IRJET- Static and Dynamic Analysis of a Two Wheeler Shock Absorber using Different Materials for Helical Coil Spring

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 03 | Mar 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 2233
Static and Dynamic Analysis of a Two Wheeler Shock Absorber Using
Different Materials for Helical Coil Spring
Mr. Ram Sagar Alla1, Dr. M. Vidya Sagar2
1M.Tech Student, Department of Mechanical Engineering, J.N.T.U. College of Engineering, JNTU, Hyderabad, India
2 Professor, Department of Mechanical Engineering, J.N.T.U. College of Engineering, JNTU, Hyderabad, India
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Abstract – The Shock Absorber is a part of the suspension
system in a vehicle which is designed mechanically to handle
shock impulse and dissipate kinetic 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 amplitudeofdisturbances. Thedesignof
spring in suspension system is very important. In this projecta
shock absorber of a popular model of a two wheeler isselected
and a 3D model is created using SolidWorks2014. Structural
analysis and modal analysis are doneontheshockabsorber by
varying material for spring viz., two variants in Steel, two
variants in Copper Alloys and one Titanium Alloy. Theanalysis
is done by considering the kerb weight of the bike and a
combined weight of two riders. Under Static Analyses, Linear
Static analysis is done to validate the Stresses, Displacements
and Modal analysis is done to determine the different
frequencies for number of modes. And under Dynamic
Analyses, Frequency Response Analysis is done to determine
the displacement due to cyclic loading and Transient Analysis
(Shock Analysis) is done to study the performanceoftheShock
Absorber during shock loading. Comparison is done for five
materials to verify best material for spring in Shock absorber.
Also, the spring diameter has been varied based on the results
to check for scope of improved performance. 3D Modelling is
done in SolidWorks 2014, Meshing is done in HyperMesh,
OPTISTRUT for solving and Hyperview and Hypergraph for
post processing and viewing the results.
Key Words: Linear Static Analysis, Modal Analysis,
Frequency Response (Harmonic) Analysis, Transient
(Shock) Analysis, Shock Absorber, HyperWorks,
SolidWorks, Helical Coil Spring, Optistruct, Redesign,
Morphing, ASTM.
Nomenclature
G : Modulas of Rigidity
Dm : Mean Diameter of the coil
d : Diameter of the Spring Wire
Do : Max. Outer Diameter of the Spring
nt : Total Number of coils
n : Number of Active coils
C : Spring Index
Lf : Free length of the spring
Ls : Solid Length of the spring
p : Pitch of the coils
k : Whal’s Stress Factor
δ : Deflection of spring under load
τ : Max. Shear Stress in the spring
K : Spring Stiffness
ωn : Natural Frequency
ω : Frequency
t : Time Period
1. INTRODUCTION
Shock absorbers are a critical part of a suspension system,
connecting the vehicle to its wheels. The need for dampers
arises because of the roll and pitches associatedwithvehicle
maneuvering, and from the roughness of roads. Shock
absorbers are devices that smooth out an impulse
experienced by a vehicle, and appropriately dissipate or
absorb the kinetic energy.
A safe vehicle must be able to stop and maneuver over a
wide range of road conditions. Good contact between the
tires and the road will able to stop and maneuver quickly.
Suspension is the term given to the system of springs, shock
absorbers and linkages that connects a vehicle to its wheels.
Shock absorber is an important part of automotive
suspension system which has an effect on ride
characteristics. Shock absorbers are also critical for tire to
road contact which to reduce the tendency of a tire to lift off
the road. This affects braking,steering,corneringandoverall
stability.
In this project a shock absorber of Avenger 150CC vehicle
will be selected and will be designed. A 3D model will be
created by using SolidWorks. Structural analysis and modal
analysis are done on the shock absorber by varying material
for spring. Further to this, Frequency Response (Harmonic
Analysis) and Transient Response (Shock Analysis) will be
performed. The analysis will consider the kerb weight of the
bike and load of two riders. Structural analysis will be done
to validate the strength and modal analysis to determine
different frequencies for number of modes. Frequency
Response will be done to find out the displacements
occurring in the frequency range. Transient analysis will be
conducted to simulate the shock loads occurring on the

shock absorber and to find the displacements occurring
during shock and the time requiredfortheshock absorberto
damp the displacements. Comparison will be done among
five materials to verify best material for spring in Shock
absorber. Also, the wire diameter of the springwill bevaried
to check for scope of improvement in the performance
characteristics of the shock absorber.
