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ISSN: 2231-5381 http://www.ijettjournal.org Page 173
Structural and Modal Analysis of Shock Absorber of
Vehicle
1
, Chinmay Patil2
1
M.E Advanced Manufacturing and Mechanical System Design, Department of Mechanical Engineering, Shri Sant Gajanan
Maharaj College Of Engineering, Shegaon,Maharashtra,India
2
Assistant Professor, Department of Mechanical Engineering, Shri Sant Gajanan Maharaj College Of Engineering,
Shegaon,Maharashtra,India
Abstract
Safety and driving comfort for a car’s driver are both
dependent on the vehicle’s suspension system. Safety refers to the
vehicle’s handling and braking capabilities. The comfort of the
occupants of a car correlates to tiredness and ability to travel
long distance with minimal annoyance. Shock absorbers are a
critical part of a suspension system, connecting the vehicle to its
wheels.
Essentially shock absorbers are devices that smooth out
an impulse experienced by a vehicle, and appropriately dissipate
or absorb the kinetic energy. Almost all suspe nsion systems
consist of springs and dampers, which tend to limit the
performance of a system due to their physical constraints.
Suspension systems, comprising of springs and dampers, are
usually designed for passengers’ safety, and do little to improve
passenger comfort. To meet the current demands of high speed
and safety we must designed and developed such a shock
absorber which can sustain more and more vibrations and also
improves the safety.
Keywords: Springs, dampers, shock absorber
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 associated with vehicle
manoeuvring, 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. When a vehicle is travelling on a level road and the
wheels strike a bump, the spring is compressed quickly. The
compressed spring will attempt to return to its normal loaded
length and, in so doing, will rebound past its normal height,
causing the body to be lifted. The weight of the vehicle will
then push the spring down below its normal loaded height.
This, in turn, causes the spring to rebound ag ain. This
bouncing process is repeated over and over, a little less each
time, until the up -and-down movement finally stops. If
bouncing is allowed to go uncontrolled, it will not only cause
an uncomfortable ride but will make handling of the vehicle
very difficult.
A safe vehicle must be able to stop and manoeuvre over a
wide range of road conditions. Good contact between the tires
and the road will able to stop and manoeuvre 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, cornering and overall stability. The removal
of the shock absorber from suspension can cause the vehicle
bounce up and down. It is possible for the vehicle to be driven,
but if the suspension drops from the driving over a severe
bump, the rear spring can fall out The design of spring in
suspension system is very important.
In this project a shock absorber will be designed and
a 3D model which will be created is by using Pro/Engineer.
The model is also changed by changing the thickness of the
spring. Structural analysis and modal analysis are done on the
shock absorber by varying material for spring.. The analysis
will consider the loads, bike weight, single person and 2
persons. Structural analysis will be done to validate the
strength and modal analysis to determine the displacements
for different frequencies for number of modes. Comparison
will be done for two materials to verify best material for
spring in Shock absorber.
CADmantra Technolgies Pvt. Ltd 12/5
Bhola Patel
Design Engineer @ CADmantra Technolgies Pvt. Ltd
Mail : bholapatel.me@gmail.com,
Share on: facebookbolapatel
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 174
Figure 1.1 Shock absorbers with different dimensions
2 DESIGN OF HELICAL COMPRESSION SPRING
FOR SHOCK ABSORBER
Material: ASTM A228 (modulus of rigidity) G = 184.48 *103
N/mm2
Mean diameter of a coil D=60 mm
Diameter of wire d = 10 mm
Total no of coils n‟= 7
Outer diameter of spring coil D0 = D +d =70mm
Inner diameter of spring coil Di = D +d =70 mm
No of active turns n= 5
Weight of bike = 150 Kgs
Let weight of 1 person = 75 Kgs
Total Weight (Wt) = Weight of bike + Weight of 1 persons
= 150+75 = 225Kgs
Rear suspension = 65%
65% of 225 = 146 Kgs
Considering dynamic loads it will be double
Wt = 292 Kgs = 2864 N
For single shock absorber weight (W) =Wt/2=2864 /2 =1432
N
We Know that, compression of spring (δ) = × × /×
C = spring index = = = 6 = 8 (δ) = × × × /× = 6.7
Solid length, Ls=n‟×d=7*10=70
Free length of spring,
Lf = solid length+maximum compression + clearance between
adjustable coils = 70+6.7+6.7*0.15 = 77.7
Spring rate, K = W/(δ) =1432/6.7 =213.73 Pitch of coil, P =
13
Stresses in helical springs: maximum shear stress induced in
the wire τ = K× K = + . = × × + . = 0.97 τ = K× = 0.97 × × × ×
= 274 N/mm2
3 CAD MODELLING
CAD/ CAE Software‟s used:
PRO/E wildfire 4.0 - For 3D Component Design.
Pro/Assembly - For Assembling Components
ANSYS Workbench 11.0 - For FEM analysis
3.1 Introduction to PRO-E
Pro/ENGINEER is a parametric, feature based, solid
modeling System. It is the only menu driven higher end
software. Pro/ENGINEER provides mechanical engineers
with an approach to mechanical design automation based on
solid modeling technology and the following features.
3-D Modeling
The essential difference between Pro/ENGINEER
and traditional CAD systems is that models created in
Pro/ENGINEER exist as three-dimensional solids. Other 3-D
modelers represent only the surface boundaries of the model.
