.
Then we enter into sketcher module and go to profile and
create a profile structure as shown in fig
FIG.8 Sketch for Lock
After completing sketcher go to workbench and
select exit work bench. Then we enter into part module
again. In part module, go to sketcher based feature and
select pad tool. In pad definition, select above sketch as
selection profile and specify length as shown in fig
FIG.9 Pad for Lock
In part design from dress up features select edge
fillet at the edge with given dimension as shown below.
Part 3: Spring
To create go to SOLID WORKS software and click
on start –mechanical design and select wireframes and
surface design module. In wireframes and surface design
module then go to sketcher tool bar and select sketch and
select yz plane. Then we enter into sketcher module, then
go profile tool and select line tool and specify as shown in
fig then click on exit workbench
FIG.10 Varying Length for Different Pitch
In wireframes and surface design module then go
to wireframe tool bar and select helix tool. In helix
definition select above point as a starting point and z axis
a reference axis. Then specify pitch and height as shown in
fig.
FIG.11 Helix Definition
FIG.12 Creating Spring Inside Definition
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 895
In wireframes and surface design module then go
to wireframe tool bar and select helix tool. In helix
definition select above point as a starting point and z axis
a reference axis. Then specify pitch and height as shown in
fig.
FIG.13 Creating Fillets
In wireframes and surface design module then go
to operation and select join. In join definition select all
three helix as show in fig. then ok to make one single helix.
FIG.14 Rib Definition
Now select front plane and go to sketcher in
sketcher from profile tool bar select rectangle and draw a
rectangle on bottom side as shown below. Exit from
workbench in part design from sketch based features
select pocket .In pocket definition specify as per given
diagram and select reverse side then click ok
FIG.15 Remove or Making Flat Support for Spring
Part 4: Watcher
Go to SOLID WORKS software and click on start –
mechanical design and select part design module. In part
design module then go to sketcher tool and select sketcher
tool and select required plane. Then we enter into
sketcher module and go to profile and create a profile
structure as shown in fig.
FIG.16 Sketch for Watcher
After completing sketcher go to workbench and
select exit work bench. Then we enter into part module
again. In part module, go to sketcher based feature and
select shaft tool. In shaft definition, select above sketch as
selection profile and specify angle as shown in fig
FIG.17 Pad Definition
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 896
3. Assembly of model component
FIG.18 ASSEMBLE PART
PROCESS OF ANALSING IN ANSYS
Static Structural Analysis with Different Materials
FIG.19 Project and its Parts
After importing the model into project schematic
window drag and drop the Static structural analysis tab on
to the screen from the toolbox window and link the
geometry to geometry both will be linked together. Double
click on the model it opens the mechanical window with
object.
IMPORTED PART
FIG.20Imported Geometry
FIG.21 Contact Region
4. STRACTURAL ANALYSIS
STEEL MATERIAl
Total deformation & equivalent stress by applying of 50KG
load
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 897
Fig.22 Total deformation & equivalent stress
Total deformation & equivalent stress by applying of
125KG load
Fig.23 Total deformation & equivalent stress
Total deformation & equivalent stress by applying of
200KG load
Fig.24 Total deformation & equivalent stress
MAGNESIUM MATERIAL
Total deformation & equivalent stress by applying of 50KG
load
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 898
Fig.25 Total deformation & equivalent stress
Total deformation & equivalent stress by applying of
125KG load
Fig.26 Total deformation & equivalent stress