1.1 Literature Survey
In an approach involvingtheshockabsorberof150CCbikeby
P. Poornamohan[1] (2012), it was designed using parametric
software Pro/Engineer. Structural and Modal were
performed to validate the strength of the design. Materials
used were Spring Steel and Beryllium Copper. It was
observed that the Stress values were less for spring Steel
compared to Beryllium Copper and hence the wire diameter
was reduced by 2mm. It was observed that the stress and
displacement values were less for the modified design which
also reduced the weight of the spring.
In another approach by Karthik A. S. [2] (2016), a different
model of a shock absorber evaluated for Structural analysis
for different materials of spring viz., Structural Steel, Copper
alloy, Aluminum alloy, Titanium alloy. It was observed that
though the overall performance of titaniumalloywasgood,it
is a very costly material to be put into general use.
In a project by Mr. A.C.Basha[3] (2017),aShockAbsorberwas
selected and analyzed by changing the materials for the
springs by Structural analysis alone and the results were
presented.
1.2 Formulation of Problem based on surveys and
reviews
Based on Literature reviews, the problem in the present
investigation is formulated as follows: “To design a model of
an existing two wheeler shock absorber and perform Static,
Modal, Frequency Response and Transient analysis to
ascertain its Structural and Vibrational performance under
various loading conditions for different materials for the
spring. To optimize the design by varyingthediameterofthe
spring wire and suggesting best suited material forspring to
achieve better performance characteristics”.
Materials proposed to be used for study will not be generic
materials but will be selected from ASTM standards.
Different materials proposed to be used are:
 Stainless Steel Spring Wire as per ASTM A 313 (DIN
17221) – AISI 302/304.
 Cold drawn, high tensile Carbon galvanized Steel as per
ASTM A 228.
 Phosphor Bronze Grade A Spring Wire as per ASTM B
159.
 Beryllium Copper Spring Wire as per ASTM B 197.
 Titanium Alloy as per Grade Ti-5Al-5V-5Mo-3Cr.
In addition to Structural and Modal analyses, it is proposed
to conduct Frequency Response and TransientAnalysesalso
because Modal analysis will give the natural frequencies and
corresponding mode shapes only. But to analyze the model
completely, the displacements and accelerations related to
the corresponding natural frequencies must be evaluated.
These results are obtained by performing a Frequency
Response analysis for a band of frequencies specified.
Graphs betweenFrequency Vs.Displacementswill be plotted
for different materials and studied for their suitability.
A true performance of a Shock Absorber can be analyzed
under shock loading. This involves a high impulse load
applied in a very small time interval. The damping
characteristics of shock absorber will beanalyzedwhich will
have a direct impact on the ride quality of the two wheeler.
2. Design of Helical Coil Spring based Shock
Absorber
SolidWorks is a parametric, feature based, solid modeling,
menu driven higher end software. It provides mechanical
engineers with an approach to mechanical design with
automation based on Built-in intelligence takes the guess
work out of 3D design.
2.1 Modeling of Bottom Mount
Draw a circle of 52mm diameter and extrude it by a value
of 3.5mm.
On its face, draw a circle of 35mm diameter and extrudeitby
a value of 36.5mm.
Now, A model of bearing pad is created by drawing two
concentric circles of 30mm and 12mm respectively and
extruding it to a length of 110mm over the top face.
Mounting eye is modeledsimilarlyforthedimensionsshown
below
This completes the model of the bottom mount and the final
model is as shown below:
Fig-2.1: Bottom Mount
2.2 Modeling of Top Mount
Draw a circle of 62mm diameter and extrude it by a value
of 40.5mm.