Pro/ENGINEER models the complete solid. This not only
facilitates the creation of realistic geometry, but also allows
for accurate model calculations, such as those for mass
properties.
Parametric Design
Dimensions such as angle, distance, and diameter
control Pro/ENGINEER model geometry. You can create
relationships that allow parameters to be automatically
calculated based on the value of other parameters. When you
modify the dimensions, the entire model geometry can update
according to the relations you created.
Feature-Based Modeling
You create models in Pro/ENGINEER by building
features. These features have intelligence, in that they contain
knowledge of their environment and adapt predictably to
change. Each features asks the user for specific information
based on the feature type. For example, a hole has a diameter,
depth, and placement, while a round has a radius and edges to
round.
Associativity
Pro/ENGINEER is a fully associative system. This
means that a change in the de sign model anytime in the
development process is propagated throughout the design,
automatically updating all engineering deliverables, including
assemblies, drawings, and manufacturing data. Associativity
makes concurrent engineering possible by encouragi ng
change, without penalty, at any point in the development
cycle. This enables downstream functions to contribute their
knowledge and expertise early in the development cycle.
Capturing Design Intent
The strength of parametric modelling is in its ability
to satisfy critical design parameters throughout the evolution
of a solid model. The concept of capturing design intent is
based on incorporating engineering knowledge into a model.
This intent is achieved by establishing feature and part
relationships and by the feature-dimensioning scheme. An
example of design intent is the proportional relationship
between the wall thickness of a pressure vessel and its surface
area, which should remain valid even as the size of the vessel
changes.
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 175
Combining Features into Parts
The various types of Pro/ENGINEER features serve
as building blocks in the progressive creation of solid parts.
Certain features, by necessity, precede others in the design
process. The features that follow rely on the previously
defined features for dimensional and geometric references.
The progressive design of features can create relationships
between features already in the design and subsequent features
in the design that reference them . The following figure
illustrates the progressive design of features
3.2 Model of Shock Absorber
I] Bottom Part
Ii] Top Part
iii] Helical Spring
Iv] Total Assembly
4 ANALYSIS
4.1 Finite Element Analysis
Fem Introduction
The finite element method (FEM), sometimes referred to as
finite element analysis (FEA), is a computational technique
used to obtain approximate solutions of boundary value
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 176
problems in engineering. Simply stated, a boundary value
problem is a mathematical problem in which one or more
dependent variables must sat isfy a differential equation
everywhere within a known domain of independent variables
and satisfy specific conditions on the boundary of the domain.
Boundary value problems are also sometimes called field
problems. The field is the domain of interest and most often
represents a physical structure.
The field variables are the dependent variables of
interest governed by the differential equation. The boundary
conditions are the specified values of the field variables (or
related variables such as derivatives) on the boundaries of the
field. Depending on the type of physical problem being
analysed, the field variables may include physical
displacement, temperature, heat flux, and fluid velocity to
name only a few.
A General Procedure for Finite Element Analysis
Certain steps in formulating a finite element analysis
of a physical problem are common to all such analyses,
whether structural, heat transfer, fluid flow, or some other
problem. These steps are embodied in commercial finite
element software packages ( some are mentioned in the
following paragraphs) and are implicitly incorporated in this
text, although we do not necessarily refer to the steps
explicitly. The steps are described as follows.
Pre-processing
The pre-processing step is, quite generally, described
as defining the model and includes
Define the geometric domain of the problem.
Define the element type(s) to be used.
Define the material properties of the elements.
Define the geometric properties of the elements (length,
area)
Define the element connectivity‟s (mesh the model).
Define the physical constraints (boundary conditions).
Define the loadings.
The pre-processing (model definition) step is critical.
In no case is there a better example of the computer -related
axiom “garbage in, garbage out.” A perfectly computed finite
element solution is of absolutely no value if it corresponds to
the wrong problem.
Solution
During the solution phase, finite element software
assembles the governing algebraic equations in matrix form
and computes the unknown values of the primary field
variable(s). The computed values are then used by back
substitution to compute additional, derived variables, such as
reaction forces, element stresses, and heat flow. As it is not
uncommon for a finite element model to be represented by
tens of thousands of equations, special solution techniques are
used to reduce data storage requirements and computation
time. For static, linear problems, a wave front solver, based on
Gauss elimination, is commonly used.
Post processing
Analysis and evaluation of the solution results is referred to as
post processing. Postprocessor software contains sophisticated
routines used for sorting, printing, and plotting selected results
from a finite element solution. Examples of operations that
can be accomplished include:
Sort element stresses in order of magnitude.
Check equilibrium.
Calculate factors of safety.
Plot deformed structural shape.
Animate dynamic model behaviour.
Produce colour-coded temperature plots.
4.2 Introduction To Ansys
ANSYS has developed product lines that allow you
to make the most of your investment and choose which
product works best in your environment. ANSYS is a Finite
Element Analysis (FEA) code widely used in the Computer -
Aided Engineering (CAE) field.
ANSYS FEA software is widely recognized as the leading
fully integrated suite of Computer Aided Engineering tools
and technologies, providing the most innovative and powerful
simulation solutions to satisfy the ever -growing needs of
organizations worldwide. ANSYS solutions are broad and
highly integrated, beginning with very strong advanced
technology in all key areas including Structural, CFD,
Thermal, Electromagnetic, Dynamics, and Meshing.