Total deformation & equivalent stress by applying of
200KG load
Fig.27 Total deformation & equivalent stress
TITANIUM MATERIAL
Total deformation & equivalent stress by applying of 50KG
load
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 899
Fig.28 Total deformation & equivalent stress
Total Deformation & Equivalent Stress By Applying Of
125KG Load
Fig.29 Total deformation & equivalent stress
Total deformation & equivalent stress by applying of
200KG load
Fig.30 Total deformation & equivalent stress
5. MODEL ANALYSIS
Total Deformation and Frequency Range in Steel Material
Fig .31 Total Deformation and Frequency Range in Steel
Material
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 900
Total Deformation and Frequency Range in Magnesium
Fig.32 Total Deformation and Frequency Range in
Magnesium
Total Deformation and Frequency Range in Titanium
Fig.33 Total Deformation And Frequency Range In
Titanium
STEEL MATERIAL DATA
TABLE 18
Structural Steel > Constants
Density 7850 kg m^-3
Coefficient of Thermal Expansion 1.2e-005 C^-1
Specific Heat 434 J kg^-1 C^-1
Thermal Conductivity 60.5 W m^-1 C^-1
Resistivity 1.7e-007 ohm m
MAGNESIUM DATA
Magnesium Alloy > Constants
Density 1800 kg m^-3
Coefficient of Thermal Expansion 2.6e-005 C^-1
Specific Heat 1024 J kg^-1 C^-1
Thermal Conductivity 156 W m^-1 C^-1
Resistivity 7.7e-007 ohm m
TITANIUM DATA
Titanium Alloy > Constants
Density 4620 kg m^-3
Coefficient of Thermal Expansion 9.4e-006 C^-1
Specific Heat 522 J kg^-1 C^-1
Thermal Conductivity 21.9 W m^-1 C^-1
Resistivity 1.7e-006 ohm m
TABLE 1 Results and Comparison
TOTAL DEFORMATION& EQUIVALENT STRESS
TOTAL DEFORMATION& EQUIVALENT STRESS Graph
S NO MATERIAL LOADS Total Deformation MmEquivalent Stress
50 1.31E-06 4.47E+06
50+75 3.27E-06 1.11E+07
50+75+75 5.24E-06 1.80E+07
50 5.80E-06 4.42E+06
50+75 1.45E-05 1.11E+07
50+75+75 2.32E-05 1.77E+07
50 2.72E-06 4.40E+06
50+75 6.80E-06 1.10E+07
50+75+75 1.09E-05 1.76E+073 TITANIUM
1 STEEL
2 MAGNESIUM
0.00E+00
5.00E+06
1.00E+07
1.50E+07
2.00E+07
Total
Deformation Mm
Equivalent Stress
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 901
FREQUENCY VARIATION IN STEEL MATERIAL
FREQUENCY VARIATION IN MAGNESIUM MATERIAL
FREQUENCY VARIATION IN TITANIUM MATERIAL
CONCLUSION
In our project we have designed a shock absorber
used in a 150cc bike .We modeled shock absorber By using
SOLID WORKS. To validate the strength of our design, we
have done structural analysis and modal analysis on the
shock absorber. We have done analysis by varying spring
material is Steel, magnesium and titanium. By observing
the analysis results, the analyzed stress values are less
than their respective yield stress values. So our design is
safe. .By comparing the results for both materials, the
stress value is less for titanium than steel and magnesium.
Also the shock absorber design is modified by changes the
diameter 2mm and loads 50kg, 125kg and 200kg and
structural, modal analysis is done on the shock absorber.
By comparing the results for both materials, the stress
value is less for titanium than steel and magnesium. By
comparing the results for present design and modified
design, the stress and displacement values are less for
modified design.
REFERENCES
1. Reza N. Jazar (2008). Vehicle Dynamics: Theory
and Applications. Spring. p. 455. Retrieved 2012-
06-24.
2. "Suspension Basics 1 - Why We Need It". Initial
Dave. Retrieved 2015-01-29.
3. Adams, William Bridges (1837). English Pleasure
Carriages. London: Charles Knight & Co.
4. "Suspension Basics 3 - Leaf Springs". Initial Dave.
Retrieved 2015-01-29.
5. "wagon and carriage".
6. "The Washington Times, Sunday 30 June 1901".
Chroniclingamerica.loc.gov. Retrieved2012-08-16.
7. Jain, K.K.; Asthana, R.B. Automobile Engineering.
London: Tata McGraw-Hill. pp. 293– 294. ISBN 0-
07-044529-X. 12. Pages 617-620 (particularly page
619) of "Race Car Vehicle Dynamics" by William
and Douglas Milliken
8. R.S. Khurmi & J.K Gupta (2003), “A textbook of
machine design”, S. Chand & company.