Shell Feature is used to create a hollow cup of 2mm wall
thickness. Mounting eye is modeled similarly for the
dimensions shown below
Fig-2.2: Top Mount
2.3 Modeling of Helical Coil Spring
The spring is measured to have a constant pitch and a
variable diameters at its ends. The spring has a total of 12
full turns and two half turns which are flattened out to be
fixed on to the Top and Bottom Mounts respectively. A helix
is constructed with a constant pitch, height of 200mm and
the diameters at the ends are 48mm and 44.5mm
respectively. The spring wire diameter is measured to be
8mm. A circle of 8mm diameter is swept around the helix to
create the basic spring. The ends of the spring are trimmed
to become flat to be fixed on to the Top and Bottom Mounts
respectively.
Fig-2.3: Helical Coil Spring
2.4 Assembly of Shock Absorber
Piston Rod for the Dampner is modeled similarly and the
shock absorber is assembled in the Assembly module of
SolidWorks as shown in the figure below:
Fig-2.4: Exploded and Assembled views
3. Design Calculations OF Helical Coil Spring of
Shock Absorber
3.1 Experimental determination of weight
distribution
The weight of the two wheeler will be distributed among the
front and rear wheels through the shock absorbers. To
accurately determine the weight taken by the rear shock
absorbers, the weight under the front and rear wheels is
measured. Kerb Weight of the two wheeler from the
specification catalogue is 148 kgs.
Fig-3.1: Determination of weight shared by front and
rear Wheels
A weighing scale is placed under the rear & front wheels of
the two wheeler and the reading is taken as 85.1kgs & 62.5
kgs respectively. Considering two persons are riding on the
two wheeler having a weight of 65kgs each totaling to 130
kgs. Now thisload has to be divided inthesameproportionof
the load distribution among the front and the rear
suspensions.
Load on rear suspension = 74.95 kgs.
Load on front suspension = 55.04 kgs.
Therefore the total load on the rear suspension= Load due to
self weight of the two wheeler + load of two persons shared
by the rear suspension
Total load on rear suspension = 85.1 + 74.95 = 160.05 kgs.

This load is shared by two shock absorbers. Therefore the
load on each shock absorber will be half of this value = 80.02
kgs. = 784.8 N
3.2 Design calculations for Helical Coil Spring
The material for the spring is taken as Stainless Steel Spring
Wire as per ASTM A 313.
Modulus of Rigidity (G) = 69000 N/mm2
Mean Diameter of the coil (Dm) = = 46.25mm
Diameter of the Spring Wire (d) = 8mm
Max. Outer Diameter of the Spring (Do) = 56mm
Total Number of coils (nt) = 14
Number of Active coils (n) = 12
Spring Index (C) = = = 5.7
Free length of the spring (Lf) = 200mm
Solid Length of the spring (Ls) = d nt = 8 x 14 = 112mm.
Pitch of the coils (p) =
Whal’s Stress Factor (k)
Deflection of spring under load (δ)
Max. Shear Stress in the spring (τ)
Spring Stiffness (K)
3.3 Experimentaldeterminationofthedeflectionof
spring under static load
The deflection of the spring under the self weight of two
wheeler and with twopersonswithacombinedweightof130
kgs sitting on the two wheeler is determined. In all the cases
the length is measured from centre to centre of the fixing
bolts of the Shock Absorber.
Fig-3.2: Determination of deflection under load
Free length of the Shock Absorber – Vehicle is parked on its
centre stand and the rear wheel is lifted off the ground =
285mm
Vehicle is taken off the centre stand, and it is resting on its
two wheels – Centre distance of the bolts of the Shock
Absorber due to self weight of the bike = 278mm.
Deflection of the Shock Absorber = 285-278 = 7mm
Two persons are made to sit on the bike of 65kgs weight
each. Centre distance of the bolts of the Shock Absorber =
251mm;
Deflection of the Shock Absorber = 278-251 = 27mm.
4. Linear Static Analysis
When loads are applied to a body, the body deforms and the
effect of loads is transmitted throughout the body. The
external loads induce internal forces and reactions to render
the body into a state of equilibrium. Linear Static analysis
calculates displacements, strains, stresses, and reaction
forces under the effect of applied loads.
4.1 Meshing the CAD Model in Hypermesh
The complete assembly as a .STEP file is imported into
Hypermeshand thedifferentpartsoftheShockAbsorberthat
were generated in SolidWorks are arranged into different
component collectors.
