Design and Analysis of Leaf Spring for Light Vehicle Mini Truck
10667 words (43 pages) Dissertation
13th Dec 2019 Dissertation Reference this
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Abstract
In present scenario weight reduction is the main focus of an automobile manufacturer. Leaf spring is an important component for any automobile. Generally leaf spring is used for suspension purpose in heavy vehicles. These springs are mainly made of steel material which having more weight. In order to reduce weight, here composite leaf spring is used instead of steel leaf spring.
This dissertation describes design and static analysis of steel leaf spring and laminated composite leaf spring. The dimensions of an existing conventional steel leaf spring of a mini truck are taken and are verified by design calculations. Static structural analysis of a 3-D model of conventional leaf spring is performed using ANSYS. Same dimensions are used in composite multi leaf spring using carbon/Epoxy and Graphite/Epoxy unidirectional laminates. The load carrying capacity, and weight of composite leaf spring are compared with that of steel leaf spring. The fatigue life is also calculated using analytically as well as using ANSYS for steel leaf spring. The frequency and mode shapes are determined using modal analysis. The size optimization is carried out for further mass reduction of composite leaf spring. The thickness of each leaf is reduced as a result of size optimization. The mass reduction has been Gained nearly 88.97 % using composite mono leaf spring. Residual stress generated in each leaf is also calculated analytically.
Nomenclature
L = Length of spring
n = No. of leaves
b = Width of spring
t = Thickness of spring
δ= Deflection of spring
σ = Bending stress
E = Modulus of elasticity
σmax = Max. tensile stress
σf = Fatigue strength co-efficent
b = Fatigue strength exponent
c = Fatigue ductility exponent
sf = Fatigue ductility co-efficent
sa = Strain Amlitute
viii
Contents
Nomenclature viii
- Introduction 1
1.1 Preliminary Remark . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1.2 Objective . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1.3 Lay Up of the report . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
1.4 Leaf Spring . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
1.5 Construction of Leaf Spring . . . . . . . . . . . . . . . . . . . . . . . 6
1.6 Standard Sizes of Suspension Leaf Spring . . . . . . . . . . . . . . . . 8
1.7 Material of Leaf Spring . . . . . . . . . . . . . . . . . . . . . . . . . . 8
1.8 Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
1.9 Manufacturing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
- Literature Review 11
- Design of Multi Leaf Spring 20
ix
- Deflection Calculation………………………………………..22
- Spring Rate Calculation………………………………………22
- Radius of Curvature…………………………………………22
- Static Analysis in Leaf Spring 23
- Preprocessor……………………………………………….23
- Solution…………………………………………………..24
- Postprocessor………………………………………………24
- Meshing………………………………………………….24
- Sizing Control………………………………………………25
- Boundary Conditions………………………………………..25
- Result……………………………………………………26
- Static analysis result in leaf spring using steel material…………..26
- Static analysis result in leaf spring using composite materials . 27
- Results table…………………………………………..29
- Fatigue Analysis and Modal Analysis in Leaf Spring 30
- Size Optimization 42
- Residual Stress Calculation 46
- Conclusion and future Scope 51
List of Figures
1.1 Flat spring cantilever type . . . . . . . . . . . . . . . . . . . . . . 3
- (a) Cross-section of plate (b) Bending stress (c)Shear stress diagram 4
- Flat spring simply supported beam type . . . . . . . . . . . . . . 4
- Flat spring simply supported beam type . . . . . . . . . . . . . . 5
- 1.5 Laminated leaf spring . . . . . . . . . . . . . . . . . . . . . . . . . 6
- Semi elliptical leaf spring . . . . . . . . . . . . . . . . . . . . . . 7
- (a) Eye end of the first design (b)Wrap of the eye-end section (c)The design with the open eye end[4] 15
- Variations of thickness along the optimized spring[11]…………….18
- Variations of width along the optimized spring[11]……………….19
- Meshing………………………………………….25
- Von-Mises stress in steel material leaf spring………………….26
- Deflection in steel material leaf spring………………………27
- Von-Mises stress in composite material leaf spring………………27
- Deflection in composite material leaf spring…………………..28
- Von-Mises stress in composite material Mono leaf spring using Hyper- Mesh 28
- Displacement in composite material Mono leaf spring using HyperMesh 29
- strain approach cycle………………………………….32