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IRJET- Modelling and Analysis of Two Wheeler Suspension System

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 892 MODELLING AND ANALYSIS OF TWO WHEELER SUSPENSION SYSTEM A. Harshavardhan Reddy1, G. Rajasekhar Reddy2, G. Phanindra3, K. Vijay Kumar4 1 Asst. Professor, Mechanical, Gurunanak Institutions, Telangana, India 2,3,4 Student, Mechanical, Gurunanak Institutions, Telangana, India ---------------------------------------------------------------------***------------------------------------------------------------------- ABSTRACT - A suspension system or shock absorber is a mechanical device designed to duty is to absorb or dissipate energy. In a vehicle, it reduces the effect of travelling over rough ground, leading to improved ride quality, and increase in comfort due to substantially reduced amplitude of disturbances. The design of spring in suspension system is very important. In this project a shock absorber is designed a 3D model software using solid works. The model is also changed by changing the material and load of the spring. Structural analysis and is done on the shock absorber by varying material for spring, magnesium, steel and titanium. The analysis is done by considering loads, bike weight, single person and 2 persons. Structural analysis is done to validate the strength and static structural analysis is done to determine the total displacements for different loads and materials. Comparison is done for three materials to verify best material for Shock absorber. Key Words: ANSYS, Damp Stock, Kinetic Energy, Ride Quality, SOLID WORKS. 1. INTRODUCTION TO SUSPENSION SYSTEM Shock absorbers are important part of vehicle's suspension- which is fabricated to reduce shock impulse. Shock absorber minimizes the effect of travelling on a rough ground. Modern vehicles are designed with strong shock absorbers to tolerate any type of bouncy conditions. If supposedly shock absorber is not used then to control excessive suspension movement- stiffer springs will be used. The shock absorbers duty is to absorb or dissipate energy. One design consideration- when designing or choosing a Shock absorber is where that energy will go. In most dashpots- energy is converted to heat inside the viscous fluid. 1.2 Literature Review For providing the best design of spring coil to the suspension system of two wheeler vehicles. A lot of technical papers and reduction processes were studied before deciding upon the most feasible process for project. The following list presents a gist of the main papers referred to, throughout the duration of the project. 1.3 Construction and Working Construction Fig. 1 Construction Components are: 1. Rod 2. The piston with seals. 3. Cylinder. 4. Oil reservoir. 5. Floating piston. 6. Air chamber 2. MODELING OF COMPONENT Part 1: Lower Shaft To create go to SOLIDWORKS software and click on start –and select part design module. In part design module then go to sketcher tool and select sketcher tool and select required plane. Then we enter into sketcher module and go to profile and create a profile structure as shown in fig. FIG.2 Sketch for Lower Suspension
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 893 After completing sketcher go to workbench and select exit work bench. Then we enter into part module again. In part module, go to HELIX TOOL and select shaft tool. In shaft definition, select above sketch as sele ction profile and specify angle as shown in fig FIG.3 Spring Now again, in part design module then go to sketcher tool and select sketcher tool and select required plane. Then we enter into sketcher module and go to profile and create a profile structure as shown in fig. FIG.4 Sketch for Locker After completing sketcher go to workbench and select exit work bench. Then we enter into part module again. In part module, feature tool and select pad tool. In pad definition, select above sketch as selection profile and specify length as shown in fig and click on mirrored extent option. FIG.5 Pad for Lock In part modules go to dress up based feature and select edge fillet tool. In edge fillet definition, Select edge of developed part and from dress up features select edge fillet and make fillet with 5mm radius. FIG.6 Fillet for Support Part 2: Upper Suspension Shaft To create go to catia software and click on start – mechanical design and select part design module. In part design module then go to sketcher tool and select sketcher tool and select required plane. Then we enter into sketcher module and go to profile and create a profile structure as shown in fig. FIG.7 Sketch for Upper Suspension After completing sketcher go to workbench and select exit work bench. Then we enter into part module again. In part module, go to sketcher based feature and select shaft tool. In shaft definition, select above sketch as selection profile and specify angle as shown in fig FIG.8 Shaft Definition