Specific Capabilities of ANSYS:
Structural Analysis
It is used to determine displacements stresses, etc. under static
loading conditions. ANSYS can compute both linear and
nonlinear static analyses. Nonlinearities can include plasticity,
stress stiffening, large deflection, large strain, hyper elasticity,
contact surfaces, and creep.
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 177
4.3 Static Structural Analysis
Structural Analysis Of Existing Material
((67SiCr5 [Din 17221 Spring Steel Grade]))
CASE I: Considering the weight of 1 person (When W=1432
N)
Material :((67SiCr5 [DIN 17221 SPRING STEEL
GRADE]))
Properties: Young‟s Modulus (EX): 2100000000 Pa
Poisson‟s Ratio (PRXY): 0.27
Density: 7700 Kg/m3
Step 1: Importing Shock Absorber Model in Ansys
Workbench and Assigning the Material (Material Properties)
Step 2: Applying the Mesh (Meshing)
Step 3: Applying the Loads and Boundary Conditions
The following figure shows that the loading and boundary
condition on a shock absorber, this load is applied according
to the design of spring, Also the boundary condition is applied
at fixed position of a model which is consider as a supports,
The load is applied considering weight of one person at top
part of shock absorber model.
Step 4: Obtaining results after applying loads
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 178
Figure shows the total deflection in the shock absorber
when the load of 1432 N is applied for the existing
material 67 SiCr5.
Fig 4.1:- Total Deflection for load of 1 person
Figure shows the Maximum Shear stress in the shock absorber
when the load of 1432 N is applied for the existing material
67SiCr5. Red colour shows the Maximum stress and blue
colour shows minimum stress generated.
Fig 4.2:- Maximum Shear Stress for load of 1 person
CASE II: Considering the weight of 2 persons (When
W=1913 N)
Material :(( 67SiCr5 [DIN 17221 SPRING STEEL GRADE]))
Properties: Young‟s Modulus (EX): 2100000000 Pa
Poisson‟s Ratio (PRXY): 0.27
Density: 7700 Kg/m3
Step 1: Importing Shock Absorber Model in Ansys
Workbench and Assigning the Material (Material Properties)
Applying the Loads and Boundary Conditions:
The following figure shows that the loading and boundary
condition on a shock absorber, this load is applied according
to the design of spring, Also the boundary condition is applied
at fixed position of a model which is consider as a supports,
The load is applied considering weight of two persons at top
part of shock absorber model.
Step 2: Obtaining results after applying loads
Figure shows the total deflection in the shock absorber
when the load of 1913 N is applied for the existing
material 67SiCr5.
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 179
Fig 4.3:- Total Deflection for load of 2 persons
Following Figure shows the Maximum Shear stress in the
shock absorber when the load of 1913 N is applied for the
existing material 67SiCr5. Red colour shows the Maximum
stress and blue colour shows minimum stress generated.
Fig 4.4:- Maximum Shear Stress for load of 2 persons
Structural Analysis Of Suggested Material
((ASTM A228 [High Carbon Spring Wire]))
CASE I: Considering the weight of 1 person (When W=1432
N)
Material:(ASTM A228 [HIGH CARBON SPRING WIRE])
Properties: Young‟s Modulus (EX): 20850000000
Poisson‟s Ratio (PRXY): 0.31
Density: 7860 Kg/m3
Step 1: Importing Shock Absorber Model in Ansys
Workbench and Assigning the Material (Material Properties)
Applying the Loads and Boundary Conditions:
The following figure shows that the loading and boundary
condition on a shock absorber, this load is applied according
to the design of spring, Also the boundary condition is applied
at fixed position of a model which is consider as a supports,
The load is applied considering weight of one person at top
part of shock absorber model.
Step 2: Obtaining results after applying loads
Figure shows the total deflection in the shock absorber when
the load of 1432 N is applied for the suggested material
ASTM A228.
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 180
Fig 4.5:- Total Deflection for load of 1 person
Figure shows the Maximum Shear stress in the shock absorber
when the load of 1432 N is applied for the suggested material
ASTM A228. Red colour shows the Maximum stress and blue
colour shows minimum stress generated.
Fig 4.6:- Maximum Shear Stress for load of 1 person
CASE II: Considering the weight of 2 persons (When
W=1913 N)
Material :( ASTM A228 [HIGH CARBON SPRING WIRE])
Properties: Young‟s Modulus (EX): 20850000000 Pa
Poisson‟s Ratio (PRXY): 0.31
Density: 7860 Kg/m3
Step 1: Importing Shock Absorber Model in Ansys
Workbench and Assigning the Material (Material
Properties)
Applying the Loads and Boundary Conditions:
The following figure shows that the loading and boundary
condition on a shock absorber, this load is applied according
to the design of spring, Also the boundary condition is applied
at fixed position of a model which is consider as a supports,
The load is applied considering weight of one person at top
part of shock absorber model.
Fig. 4.7 Loading and Boundary Condition
Step 2: Obtaining results after applying loads
Figure shows the total deflection in the shock absorber when
the load of 1913 N is applied for the suggested material
ASTM A228.