- strain – reversals graph………………………………..33
- Fatigue life calculated using Morrow Approach for Leaf Spring……….36
- Fatigue life calculated using Mean Approach for Leaf Spring………..36
- Fatigue life calculated using SWT Approach for Leaf Spring…………37
- First mode shape natural frequency using hyperMesh…………….40
- Second mode shape natural frequency using hyperMesh…………..40
- Third mode shape natural frequency using hyperMesh……………40
- Fourth mode shape natural frequency using HyperMesh…………..41
- Fifth mode shape natural frequency using HyperMesh…………….41
- von misses stress in mono leaf spring using hyper mesh……………44
- Deflection in mono leaf spring using hyper mesh………………..44
xii
LISTOFFIGURES xiii
- After Optimization mono leaf spring using hyper mesh……………45
7.1 Single Leaf of the Spring………………………………….50
List of Tables
1.1 Dimension for center bolt . . . . . . . . . . . . . . . . . . . . . . . . 8
1.2 Dimension for clip, rivet , bolt . . . . . . . . . . . . . . . . . . . . . . 8
- Material properties of Steel materials……………………….20
- Properties for composite material………………………….21
- Static result analytical and FEA comparison…………………..29
- Static steel and composite result comparison…………………..29
- Fatigue Material properties……………………………..34
- Predicted fatigue life using strain life approach…………………37
7.1 Residual stress calculation…………………………………50
xiv
Chapter 1 Introduction
1.1 Preliminary Remark
A leaf spring is a simple form of spring commonly used for the suspension in wheeled vehicles. Originally called a laminated or carriage spring, and sometimes referred to as a semi-elliptical spring or cart spring.
A leaf spring takes the form of a slender arc-shaped and rectangular cross section. The center of the arc provides location for the axle, while tie holes are provided at either end for attaching to the vehicle body. For very heavy vehicles, a leaf spring can be made from several leaves stacked on top of each other in several layers, often with progressively shorter leaves. Leaf springs can serve locating and to some ex- tent damping as well as springing functions. While the interleaf friction provides a damping action, it is not well controlled and results in stiction in the motion of the suspension. For this reason manufacturers have experimented with mono-leaf springs.
1.2 Objective
The objective of this report is as follows:
- Replace Composite leaf spring instead of steel leaf spring.
1
- Size optimization of composite leaf spring.
- Frequency calculation for different mode shape.
- Life cycle calculation of leaf spring.
- Residual stress calculation of different leaves of leaf spring.
1.3 Lay Up of the report
The lay-up of this report is as follows:
- Second chapter covers literature review in that give a brief idea about the various research has been done in the composite leaf spring.
- Third chapter includes static analysis in steel and composite leaf spring and compare results in FEA and analytically.
- Fourth chapter contains size optimization leaf spring.
- Fifth chapter consists of fatigue analysis in leaf spring compare with FEA and Analytically. and frequency calculation for different mode shape.
- Sixth chapter contains Residual stress in leaf spring on different leaves.
1.4 Leaf Spring
Single plate fixed at one end and loaded at the other end as shown in fig.1.1. This
plate may be used as a flat spring.
Figure 1.1: Flat spring cantilever type
The bending stress and deflection of this flat plate is calculated using following equation.
Bending stress in spring:
Deflection of spring:–
6WL
σ = Bt2
4WL3
δ = EBt3
(1.1)
(1.2)
In the bending moment, top fiber will be in tension and bottom fibers in compres- sion, but the shear stress is zero at the extreme fibers and maximum at the center. Bending stress zero at the centre where shear stress maximum at the center as shown in fig 1.2.
Figure 1.2: (a) Cross-section of plate (b) Bending stress (c)Shear stress diagram
If we consider the spring as simply supported beam the length is 2L and load 2W as shown in fig 1.3.The bending stress and deflection of this flat plate is calculated using following equation.
Figure 1.3: Flat spring simply supported beam type
The bending stress and deflection of this flat plate is calculated using following equation.
Bending stress in spring:
6WL
σ = Bt2
(1.3)
Deflection of spring:
WL3
δ =
3EI
(1.4)
If we consider n-strips cantilever beam having width b and thickness t then we can use equation 1.5 and 1.6. and n-strips cantilever beam is shown in fig 1.4.The bending stress and deflection of this flat plate is calculated using following equation.