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 894 In part design module then go to sketcher tool and select sketcher tool and select required plane or surface. Then we enter into sketcher module and go to profile and create a profile structure as shown in fig FIG.8 Sketch for Lock After completing sketcher go to workbench and select exit work bench. Then we enter into part module again. In part module, go to sketcher based feature and select pad tool. In pad definition, select above sketch as selection profile and specify length as shown in fig FIG.9 Pad for Lock In part design from dress up features select edge fillet at the edge with given dimension as shown below. Part 3: Spring To create go to SOLID WORKS software and click on start –mechanical design and select wireframes and surface design module. In wireframes and surface design module then go to sketcher tool bar and select sketch and select yz plane. Then we enter into sketcher module, then go profile tool and select line tool and specify as shown in fig then click on exit workbench FIG.10 Varying Length for Different Pitch In wireframes and surface design module then go to wireframe tool bar and select helix tool. In helix definition select above point as a starting point and z axis a reference axis. Then specify pitch and height as shown in fig. FIG.11 Helix Definition FIG.12 Creating Spring Inside Definition
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 895 In wireframes and surface design module then go to wireframe tool bar and select helix tool. In helix definition select above point as a starting point and z axis a reference axis. Then specify pitch and height as shown in fig. FIG.13 Creating Fillets In wireframes and surface design module then go to operation and select join. In join definition select all three helix as show in fig. then ok to make one single helix. FIG.14 Rib Definition Now select front plane and go to sketcher in sketcher from profile tool bar select rectangle and draw a rectangle on bottom side as shown below. Exit from workbench in part design from sketch based features select pocket .In pocket definition specify as per given diagram and select reverse side then click ok FIG.15 Remove or Making Flat Support for Spring Part 4: Watcher Go to SOLID WORKS software and click on start – mechanical design and select part design module. In part design module then go to sketcher tool and select sketcher tool and select required plane. Then we enter into sketcher module and go to profile and create a profile structure as shown in fig. FIG.16 Sketch for Watcher After completing sketcher go to workbench and select exit work bench. Then we enter into part module again. In part module, go to sketcher based feature and select shaft tool. In shaft definition, select above sketch as selection profile and specify angle as shown in fig FIG.17 Pad Definition
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 896 3. Assembly of model component FIG.18 ASSEMBLE PART PROCESS OF ANALSING IN ANSYS Static Structural Analysis with Different Materials FIG.19 Project and its Parts After importing the model into project schematic window drag and drop the Static structural analysis tab on to the screen from the toolbox window and link the geometry to geometry both will be linked together. Double click on the model it opens the mechanical window with object. IMPORTED PART FIG.20Imported Geometry FIG.21 Contact Region 4. STRACTURAL ANALYSIS STEEL MATERIAl Total deformation & equivalent stress by applying of 50KG load
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 897 Fig.22 Total deformation & equivalent stress Total deformation & equivalent stress by applying of 125KG load Fig.23 Total deformation & equivalent stress Total deformation & equivalent stress by applying of 200KG load Fig.24 Total deformation & equivalent stress MAGNESIUM MATERIAL Total deformation & equivalent stress by applying of 50KG load