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 181
Fig 4.8:- Total Deflection for load of 2 persons
Figure shows the Maximum Shear stress in the shock absorber
when the load of 1913 N is applied for the suggested material
ASTM A228. Red colour shows the Maximum stress and blue
colour shows minimum stress generated.
Fig 4.9:- Maximum Shear Stress for load of 2 person
4.4 Modal Analysis
A modal analysis is typically used to determine
the vibration characteristics (natural frequencies and
mode shapes) of a structure or a machine component
while it is being designed. It can also serve as a
starting point for another, more detailed, dynamic
analysis, such as a harmonic response or full
transient dynamic analysis. Modal analyses, while
being one of the most basic dynamic analysis types
available in ANSYS, can also be more
computationally time consuming than a typical static
analysis. A reduced solver, utilizing automatically or
manually selected master degrees of freedom is used
to drastically reduce the problem size and solution
time
Modal Analysis Results For Existing Material
((67sicr5 [Din 17221 Spring Steel Grade]))
The following bar chart indicates the frequency at
each calculated mode:
Fig 4.10 Frequency of shock absorber for existing material
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 182
Fig 4.11 :- First Mode Shape
Fig 4.12:- Second Mode Shape
Fig 4.13 :- Third Mode Shape
TABLE 1
Model > Modal > Solution
Mode Frequency [Hz]
1. 60.773
2. 67.243
3. 94.093
4. 115.63
5. 138.68
6. 140.72
7. 180.52
8. 212.66
9. 219.91
10. 237.42
Table 4.1: Frequency at ten mode shapes for existing material
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 183
Modal Analysis Results For Suggested Material
((ASTM A228 [High Carbon Spring Wire]))
The following bar chart indicates the frequency at each
calculated
mode
Fig 4.14. Frequency of shock absorber for suggested material
Fig 4.15 :- First Mode Shape
Fig 4.16:- Second Mode Shape
Fig 4.17:- Third Mode Shape
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 184
TABLE 2
Model > Modal > Solution
Mode Frequency [Hz]
1. 66.261
2. 73.316
3. 102.59
4. 126.07
5. 151.21
6. 153.43
7. 196.82
8. 231.86
9. 239.77
10. 258.86
Table 4.2 : Frequency at ten mode shapes for suggested material
5 RESULTS AND DISCUSSION
Deflection Result Table
Total Deflection in mm
Material Analytical Ansys Workbench
1
Person
Load
[W=1
432
N]
2
Person
s
Load
[1913
N]
1 Person
Load
[W=1432
N]
2
Persons
Load
[1913
N]
1) Existing
Material [
67SiCr5]
Spring Steel
7.23
9.66 7.29 9.74
2) Suggested
Material [
ASTM
A228]
Spring Steel
6.70 8.90 6.71 8.96
Table 5.1: Reduction in deflection
Graph
Reduction in Deflection (mm)
Fig 5.1. Reduction in deflection for load of single person
Fig 5.2. Reduction in deflection for load of two persons
International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015
ISSN: 2231-5381 http://www.ijettjournal.org Page 186
Graphs
Natural Frequency
Fig 5.5. Increase in Natural Frequency
CONCLUSION
1. In this project we have designed a shock absorber. We
have modeled the shock absorber by using 3D parametric
software Pro/Engineer.
2. To validate the strength of our design, we have done
structural analysis and modal analysis on the shock
absorber. We have done analysis by changing existing
material ((67SiCr5 [din 17221 spring steel grade])) to
suggested material ((ASTM A228 [high carbon spring
wire]))
3. By observing the analysis results, the analyzed stress
values are less than their respective yield stress values. So
our design is safe.
4. By comparing the results for both materials, the total
deflection value is less for ASTM A228 than 67SiCr5. So
stiffness is more for Spring Steel.
5. By comparing the results for both materials, the Natural
Frequency is more for ASTM A228 than 67SiCr5.
6. So we can conclude that as per our analysis using ASTM
A228 [high carbon spring wire] for spring is best.
REFERENCES
1) John C. Dixon, "The Shock Absorber Handbook", 2nd
Ed., John Wiley & Sons Ltd, England, 2007
2) Mr. SudarshanMartande, Design and Analysis of Shock
Absorber, IJAIEM, Volume 2, Issue 3, March 2013 ISSN
2319 – 4847
3) M.S.M.Sani, M.M. Rahman, M.M.Noor, Study on
Dynamic Characteristics of Automotive Shock Absorber
System, Malaysian Science and Technology Congress,
MSTC08, 16~17 Dec, KLCC, Malaysia, 2008.
4) PiotrCzop, Paweliwa, A COMPUTATIONAL FLUID
FLOW ANALYSIS OF A DISC VALVE SYSTEM,
Journal of KONES Powertrain and Transport, Vol. 18, No.
1 2011
5) Reybrouck K.G., A Non Linear Parametric Model of an
Automotive Shock Absorber, SAE Technical Paper Series
940869, 1994
6) Talbots M.S., An Experimentally Validated Physical
Model of a High Performance Automotive Damper, M.S.
Thesis, Purdue University, Lafayette, IN, 2002
7) Pinjarla.Poornamohan, „DESIGN AND ANALYSIS OF
A SHOCK ABSORBER‟, IJRET DEC 2012, Volume: 1
Issue: 4 578 – 592
8) Achyut P. Banginwar ,Nitin D. Bhusale, Kautuk V.