Taking Spring as an example, once the flat surface of the end
of the spring is trimmed with plane, goto 2D page 
Automesh  Mesh. Select the surface  Element Size=2 
Mesh Typeis quads  Mesh. Once the surface is meshed, use
3D page  Line Drag  Meshto createa Solid Hexa Mesh for
the spring.
Fig-4.1: Hex Mesh for Spring

Fig-4.2: Tetra Mesh for Bottom & Top Mounts
Once the meshing of all the components iscompleted,quality
of the mesh is to be checked. Goto Tool page  Check elems
 3d. Warpage, Aspect, Skew etc have to be checked for
failed elements. Failed elements have to be adjusted using
Geom Page  Node Edit  associate or move node options.
All the nodes in the assembly should have connectivity to
avoid failures during analysis runs.
Fig-4.3: Final Mesh Model of Shock Absorber
4.2 Applying Material Properties
As it is proposed to carry out the analyses for five different
materials, Material cards for the different materials to be
applied to the components have to be created first with the
following material properties:
Table 4.1: Material Properties
Material Properties
Material
Specification
Young’s
Modulas
(GPa)
Poisson’s
Ratio
Density
(g/cc)
Stainless Steel
Spring Wire as per
ASTM A 313
193 0.3 7.92
Cold drawn, high
tensile Carbon
galvanized Steel
as per ASTM A 228
207 0.31 7.85
Phosphor Bronze
Grade A Spring
103 0.341 8.86
Wire as per ASTM
B 159
Beryllium Copper
Spring Wire as per
ASTM B 197
128 0.3 8.26
Titanium Alloy as
per Grade Ti-5Al-
5V-5Mo-3Cr
112 0.3 4.65
4.3 Applying Boundary Conditions & Loads
By the physical assembly of the Shock Absorber to a two
wheeler, it can be noted that the top eye is a fixed contactand
the bottom eye fixes to the axle of the rear wheel which is
where the loads are exerted. The Strut rod is in sliding
contact with the bottom mount and the spring isconstrained
within the top and bottom mounts.
Creating Contact Surfaces is of paramount importance in the
modeling of a Shock Absorber as the dampner is simulated
for analysis by giving dampning percentage to the contact
surfaces of the strut rod and the dashpot of the Bottom
Mount.
A Load of 784.8N has to be applied on the nodes of the fixing
eye of the bottom mount. For this, the load has to be divided
among the nodes of the eye. The number of nodes should be
determined and the load hasto be divided equally amongthe
nodes and appliedat the bottom mountfixingeye.LoadSteps
for Linear Static Analysis have to be created.
4.4 Solving the setup using OPTISTRUCT solver
Altair® OptiStruct® is an industry proven, modern structural
analysis solver forlinear and non-linear structural problems
under static and dynamic loadings. It is the market-leading
solution for structural design and optimization. Based on
finite-element and multi-body dynamics technology and
through advanced analysis and optimization algorithms,
OptiStruct helps designers and engineers rapidly develop
innovative, lightweight and structurally efficient designs.
The analyses will be run for all the five materials and
respective .h3d files which are the output files will be
generated.
4.5 Viewing Results on Hyperview
Case-1: Stainless Steel Spring Wire as per ASTM A 313
Open Hyperview window and browse to the location of the
.h3d file of the Case-1 Analysis folder. Apply. The results will
be loaded in to the model window.
Select Contour  Result Type: Displacement, Magnitude 
Selection: Components: All  Apply. Result Type: Element
Stresses, von Mises  Selection: Components: All  Apply
Meshing of the Shock
Absorber assemblyis
completed and now
the further steps of
preprocessing can be
proceeded with.

Fig-4.4: Max. Displacement (27.85mm); Stress (605.6MPa)
Case-2: Cold drawn, high tensile Carbon galvanized Steel as
per ASTM A 228
Fig-4.5: Max. Displacement (26.17mm); Stress (597MPa)
Case-3: Phosphor Bronze GradeASpring WireasperASTMB
159
Case-4: Beryllium Copper Spring Wire as per ASTM B 197
Case-5: Titanium Alloy as per Grade Ti-5Al-5V-5Mo-3Cr
From the results of Linear Static Analyses it is evident that
the displacementandstressvaluesobtainedforCopperAlloy
based springs and Titanium alloy springs is on the higher
side. Similar is the case with the maximum stress valuesthat
are obtained.