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 898 Fig.25 Total deformation & equivalent stress Total deformation & equivalent stress by applying of 125KG load Fig.26 Total deformation & equivalent stress Total deformation & equivalent stress by applying of 200KG load Fig.27 Total deformation & equivalent stress TITANIUM MATERIAL Total deformation & equivalent stress by applying of 50KG load
  • 8. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 899 Fig.28 Total deformation & equivalent stress Total Deformation & Equivalent Stress By Applying Of 125KG Load Fig.29 Total deformation & equivalent stress Total deformation & equivalent stress by applying of 200KG load Fig.30 Total deformation & equivalent stress 5. MODEL ANALYSIS Total Deformation and Frequency Range in Steel Material Fig .31 Total Deformation and Frequency Range in Steel Material
  • 9. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 900 Total Deformation and Frequency Range in Magnesium Fig.32 Total Deformation and Frequency Range in Magnesium Total Deformation and Frequency Range in Titanium Fig.33 Total Deformation And Frequency Range In Titanium STEEL MATERIAL DATA TABLE 18 Structural Steel > Constants Density 7850 kg m^-3 Coefficient of Thermal Expansion 1.2e-005 C^-1 Specific Heat 434 J kg^-1 C^-1 Thermal Conductivity 60.5 W m^-1 C^-1 Resistivity 1.7e-007 ohm m MAGNESIUM DATA Magnesium Alloy > Constants Density 1800 kg m^-3 Coefficient of Thermal Expansion 2.6e-005 C^-1 Specific Heat 1024 J kg^-1 C^-1 Thermal Conductivity 156 W m^-1 C^-1 Resistivity 7.7e-007 ohm m TITANIUM DATA Titanium Alloy > Constants Density 4620 kg m^-3 Coefficient of Thermal Expansion 9.4e-006 C^-1 Specific Heat 522 J kg^-1 C^-1 Thermal Conductivity 21.9 W m^-1 C^-1 Resistivity 1.7e-006 ohm m TABLE 1 Results and Comparison TOTAL DEFORMATION& EQUIVALENT STRESS TOTAL DEFORMATION& EQUIVALENT STRESS Graph S NO MATERIAL LOADS Total Deformation MmEquivalent Stress 50 1.31E-06 4.47E+06 50+75 3.27E-06 1.11E+07 50+75+75 5.24E-06 1.80E+07 50 5.80E-06 4.42E+06 50+75 1.45E-05 1.11E+07 50+75+75 2.32E-05 1.77E+07 50 2.72E-06 4.40E+06 50+75 6.80E-06 1.10E+07 50+75+75 1.09E-05 1.76E+073 TITANIUM 1 STEEL 2 MAGNESIUM 0.00E+00 5.00E+06 1.00E+07 1.50E+07 2.00E+07 Total Deformation Mm Equivalent Stress
  • 10. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 04 | Apr-2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 901 FREQUENCY VARIATION IN STEEL MATERIAL FREQUENCY VARIATION IN MAGNESIUM MATERIAL FREQUENCY VARIATION IN TITANIUM MATERIAL CONCLUSION In our project we have designed a shock absorber used in a 150cc bike .We modeled shock absorber By using SOLID WORKS. To validate the strength of our design, we have done structural analysis and modal analysis on the shock absorber. We have done analysis by varying spring material is Steel, magnesium and titanium. By observing the analysis results, the analyzed stress values are less than their respective yield stress values. So our design is safe. .By comparing the results for both materials, the stress value is less for titanium than steel and magnesium. Also the shock absorber design is modified by changes the diameter 2mm and loads 50kg, 125kg and 200kg and structural, modal analysis is done on the shock absorber. By comparing the results for both materials, the stress value is less for titanium than steel and magnesium. By comparing the results for present design and modified design, the stress and displacement values are less for modified design. REFERENCES 1. Reza N. Jazar (2008). Vehicle Dynamics: Theory and Applications. Spring. p. 455. Retrieved 2012- 06-24. 2. "Suspension Basics 1 - Why We Need It". Initial Dave. Retrieved 2015-01-29. 3. Adams, William Bridges (1837). English Pleasure Carriages. London: Charles Knight & Co. 4. "Suspension Basics 3 - Leaf Springs". Initial Dave. Retrieved 2015-01-29. 5. "wagon and carriage". 6. "The Washington Times, Sunday 30 June 1901". Chroniclingamerica.loc.gov. Retrieved2012-08-16. 7. Jain, K.K.; Asthana, R.B. Automobile Engineering. London: Tata McGraw-Hill. pp. 293– 294. ISBN 0- 07-044529-X. 12. Pages 617-620 (particularly page 619) of "Race Car Vehicle Dynamics" by William and Douglas Milliken 8. R.S. Khurmi & J.K Gupta (2003), “A textbook of machine design”, S. Chand & company.