Totawar ,
Design and analysis of shock absorber using
FEA tool , Volume 10, Issue 2 (February 2014), PP.22-28
9) R. S. Khurmi and J. K. Gupta, „Machine Design‟ ,
Fourteen Edition, 2012, Eurasia Publishing House, pp.
820-833.

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Analysis report volume 2

  • 1. ISSN: 2231-5381 http://www.ijettjournal.org Page 173 Structural and Modal Analysis of Shock Absorber of Vehicle 1 , Chinmay Patil2 1 M.E Advanced Manufacturing and Mechanical System Design, Department of Mechanical Engineering, Shri Sant Gajanan Maharaj College Of Engineering, Shegaon,Maharashtra,India 2 Assistant Professor, Department of Mechanical Engineering, Shri Sant Gajanan Maharaj College Of Engineering, Shegaon,Maharashtra,India Abstract Safety and driving comfort for a car’s driver are both dependent on the vehicle’s suspension system. Safety refers to the vehicle’s handling and braking capabilities. The comfort of the occupants of a car correlates to tiredness and ability to travel long distance with minimal annoyance. Shock absorbers are a critical part of a suspension system, connecting the vehicle to its wheels. Essentially shock absorbers are devices that smooth out an impulse experienced by a vehicle, and appropriately dissipate or absorb the kinetic energy. Almost all suspe nsion systems consist of springs and dampers, which tend to limit the performance of a system due to their physical constraints. Suspension systems, comprising of springs and dampers, are usually designed for passengers’ safety, and do little to improve passenger comfort. To meet the current demands of high speed and safety we must designed and developed such a shock absorber which can sustain more and more vibrations and also improves the safety. Keywords: Springs, dampers, shock absorber 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 associated with vehicle manoeuvring, 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. When a vehicle is travelling on a level road and the wheels strike a bump, the spring is compressed quickly. The compressed spring will attempt to return to its normal loaded length and, in so doing, will rebound past its normal height, causing the body to be lifted. The weight of the vehicle will then push the spring down below its normal loaded height. This, in turn, causes the spring to rebound ag ain. This bouncing process is repeated over and over, a little less each time, until the up -and-down movement finally stops. If bouncing is allowed to go uncontrolled, it will not only cause an uncomfortable ride but will make handling of the vehicle very difficult. A safe vehicle must be able to stop and manoeuvre over a wide range of road conditions. Good contact between the tires and the road will able to stop and manoeuvre 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, cornering and overall stability. The removal of the shock absorber from suspension can cause the vehicle bounce up and down. It is possible for the vehicle to be driven, but if the suspension drops from the driving over a severe bump, the rear spring can fall out The design of spring in suspension system is very important. In this project a shock absorber will be designed and a 3D model which will be created is by using Pro/Engineer. The model is also changed by changing the thickness of the spring. Structural analysis and modal analysis are done on the shock absorber by varying material for spring.. The analysis will consider the loads, bike weight, single person and 2 persons. Structural analysis will be done to validate the strength and modal analysis to determine the displacements for different frequencies for number of modes. Comparison will be done for two materials to verify best material for spring in Shock absorber. CADmantra Technolgies Pvt. Ltd 12/5 Bhola Patel Design Engineer @ CADmantra Technolgies Pvt. Ltd Mail : bholapatel.me@gmail.com, Share on: facebookbolapatel
  • 2. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 174 Figure 1.1 Shock absorbers with different dimensions 2 DESIGN OF HELICAL COMPRESSION SPRING FOR SHOCK ABSORBER Material: ASTM A228 (modulus of rigidity) G = 184.48 *103 N/mm2 Mean diameter of a coil D=60 mm Diameter of wire d = 10 mm Total no of coils n‟= 7 Outer diameter of spring coil D0 = D +d =70mm Inner diameter of spring coil Di = D +d =70 mm No of active turns n= 5 Weight of bike = 150 Kgs Let weight of 1 person = 75 Kgs Total Weight (Wt) = Weight of bike + Weight of 1 persons = 150+75 = 225Kgs Rear suspension = 65% 65% of 225 = 146 Kgs Considering dynamic loads it will be double Wt = 292 Kgs = 2864 N For single shock absorber weight (W) =Wt/2=2864 /2 =1432 N We Know that, compression of spring (δ) = × × /× C = spring index = = = 6 = 8 (δ) = × × × /× = 6.7 Solid length, Ls=n‟×d=7*10=70 Free length of spring, Lf = solid length+maximum compression + clearance between adjustable coils = 70+6.7+6.7*0.15 = 77.7 Spring rate, K = W/(δ) =1432/6.7 =213.73 Pitch of coil, P = 13 Stresses in helical springs: maximum shear stress induced in the wire τ = K× K = + . = × × + . = 0.97 τ = K× = 0.97 × × × × = 274 N/mm2 3 CAD MODELLING CAD/ CAE Software‟s used: PRO/E wildfire 4.0 - For 3D Component Design. Pro/Assembly - For Assembling Components ANSYS Workbench 11.0 - For FEM analysis 3.1 Introduction to PRO-E Pro/ENGINEER is a parametric, feature based, solid modeling System. It is the only menu driven higher end software. Pro/ENGINEER provides mechanical engineers with an approach to mechanical design automation based on solid modeling technology and the following features. 