Figure 1.4: Flat spring simply supported beam type
Bending stress in spring:
6WL
σ = nBt2
(1.5)
Deflection of spring:
4WL3
δ = nEBt3
(1.6)
The above relations give the stress and deflection of a spring of uniform cross section. The stress at such a spring is maximum at the support. If we consider triangular plate is used as shown in fig.1.5 the stress will be uniform throughout. If this triangle plate is cut into strips of width and Fitted one below the other as shown fig 1.5 to form a graduated or laminated leaf spring, then The bending stress and deflection
of this flat plate is calculated using following equation.
Figure 1.5: Laminated leaf spring
Bending stress of leaf spring;
6WL
σ = nBt2
(1.7)
Deflection of spring:
6WL3
δ = nEBt3
(1.8)
1.5 Construction of Leaf Spring
A Leaf spring is generally used in automobiles is of semi elliptical form shown in fig.1.6. It is built up of a number of plates. The leaves are usually given an initial curvature or cambered so that they will tend to straighten under the load .The leaves are held together by means of a band shrunk around them at the center or by a bolt passing through the center. Since the band exerts a stiffening and strengthening effect, therefore the effective length of the spring for bending will be the overall length
of the spring minus width of band. In case of a center bolt, two-third distance between center of bolt should be subtracted from the overall length of the spring in order to find effective length. The spring is clamped to the axle housing by means of U-bolts. The longer leaf known as main leaf or master leaf has its ends formed in the formed
Figure 1.6: Semi elliptical leaf spring
in the shape of an eye through which the bolts are passed to secure the spring to its supports. Usually the eyes, through which the spring is attached to the hanger or shackle, are provided with the bushing of some antifriction materials such as bronze or rubber. The other leaves of the spring are known graduated leaves. In order to prevent digging in the adjacent leaves, the ends of graduated leaves are trimmed in various forms as shown in fig.1.6. Since the master leaf has to with stand vertical bending loads as well as loads due to sideways of the vehicle and twisting, therefore due to presence of stresses caused by these loads, it is usual to provide two full length leaves and the rest graduated as shown in fig.1.6.
Table 1.1: Dimension for center bolt
Width of leaves mm | Dia. Of center bolt (mm) | Dia. Of head bolt (mm) | Length of bolt head (mm) |
Up to and including 65 | 8 or 10 | 12 to 15 | 10 or 11 |
Above 65 | 12 or16 | 17 or 20 | 11 |
Table 1.2: Dimension for clip, rivet , bolt
Spring width mm | Clip section (b * t) mm*mm | Dia. Of rivet (d1) mm | Dia. Of bolt(d2) mm |
Under 50 | 20*4 | 6 | 6 |
50, 55 and 60 | 25*5 | 8 | 8 |
65,70,75 and 80 | 25*6 | 10 | 8 |
90,100 and 125 | 32*6 | 10 | 10 |
1.6 Standard Sizes of Suspension Leaf Spring
• Standard nominal widths are: 32,40,45,55,60,65,70,75,80,90,100 and 125 mm.
• Standard nominal thickness are: 3.2,4.5,5,6,6.5,7,7.5,8,9,10,11,12,14 and 16 mm.
- At the eye, the following bore diameter are recommended- 19,20,22,23,25,27,28, 30,32,35,38,50,55 mm.
- Dimension for the centre bolts, if employed, shall be as given in the table 1.1.
- Minimum clip sections and the corresponding sizes of rivets and bolts used with the clips shall be as given in the table 1.2.