Spring Steel based springs are showing better results in
Linear Static Analysis.
5. Normal Mode / Modal Analysis
If an elastic structure is disturbed from its stationery
position by applying a force to have an initial displacement
and then the force is removed, the structure will oscillate
about its equilibrium position. This type of oscillation bythe
initial disturbance only is called free vibration. The
oscillatory motion occurringatcertainfrequencies knownas
natural frequencies and characteristic values follow well
defined deformation patterns known as mode shapes.When
a structure vibrates with a given natural frequency (ω), that
unique shape with arbitrary amplitudecorrespondingto (ω)
is called a mode. In general for a ‘n’ DoF system, there will be
‘n’ natural frequencies and modes. The study of such free
vibrations is very important in findingthedynamicresponse
of the system. First ten modal frequencies are evaluated for
all the materials:
Table 5.1: Results of Modal Analysis (Freq-Hz)
Mode Case-1 Case-2 Case-3 Case-4 Case-5
Mode 1 25 24.6 16.9 19.3 19.1
Mode 2 77 76.3 50.6 58.7 73.3
Mode 3 77.5 76.7 50.8 59 73.6
Mode 4 107.4 105.8 70.1 81.8 99.1
Mode 5 112.8 111.9 74.4 85.9 107

Mode 6 177.3 175.6 116.5 135.1 168.5
Mode 7 179.1 177.4 117.5 136.4 170.1
Mode 8 202.9 200.1 131.9 154.3 190.8
Mode 9 223.9 222.3 147.7 170.5 212.6
Mode 10 291.7 288.8 190.9 222 276.6
From the results of Modal Analysis it is observed thatCase-3
pertaining to Phosphor Bronze material has the first modal
frequency below the 20Hz range. Low frequencies, typically
less than 20Hz range have a high possibility of getting into
resonance with the engine frequencies which are also low
frequencies.
Case-4 & Case-5 pertainingtoBerylliumcopperandtitanium
alloy are also border line with the low frequency levels.
These are also not in the acceptable performance levels.
Case-1 & Case-2 of Steel based springs havetheirfirstmodes
beyond the low frequency levels. Though their performance
is acceptable, there is scope of improvement by optimizing
the spring parameters.
6. Frequency Response (Harmonic) Analysis
Frequency response analysis is used to calculate the
response of a structure to steady state oscillatory excitation.
Frequency response analysis is used to compute the
response of the structure, which is actually transient, in a
static frequency domain. Theloadingissinusoidal.Theloads
can be forces, displacements, velocity, and acceleration. The
results from a frequency response analysis are
displacements, velocities, accelerations,forces,stresses, and
strains. OPTISTRUCT supports Direct and Modal frequency
response analysis. Results of this analysis for the five
materials selected are as follows:
Fig-6.1: Max. Displacement 59.9mm @ 26Hz
Case-2: Cold drawn, high tensile Carbon galvanized Steel
as per ASTM A 228
Case-3: Phosphor Bronze Grade A Spring Wire as per
ASTM B 159

All the analyses under Frequency Response Analysis are
done by giving a unit load excitation to the bottom eye of the
Shock Absorber and a cyclic load isapplied.Asinusoidal load
is applied in a frequency range of 0Hz to 60Hz.
In the results obtained, it can be observed thatthefrequency
at the first resonance point matches nearest to the results of
first modal frequency obtained in modal analysis. This
proves the accuracy of frequency response analysis and the
corresponding displacements are thus obtained.
From the results above, Copper Alloy based springs and
titanium alloy springs haveveryhighdeflectionsalmostnear
to the complete compression of the spring which is not
acceptable. Spring Steel based springs are showing
considerably better results but there is a scope available for
improvement.
7. Transient Response (Shock) Analysis
Transient response analysis isusedtocalculatetheresponse
of a structure to time-dependent loads. Typical applications
are structures subject to earthquakes, wind, explosions, ora
vehicle going through a pothole.
The loads are time-dependent forces and displacements.
Initial conditions define the initial displacement and initial
velocities in grid points.
The results of a transient response analysis are
displacements, velocities, accelerations,forces,stresses, and
strains. The responses are usually time-dependent.