3-D Modeling The essential difference between Pro/ENGINEER and traditional CAD systems is that models created in Pro/ENGINEER exist as three-dimensional solids. Other 3-D modelers represent only the surface boundaries of the model. Pro/ENGINEER models the complete solid. This not only facilitates the creation of realistic geometry, but also allows for accurate model calculations, such as those for mass properties. Parametric Design Dimensions such as angle, distance, and diameter control Pro/ENGINEER model geometry. You can create relationships that allow parameters to be automatically calculated based on the value of other parameters. When you modify the dimensions, the entire model geometry can update according to the relations you created. Feature-Based Modeling You create models in Pro/ENGINEER by building features. These features have intelligence, in that they contain knowledge of their environment and adapt predictably to change. Each features asks the user for specific information based on the feature type. For example, a hole has a diameter, depth, and placement, while a round has a radius and edges to round. Associativity Pro/ENGINEER is a fully associative system. This means that a change in the de sign model anytime in the development process is propagated throughout the design, automatically updating all engineering deliverables, including assemblies, drawings, and manufacturing data. Associativity makes concurrent engineering possible by encouragi ng change, without penalty, at any point in the development cycle. This enables downstream functions to contribute their knowledge and expertise early in the development cycle. Capturing Design Intent The strength of parametric modelling is in its ability to satisfy critical design parameters throughout the evolution of a solid model. The concept of capturing design intent is based on incorporating engineering knowledge into a model. This intent is achieved by establishing feature and part relationships and by the feature-dimensioning scheme. An example of design intent is the proportional relationship between the wall thickness of a pressure vessel and its surface area, which should remain valid even as the size of the vessel changes.
  • 3. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 175 Combining Features into Parts The various types of Pro/ENGINEER features serve as building blocks in the progressive creation of solid parts. Certain features, by necessity, precede others in the design process. The features that follow rely on the previously defined features for dimensional and geometric references. The progressive design of features can create relationships between features already in the design and subsequent features in the design that reference them . The following figure illustrates the progressive design of features 3.2 Model of Shock Absorber I] Bottom Part Ii] Top Part iii] Helical Spring Iv] Total Assembly 4 ANALYSIS 4.1 Finite Element Analysis Fem Introduction The finite element method (FEM), sometimes referred to as finite element analysis (FEA), is a computational technique used to obtain approximate solutions of boundary value
  • 4. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 176 problems in engineering. Simply stated, a boundary value problem is a mathematical problem in which one or more dependent variables must sat isfy a differential equation everywhere within a known domain of independent variables and satisfy specific conditions on the boundary of the domain. Boundary value problems are also sometimes called field problems. The field is the domain of interest and most often represents a physical structure. The field variables are the dependent variables of interest governed by the differential equation. The boundary conditions are the specified values of the field variables (or related variables such as derivatives) on the boundaries of the field. Depending on the type of physical problem being analysed, the field variables may include physical displacement, temperature, heat flux, and fluid velocity to name only a few. A General Procedure for Finite Element Analysis Certain steps in formulating a finite element analysis of a physical problem are common to all such analyses, whether structural, heat transfer, fluid flow, or some other problem. These steps are embodied in commercial finite element software packages ( some are mentioned in the following paragraphs) and are implicitly incorporated in this text, although we do not necessarily refer to the steps explicitly. The steps are described as follows. Pre-processing The pre-processing step is, quite generally, described as defining the model and includes Define the geometric domain of the problem. Define the element type(s) to be used. Define the material properties of the elements. Define the geometric properties of the elements (length, area) Define the element connectivity‟s (mesh the model). Define the physical constraints (boundary conditions). Define the loadings. The pre-processing (model definition) step is critical. In no case is there a better example of the computer -related axiom “garbage in, garbage out.” A perfectly computed finite element solution is of absolutely no value if it corresponds to the wrong problem. Solution During the solution phase, finite element software assembles the governing algebraic equations in matrix form and computes the unknown values of the primary field variable(s). The computed values are then used by back substitution to compute additional, derived variables, such as reaction forces, element stresses, and heat flow. As it is not uncommon for a finite element model to be represented by tens of thousands of equations, special solution techniques are used to reduce data storage requirements and computation time. For static, linear problems, a wave front solver, based on Gauss elimination, is commonly used. Post processing Analysis and evaluation of the solution results is referred to as post processing. Postprocessor software contains sophisticated routines used for sorting, printing, and plotting selected results from a finite element solution. Examples of operations that can be accomplished include: Sort element stresses in order of magnitude. Check equilibrium. Calculate factors of safety. Plot deformed structural shape. Animate dynamic model behaviour. Produce colour-coded temperature plots. 4.2 Introduction To Ansys ANSYS has developed product lines that allow you to make the most of your investment and choose which product works best in your environment. ANSYS is a Finite Element Analysis (FEA) code widely used in the Computer - Aided Engineering (CAE) field. ANSYS FEA software is widely recognized as the leading fully integrated suite of Computer Aided Engineering tools and technologies, providing the most innovative and powerful simulation solutions to satisfy the ever -growing needs of organizations worldwide. ANSYS solutions are broad and highly integrated, beginning with very strong advanced technology in all key areas including Structural, CFD, Thermal, Electromagnetic, Dynamics, and Meshing. Specific Capabilities of ANSYS: Structural Analysis It is used to determine displacements stresses, etc. under static loading conditions. ANSYS can compute both linear and nonlinear static analyses. Nonlinearities can include plasticity, stress stiffening, large deflection, large strain, hyper elasticity, contact surfaces, and creep.