Chapter 3
Design of Multi LeafSpring
3.1 Properties for Steel and Composite Material
Consider loaded mini truck leaf spring load carrying 80000 N, length 1025 mm , Width 60 mm, thickness 16 mm, Camber distance 90.8 mm. and number of the leaves are 10.The material properties for steel and composite materials are as shown in table 3.1 and 3.2
Table 3.1: Material properties of Steel materials
parameter | values |
Material Selected | Steel(Sup9) |
Young’s Modulus, E | 2.1*10ˆ5 N/mm2 |
Possion’s Ratio | .266 |
BHN | 400-425 |
Tensile strength Ultimate | 1272 Mpa |
Tensile strength Yield | 1158 Mpa |
Density | 7850 Kg/m3 |
20
Table 3.2: Properties for composite material
parameter | values |
Exx | 206.85 Mpa |
Eyy | 517.12 Mpa |
Ezz | 517.13 Mpa |
Mx | .26 |
My | .26 |
Mz | .26 |
Gxy | 258.6 Mpa |
Gyz | 258.6 Mpa |
Gxz | 258.6 Mpa |
Density | 1602 kg/m3 |
3.2 Design Calculation
In design of leaf spring these condition must be satisfy,
σa“σ δmax“δ
3.3 Bending Stress Calculation
If σa“σthen Design is safe.
Allowable Stress:
σmax
σa = FactorofSafety = 508.8MPa (3.1)
Bending Stress:
6WL
σ = nbt2
= 187.7 MPa (3.2)
Here σa“σso design is safe.
If δmax“δthen Design is safe.
Max. Deflection:
σL2
δmax = 6tE = 16.35mm (3.3)
Deflection of spring
6PL3
δ =
(3nf + 2ng )Ebt3
= 6.69mm (3.4)
Here δmax“δso design is safe.
3.5 Spring Rate Calculation
p
K= = 1347.3053N/mm (3.5)
δ
3.6 Radius of Curvature
L2
R =
8δ0
= 1446.34mm (3.6)
Chapter 4
Static Analysis in LeafSpring
A stress-deflection analysis is performed using finite element analysis (FEA). The complete Steps of analysis has been done using ANSYS. To conduct finite element analysis, the general process of FEA is divided into three main phases.
- Preprocessor
- Solution
- Postprocessor
4.1 Preprocessor
The preprocessor is a program that processes the input data to produce the output that is used as input to the subsequent phase (solution). Following are the input data that need to be given to the preprocessor
- Type of analysis
- Geometric modal
- Type of Element
- Material properties
23
- Meshing
- Loading Conditions
- Boundary Conditions
4.2 Solution
Solution phase is completely automatic. The FEA software generates the element matrices, computes nodal values and derivatives, and stores the result data in files. These files are further used by the subsequent phase (postprocessor) to review and analyze the results through the graphic display and tabular listings.
4.3 Postprocessor
The output from the solution phase is in the numerical form and consists of nodal values of the field variable and its derivatives. material used for the leaf spring for analysis is structural steel, which has approximately similar isotropic behavior and properties as compared to SUP9.
4.4 Meshing
Meshing is the process in which your geometry is spatially discredited into elements and nodes. This mesh along with material properties is used to mathematically represent the stiffness and mass distribution of the structure. The mesh has been generated automatically. The default element size is determined based on a number
of factors including the overall model size, the proximity of other topologies, body curvature, and the complexity of the feature. If necessary, the fineness of the mesh is adjusted up to four times (eight times for an assembly) to achieve mesh. As shown in fig 4.1 Number of elements used are 56568 and and number of nodes used are 286796.
.
Figure 4.1: Meshing
4.5 Sizing Control
The sizing control sets the element size for a selected body, face, edge. The number of divisions along an edge. The element size within a user of influence that can include a selected body, face, edge, or vertex. This control is recommended for local mesh sizing. The control must also be attached to a coordinate system if it is to be scoped to anything other than a vertex.
4.6 Boundary Conditions
The boundary condition is the collection of different forces, pressure, velocity, sup- ports. Applying boundary condition is one of the most typical processes of analy- sis. A special care is required while assigning loads and constraints to the elements. Boundary condition of the spring involves the fixation of one of the revolute joint and applying displacement support at the other end of leaf spring. Loading conditions involves applying a load upper side at the centre of the main leaf.
4.7 Result
4.7.1 Static analysis result in leaf spring using steel material
- Make simplified 3D model leaf spring in SolidWorks.
- Make and save above modal STEP format and importing in to ANSYS.
- After importing modal provide material properties as table 3.1.
- After providing material properties Make mesh.
- After providing mesh input boundary condition one end fixed and other end X and Y axis displacement is given.Loading conditions involves applying a load upper side at the centre of the bottom leaf.
- After Solving the model for static structural analysis and bending stress and deflection as shown in fig 4.2 to 4.3.