OPTISTRUCT supports Direct and Modal transient response
analysis.
7.1 Generation of a Time dependant LoadingCurve
A load of 1500N is to be applied as a shock/impulse load for
24 milliseconds. The response of the shock absorber for100
milliseconds will be studied with an damping of 4% applied
to the model. The loading will be a half sine curve calculated
as below:
The loading curve is generated as a Table in MS Excel first
and the same will be imported to Hypermesh as a .csv file
which will be used as an input for loading curve in transient
response analysis.
Table 7.1: Table for loading curve for Shock/Impact
Time
Interval (t)
(ms)
Force
Applied
(Ft) (N)
Time
Interval
(t) (ms)
Force
Applied
(Ft) (N)
0 0 0.013 1487.17
0.001 195.79 0.014 1448.89
0.002 388.23 0.015 1385.82
0.003 574.03 0.016 1299.04
0.004 750 0.017 1190.03
0.005 913.14 0.018 1060.66
0.006 1060.66 0.019 913.14
0.007 1190.03 0.02 750
0.008 1299.04 0.021 574.03
0.009 1385.82 0.022 388.23
0.01 1448.89 0.023 195.79
0.011 1487.17 0.024 0
0.012 1500 0.1 0
Fig-7.1: Loading Curve imported to Hypermesh
With this loading curve as input along with 4% of damping
applied to the model to simulatetheactionofdampnerinthe
Shock Absorber, Transient Analysis is performed for all the
five materials and the results are as per figures below:

Fig-7.2: Max Displacement: 41.5mm
Case-2: Cold drawn, high tensile Carbon galvanized Steel as
per ASTM A 228
Case-3: Phosphor Bronze GradeASpring WireasperASTMB
159
From the results of the Transient Analysis, again the Copper
based and Titanium Alloyspringshaven’tshownsatisfactory
results. The deflection ranges are too high in comparison
with Spring Steel based springs.
8. Redesign of Spring
The re-design of the spring is targeted at increasing the
stiffness of the spring to reduce the deflections in impact
loading cases and to shift the resonant frequencies away
from the lower frequency ranges of 0-20Hz.
This is achieved by changing the wire diameter of the spring
and selecting a different (stiffer) grade of spring steel.
Table 5.1: Results of Modal Analysis (Freq-Hz)
Existing Design
Parameters
Proposed Design
Parameters
Spring Diameter: 8.0mm
Spring Diameter: Next
higher Standard Wire
Diameter of 9.125mm
Material of the Spring:
Stainless Steel Spring Wire
as per ASTM A 313
Material of the Spring:
Cold drawn, high tensile
Carbon galvanized Steel as
per ASTM A 228
8.1 Increasing the Spring Wire DiameterGeometry
using Morphing
HyperMorph is a mesh morphingtool thatallowsyoutoalter
finite element models while keeping mesh distortions to a
minimum.
HyperMorph can be used to Change the profile and the
dimensions of your mesh, Map an existing mesh onto a new
geometry, Create shape variables that can be used for
optimization.

Using this module, the wire diameterofthemeshed model of
the spring is increased to 9.1mm withoutaffectingtherestof
the model or the continuity.
Material propertiespertainingtoASTMA228gradeofSpring
Steel are assigned to the redesigned spring and all the four
analyses are repeated.
8.2 Linear Static Analysis
8.3 Modal Analysis
Table 8.1: Table for loading curve for Shock/Impact
Mode Frequency Mode Frequency
Mode 1 30.1 Hz Mode 6 195.3 Hz
Mode 4 120.2 Hz Mode 9 247.9 Hz
Mode 5 124.9 Hz Mode 10 322 Hz
8.4 Frequency Response Analysis
8.5 Transient Response Analysis
9. Results and Discussions
In this project, the Shock Absorber used in a 150CC bike was
modeled using 3d parametric software – SolidWorks2014.
To validate the strength of the design, Structural Analysis
and Modal Analysis wereperformed.Toevaluateitsdynamic
performance characteristics, Frequency Response Analysis
and Transient analysis (Shock analysis) were performed. All
these different analyses were performed by changing the
material of the Spring Wire. The materials that were used
were:
Stainless Steel Spring Wire asperASTMA313(DIN 17221) –
AISI 302/304.