  • 5. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 177 4.3 Static Structural Analysis Structural Analysis Of Existing Material ((67SiCr5 [Din 17221 Spring Steel Grade])) CASE I: Considering the weight of 1 person (When W=1432 N) Material :((67SiCr5 [DIN 17221 SPRING STEEL GRADE])) Properties: Young‟s Modulus (EX): 2100000000 Pa Poisson‟s Ratio (PRXY): 0.27 Density: 7700 Kg/m3 Step 1: Importing Shock Absorber Model in Ansys Workbench and Assigning the Material (Material Properties) Step 2: Applying the Mesh (Meshing) Step 3: Applying the Loads and Boundary Conditions The following figure shows that the loading and boundary condition on a shock absorber, this load is applied according to the design of spring, Also the boundary condition is applied at fixed position of a model which is consider as a supports, The load is applied considering weight of one person at top part of shock absorber model. Step 4: Obtaining results after applying loads
  • 6. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 178 Figure shows the total deflection in the shock absorber when the load of 1432 N is applied for the existing material 67 SiCr5. Fig 4.1:- Total Deflection for load of 1 person Figure shows the Maximum Shear stress in the shock absorber when the load of 1432 N is applied for the existing material 67SiCr5. Red colour shows the Maximum stress and blue colour shows minimum stress generated. Fig 4.2:- Maximum Shear Stress for load of 1 person CASE II: Considering the weight of 2 persons (When W=1913 N) Material :(( 67SiCr5 [DIN 17221 SPRING STEEL GRADE])) Properties: Young‟s Modulus (EX): 2100000000 Pa Poisson‟s Ratio (PRXY): 0.27 Density: 7700 Kg/m3 Step 1: Importing Shock Absorber Model in Ansys Workbench and Assigning the Material (Material Properties) Applying the Loads and Boundary Conditions: The following figure shows that the loading and boundary condition on a shock absorber, this load is applied according to the design of spring, Also the boundary condition is applied at fixed position of a model which is consider as a supports, The load is applied considering weight of two persons at top part of shock absorber model. Step 2: Obtaining results after applying loads Figure shows the total deflection in the shock absorber when the load of 1913 N is applied for the existing material 67SiCr5.
  • 7. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 179 Fig 4.3:- Total Deflection for load of 2 persons Following Figure shows the Maximum Shear stress in the shock absorber when the load of 1913 N is applied for the existing material 67SiCr5. Red colour shows the Maximum stress and blue colour shows minimum stress generated. Fig 4.4:- Maximum Shear Stress for load of 2 persons Structural Analysis Of Suggested Material ((ASTM A228 [High Carbon Spring Wire])) CASE I: Considering the weight of 1 person (When W=1432 N) Material:(ASTM A228 [HIGH CARBON SPRING WIRE]) Properties: Young‟s Modulus (EX): 20850000000 Poisson‟s Ratio (PRXY): 0.31 Density: 7860 Kg/m3 Step 1: Importing Shock Absorber Model in Ansys Workbench and Assigning the Material (Material Properties) Applying the Loads and Boundary Conditions: The following figure shows that the loading and boundary condition on a shock absorber, this load is applied according to the design of spring, Also the boundary condition is applied at fixed position of a model which is consider as a supports, The load is applied considering weight of one person at top part of shock absorber model. Step 2: Obtaining results after applying loads Figure shows the total deflection in the shock absorber when the load of 1432 N is applied for the suggested material ASTM A228.
  • 8. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 180 Fig 4.5:- Total Deflection for load of 1 person Figure shows the Maximum Shear stress in the shock absorber when the load of 1432 N is applied for the suggested material ASTM A228. Red colour shows the Maximum stress and blue colour shows minimum stress generated. Fig 4.6:- Maximum Shear Stress for load of 1 person CASE II: Considering the weight of 2 persons (When W=1913 N) Material :( ASTM A228 [HIGH CARBON SPRING WIRE]) Properties: Young‟s Modulus (EX): 20850000000 Pa Poisson‟s Ratio (PRXY): 0.31 Density: 7860 Kg/m3 Step 1: Importing Shock Absorber Model in Ansys Workbench and Assigning the Material (Material Properties) Applying the Loads and Boundary Conditions: The following figure shows that the loading and boundary condition on a shock absorber, this load is applied according to the design of spring, Also the boundary condition is applied at fixed position of a model which is consider as a supports, The load is applied considering weight of one person at top part of shock absorber model. Fig. 4.7 Loading and Boundary Condition Step 2: Obtaining results after applying loads Figure shows the total deflection in the shock absorber when the load of 1913 N is applied for the suggested material ASTM A228.