Figure 4.2: Von-Mises stress in steel material leaf spring
Figure 4.3: Deflection in steel material leaf spring
4.7.2 Static analysis result in leaf spring using composite ma- terials
For composite material same Steps has been adopted as steel material except material properties. After solving the model for static structural analysis Von-Mises stress plot is as shown in fig. 4.4. The deflection plot for the same model is as shown in fig. 4.5.
Figure 4.4: Von-Mises stress in composite material leaf spring
Figure 4.5: Deflection in composite material leaf spring
If we consider mono leaf spring and taken same dimension as multi leaf spring only thickness is varies by considering same deflection and same von-Mises stress. Mono composite leaf spring weight reduction is Gained 90.09%. Using HyperMesh, considering mono leaf spring as shown in fig.4.6 maximum Von-Misses stress Gained 190 MPa and maximum deflection is Gained as shown in fig. 4.7 is 7.11 mm. The thickness for mono leaf spring is derived 36 mm.
Figure 4.6: Von-Mises stress in composite material Mono leaf spring using HyperMesh
Figure 4.7: Displacement in composite material Mono leaf spring using HyperMesh
4.7.3 Results table
As shown in table 4.1 deflection value analytically 6.60 mm and FEA 6.34 mm so 5.56% difference and bending stress value analytically 187.68 MPa and 206.1 MPa so 9.064% difference.
Table 4.1: Static result analytical and FEA comparison
Parameter | Analytical | FEA | Difference |
Deflection | 6.69 mm | 6.34 mm | 5.56% |
Bending Stress | 187.7 Mpa | 206.1 Mpa | 9.06% |
As shown in table 4.2 compression of mass properties steel and composite material. Composite material mass reduction is 90.094% Gained.
Table 4.2: Static steel and composite result comparison
Parameter | Steel | Composite | Difference |
Bending Stress | 187.5 Mpa | 135 Mpa | 5.8% |
Mass | 44.494 kg | 5.1 kg | 90.09% |
Chapter 5
Fatigue Analysis and Modal Analysis in Leaf Spring
5.1 Fatigue Analysis
5.1.1 Introduction
Fatigue occurs when a material is subjected to repeated loading and unloading. If the loads are above a certain threshold, microscopic cracks will begin to form at the stress concentration such as the surface and grain interfaces. Eventually a crack will reach a critical size, and the structure will suddenly fracture. The shape of the structure will significantly affect the fatigue life; square holes or sharp corners will lead to elevated local stresses where fatigue cracks can initiate. Round holes and smooth transitions or fillets are therefore important to increase the fatigue strength of the structure.
30
5.1.2 Characteristics of fatigue
- In metals and alloys, when there are no macroscopic or microscopic discon- tinuities, the process starts with dislocation movements, eventually forming persistent slip bands that nucleate short cracks.
- Macroscopic and microscopic discontinuities as well as component design fea- tures which cause stress concentration (keyways, sharp changes of direction etc.) are the preferred location for starting the fatigue process.
- Fatigue is a stochastic process, often showing considerable scatter even in con- trolled environments.
- The greater the applied stress range, the shorter the life.
- Fatigue life scatter tends to increase for longer fatigue lives.
- Damage is cumulative. Materials do not recover when rested.
- Fatigue life is influenced by a variety of factors, such as temperature, surface finish, microstructure, presence of oxidizing or inert chemicals, residual stresses, contact (fretting), etc.
5.1.3 Fatigue Analysis
Analysis of fatigue can be carried out by in three basic Method:
- Strain Approach
- Stress Approach
- Crack Propagation
Strain life Approach three is again classified into three methods as:
- Morrow Approach
- Mean Approach
- SWT (Smith-Watson-Topper)Approach
Strain controlled tests are always conducted in axial loading. Deflections are con- trolled and converted into strain. The resulting forces are measured to compute the applied stress. Metals undergo transient behavior when they are first cycled. In this
Figure 5.1: strain approach cycle
Before plotting the strain vs. fatigue life, the total strain that was controlled during
the test is divided into the elastic and plastic part. The elastic strain is computed as the stress range divided by the elastic modulus. Plastic strain is obtained by sub- tracting the elastic strain from the total strain. The total strain is then obtained by
Figure 5.2: strain – reversals graph
adding the elastic and plastic portions of the strain to obtain a relationship between the applied strain and the fatigue life.