Cold drawn, high tensile Carbon galvanized Steel as per
ASTM A 228.
Phosphor Bronze Grade A Spring Wire as per ASTM B 159.
Beryllium Copper Spring Wire as per ASTM B 197.
Titanium Alloy as per Grade Ti-5Al-5V-5Mo-3Cr.
All the analyses were done and from the detailed results
presented in previous sections for different material for
different analyses, the maximum values of Displacements,
stresses, modal frequencies, displacements for cyclic and
transient (impact) loading are consolidated and tabulated
and shown in Table 9.1
1. By observing the analysis results of Linear Static
Analysis, the stresses observed are less than their
respective yield stress values. So from Stress point of
view all the materials qualify as suitable materials for
Spring.

Table 9.1: Results of all the Analyses of Existing Design
Material
Linear Static Modal FRA TRA
Disp.
(mm)
Stress
(MPa)
Freq
(Hz)
Freq
(Hz)
@
Disp.
(mm)
Disp.
(mm)
Case 1 27.85 605.6
25,
77,
77.5
26
@
59.9
41.5
Case 2 26.17 597.0
24.6,
76.3,
76.7
24
@
62.2
42.5
Case 3 53.70 636.3
16.9,
50.6,
50.8
16
@
124.1
92.1
Case 4 41.94 647.1
19.3,
58.7
59
20
@
99.1
52.4
Case 5 47.90 657.4
19.1,
73.3,
73.6
20
@
112.8
82.5
2. The results of displacements from Linear Static Analysis,
the existing design of the spring with the above referred
material grades is within 50% of the total allowable
compression of the spring. Thus the base design with its
properties is validated from maximum displacement
point of view.
3. The static deflections of Phosphor Bronze, Beryllium
Copper, Titanium alloy are all in high ranges. If these
materials are employed as springs,therewill beveryplay
left in the spring to deflect during shock/impact loads.
4. By comparing the results of Normal Mode analysis, the
natural frequencies of Phosphor Bronze, Beryllium
Copper, Titanium alloy based Springs are below low
frequency ranges of 0-20Hz. This can lead to resonance
conditions with the engine operating frequencies.
5. Frequency Response Analysis gives the Resonant
Frequency and the associated Displacement at that
frequency. From the two grades of Spring Steel of ASTM
A313 and ASTM A228,thoughthenatural frequenciesare
above the 20Hz range, the associated displacements of
59.9mm and 62.2mm are quite high. These values are
quite near to the maximumallowabledisplacementofthe
Shock Absorber of 70mm.
6. The actual performance of a Shock Absorber can be
evaluated from Transient Response analysis as most of
the loads that occur during the movement of the two
wheeler are Shock/impact loads only.Fromtheresults,it
is evident that the displacement values of Spring Steel
ASTM A313, Spring Steel ASTM A228 and Beryllium
Copper are nearest to acceptable range. Beryllium
Copper based spring takes beyond 70ms to damp the
vibrations whereas both the grades of Spring Steel damp
the vibrations within 50ms.
7. These results clearly show that Copper based Alloys and
Titanium alloys though have a lighter weight advantage,
they do not possess the required properties to achieve
acceptable performance characteristics. Commercial
viability of using titanium alloy based springs for
automobiles is also questionable.
8. From the results it is also evident that Spring Steel based
springs are most suitable, yet there is a scope for
improvement in the design of the springtomakeitstiffer.
This will result is lower displacements in static and
dynamic conditions as well as the resonant frequencies
will be shifted away from low engine frequency values.
9.1 Comparison of Existing Design Vs. Redesigned
Spring
With the modified properties all the four analyses viz.,
Structural, Modal, Frequency Response and Transient
Analyses are repeated. The results of the existing designand
the modified design are compared and tabulated as below.
Table 9.2: Comparison of results of Existing Design Vs.
Redesigned Spring
Parameter
Existing
Design
Modified
Design
Remarks
Linear Static
Analysis
Disp. (mm)
27.85 mm 16.56 mm
40% reduction
in the Static
Displacement
Static
Analysis
Max. Stress
(MPa)
605.6
MPa
374.3 MPa
38% reduction
in the Max.