  • 9. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 181 Fig 4.8:- Total Deflection for load of 2 persons Figure shows the Maximum Shear stress in the shock absorber when the load of 1913 N is applied for the suggested material ASTM A228. Red colour shows the Maximum stress and blue colour shows minimum stress generated. Fig 4.9:- Maximum Shear Stress for load of 2 person 4.4 Modal Analysis A modal analysis is typically used to determine the vibration characteristics (natural frequencies and mode shapes) of a structure or a machine component while it is being designed. It can also serve as a starting point for another, more detailed, dynamic analysis, such as a harmonic response or full transient dynamic analysis. Modal analyses, while being one of the most basic dynamic analysis types available in ANSYS, can also be more computationally time consuming than a typical static analysis. A reduced solver, utilizing automatically or manually selected master degrees of freedom is used to drastically reduce the problem size and solution time Modal Analysis Results For Existing Material ((67sicr5 [Din 17221 Spring Steel Grade])) The following bar chart indicates the frequency at each calculated mode: Fig 4.10 Frequency of shock absorber for existing material
  • 10. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 182 Fig 4.11 :- First Mode Shape Fig 4.12:- Second Mode Shape Fig 4.13 :- Third Mode Shape TABLE 1 Model > Modal > Solution Mode Frequency [Hz] 1. 60.773 2. 67.243 3. 94.093 4. 115.63 5. 138.68 6. 140.72 7. 180.52 8. 212.66 9. 219.91 10. 237.42 Table 4.1: Frequency at ten mode shapes for existing material
  • 11. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 183 Modal Analysis Results For Suggested Material ((ASTM A228 [High Carbon Spring Wire])) The following bar chart indicates the frequency at each calculated mode Fig 4.14. Frequency of shock absorber for suggested material Fig 4.15 :- First Mode Shape Fig 4.16:- Second Mode Shape Fig 4.17:- Third Mode Shape
  • 12. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 184 TABLE 2 Model > Modal > Solution Mode Frequency [Hz] 1. 66.261 2. 73.316 3. 102.59 4. 126.07 5. 151.21 6. 153.43 7. 196.82 8. 231.86 9. 239.77 10. 258.86 Table 4.2 : Frequency at ten mode shapes for suggested material 5 RESULTS AND DISCUSSION Deflection Result Table Total Deflection in mm Material Analytical Ansys Workbench 1 Person Load [W=1 432 N] 2 Person s Load [1913 N] 1 Person Load [W=1432 N] 2 Persons Load [1913 N] 1) Existing Material [ 67SiCr5] Spring Steel 7.23 9.66 7.29 9.74 2) Suggested Material [ ASTM A228] Spring Steel 6.70 8.90 6.71 8.96 Table 5.1: Reduction in deflection Graph Reduction in Deflection (mm) Fig 5.1. Reduction in deflection for load of single person Fig 5.2. Reduction in deflection for load of two persons
  • 13. International Journal of Engineering Trends and Technology (IJETT) – Volume 21 Number 4 – March 2015 ISSN: 2231-5381 http://www.ijettjournal.org Page 186 Graphs Natural Frequency Fig 5.5. Increase in Natural Frequency CONCLUSION 1. In this project we have designed a shock absorber. We have modeled the shock absorber by using 3D parametric software Pro/Engineer. 2. To validate the strength of our design, we have done structural analysis and modal analysis on the shock absorber. We have done analysis by changing existing material ((67SiCr5 [din 17221 spring steel grade])) to suggested material ((ASTM A228 [high carbon spring wire])) 3. By observing the analysis results, the analyzed stress values are less than their respective yield stress values. So our design is safe. 4. By comparing the results for both materials, the total deflection value is less for ASTM A228 than 67SiCr5. So stiffness is more for Spring Steel. 5. By comparing the results for both materials, the Natural Frequency is more for ASTM A228 than 67SiCr5. 6. So we can conclude that as per our analysis using ASTM A228 [high carbon spring wire] for spring is best. REFERENCES 1) John C. Dixon, "The Shock Absorber Handbook", 2nd Ed., John Wiley & Sons Ltd, England, 2007 2) Mr. SudarshanMartande, Design and Analysis of Shock Absorber, IJAIEM, Volume 2, Issue 3, March 2013 ISSN 2319 – 4847 3) M.S.M.Sani, M.M. Rahman, M.M.Noor, Study on Dynamic Characteristics of Automotive Shock Absorber System, Malaysian Science and Technology Congress, MSTC08, 16~17 Dec, KLCC, Malaysia, 2008. 4) PiotrCzop, Paweliwa, A COMPUTATIONAL FLUID FLOW ANALYSIS OF A DISC VALVE SYSTEM, Journal of KONES Powertrain and Transport, Vol. 18, No. 1 2011 5) Reybrouck K.G., A Non Linear Parametric Model of an Automotive Shock Absorber, SAE Technical Paper Series 940869, 1994 6) Talbots M.S., An Experimentally Validated Physical Model of a High Performance Automotive Damper, M.S. Thesis, Purdue University, Lafayette, IN, 2002 7) Pinjarla.Poornamohan, „DESIGN AND ANALYSIS OF A SHOCK ABSORBER‟, IJRET DEC 2012, Volume: 1 Issue: 4 578 – 592 8) Achyut P. Banginwar ,Nitin D. Bhusale, Kautuk V. Totawar , Design and analysis of shock absorber using FEA tool , Volume 10, Issue 2 (February 2014), PP.22-28 9) R. S. Khurmi and J. K. Gupta, „Machine Design‟ , Fourteen Edition, 2012, Eurasia Publishing House, pp. 820-833.