Stress
Normal
Modes
(Hz)
25,
77,
77.5,
107.4,
112.8
30.1,
84.7,
85.5,
120.2,
124.9
No low
frequency
ranges nearest
to 20Hz
Frequency
Response
59.9mm
@ 26Hz
39.5mm @
30Hz
34% decrease in
the max.
displacement.
Resonant
Frequency has
moved to 30Hz
Transient
Response
Disp. (mm)
41.5 mm 29.7 mm
28% reduction
in max.
displacement
during impact
loads.
From the results, it can be noted that there is a considerable
reduction in the Static deflection and the max stress values
of the modified design by 40% and 38% respectively. The
low frequencies observed in the existing design have shifted
to 30Hz and above eliminating the low frequency bands
which usually tend to resonate with the engine frequencies.

The maximum displacement observed in cyclic loading at
30Hz also has reduced by 34%. Impact loading also has
shown an improvement by a 28% reduction in maximum
displacement values. In all the parameters considered, the
modified design is showing better results. On the down side,
there will be a marginal increase in the kerb weight of the
vehicle as the weight of the spring is going to increase.
11. Conclusions
In this project, a Shock Absorber of an existing model of a
150 cc Two-wheeler has been designed using Solid Works-
2014. To validate the strength of the existing design, Linear
Static and Modal Analysis were performed. To validate the
dynamic performance of the Shock Absorber, Harmonic
(Frequency Response) Analysis and Transient Response
Analysis were performed using HyperWorks packages. The
material of the Helical Spring was varied for five different
materials and the Analyses were performed. From the
results, the following conclusions are made
1. It is observed that, Copper based alloys and Titanium
alloy based materials for springs are not suitable for
Two Wheeler Shock Absorber applications as their
spring stiffness is too less for automobile applications.
2. Keeping all the other parameters constant, the wire
diameter of the spring is increased to the nextstandard
value and the better performing material of ASTM A
228 is selected for the modified spring.
3. The Static deflection has reduced, which in-turn gives
more displacement to be available for the spring to
deflect during Shock/Impact loads.
4. The resonant frequencies aremovedto30Hz.Thereare
no frequencies below the low frequency ranges of 0-
20Hz.
5. The reduced deflection in Transient Analysis indicate
that the modified Spring is stiff compared to the
existing design. This will cater to higher payload on the
two wheeler and gives sufficient room for deflection of
the Shock Absorber when going over bad roads.
6. As per the above study conducted, wire diameter of
spring with 9.125mm and material for spring as per
ASTM A 228 is found to be a better choice for thespring
of the shock absorber as when comparedtotheexisting
model.
REFERENCES
[1] Pinjarla Poornamohan, Lakshmana Kishore .T
“DESIGN AND ANALYSIS OF A SHOCK ABSORBER”,
IJRET - International Journal of Research in
Engineering and Technology, Dec-2012, Volume: 1,
Issue: 4, pp 578 – 592.
[2] Karthik A. S., “DESIGN AND STATIC ANALYSIS OF
SHOCK ABSORBER”, IJIRST –International Journal for
Innovative Research inScience&Technology,Volume
2, Issue 12, May 2016.
[3] Mr. a. Chinnamahammad Basha, Mr. Vijay Rami
Reddy, “DESIGN AND ANALYSIS OF SHOCK
ABSORBER” IRJET - International ResearchJournal of
Engineering and Technology, Jan-2017, Volume: 4,
Issue: 1, pp 201 – 207.
[4] R. S. Khurmi and J. K. Gupta, “Machine Design”, S.
Chand Publications.
[5] S. Md. Jalaludeen, “Finite Elememnt Analysis in
Enigneering”, Anuradha Publications.
[6] P. Kannaiah, “Machine Design”, Scitech Publications
India Pvt. Ltd.
[7] J.B.K. Das, Dr. P.L. Srinivasa Murthy, “Mechanical
Vibrations”, Sapna Book House Publications.
[8] http://en.wikipedia.org/wiki/Shock_absorber
[9] http://en.wikipedia.org/wiki/Suspension_(motorcycl
e)
[10] http://www.optimumspring.com/technical_resources
/materials

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