The material deformation during a fatigue test is measured in the form of a hysteresis loop. After the initial transient behavior the material stabilizes and the same hys-
teresis loop is obtained for every loading cycle. Each strain range tested will have a corresponding stress range that is measured. The cyclic stress strain curve is a plot of all of this data.
Fatigue Material Properties :
The fatigue material properties are described in table 5.1.
Table 5.1: Fatigue Material properties
Parameter | Values |
Material Selected | Steel(Sup9) |
Young’s Modulus, E | 2.1*10ˆ5 N/mm2 |
Tensile strength Ultimate | 1272 Mpa |
Tensile strength Yield | 1158 Mpa |
Fatigue Strength co-efficient | 2063 Mpa |
Fatigue Strength exponent | -.08 |
Fatigue ductility coefficient | 9.56 |
Fatigue ductility exponent | -1.05 |
The Equation for strain life approaches are as follows.
Morrow Approach:
sa =
σf (2N∗)b
E
+ sf(2N σm
∗)c
(5.3)
Nf = N∗(1 −
) (5.4)
σf
Mean Approach:
sa =
σf − σm (2N )b
E f
+ sf(2Nf)c
(5.5)
SWT (Smith-Watson-Topper) Approach:
saσmax =
σf 2
(2Nf)2b
E
+ sfσf(2Nf)
b+c
(5.6)
5.2 Loading Information
Loading is major input for the finite element based fatigue analysis. Unlike static stress, which is analyzed with calculations for a single stress state, fatigue damage occurs when stress at a point changes over time.
Here non-constant amplitude, proportional loading has been considered within the ANSYS. Fatigue Module uses a“quick counting” technique to substantially reduce runtime and memory. In quick counting, alternating and mean stresses are sorted into bins before partial damage is calculated.
5.3 Fatigue Analysis using FEA
The Steps for fatigue analysis using FEA is explained as follows.
- Make simplified 3D model leaf spring in SolidWorks.
- Make and save above modal STEP format and importing in to HyperMesh.
- After importing modal and provide material properties as table 3.1.
- After providing material properties Make mesh.
- After providing mesh input boundary condition one end fixed and other end X and Y axis displacement is given. Loading conditions involves applying a load upper side at the centre of the bottom leaf.
- After Solving the model for fatigue analysis and obtain life cycle as shown in fig 5.3 to 5.5.
As shown in fig 5.3, 5.4 and 5.5 are FEA result of strain based approach. Using three strain approach and calculated life cycle for leaf spring. Fig 5.4 is for Morrow approach, Fig. 5.5 is for Mean approach and Fig 5.6 for SWT approach to calculate fatigue life.
Figure 5.3: Fatigue life calculated using Morrow Approach for Leaf Spring
Figure 5.4: Fatigue life calculated using Mean Approach for Leaf Spring
Figure 5.5: Fatigue life calculated using SWT Approach for Leaf Spring
5.4 Fatigue Analysis Result
Using strain based approach fatigue life has been calculated using analytically as well as FEA. The %difference is given in table 5.2.
Table 5.2: Predicted fatigue life using strain life approach
Approach | Analytical(life cycle) | FEA (life cycle) | %Difference |
Mean | 8.9e4 | 9.40e4 | 5.31 |
Morrow | 1.2e4 | 1.0081e4 | 16 |
SWT | 1.15e4 | 1.02e4 | 11.13 |
5.5 Modal Analysis
Modal analysis is the field of measuring and analyzing the dynamic response of struc- tures and or fluids when excited by an input. The goal of modal analysis in structural mechanics is to determine the natural mode shapes and frequencies of an object or structure during free vibration. It is common to use the finite element method (FEM) to perform this analysis because, like other calculations using the FEM, the object being analyzed can have arbitrary shape and the results of the calculations are acceptable. The types of equations which arise from
modal analysis are those seen in eigen systems. The physical interpretation of the eigenvalues and eigenvectors which come from solving the system are that they rep- resent the frequencies and corresponding mode shapes. Sometimes, the only desired modes are the lowest frequencies because they can be the most prominent modes at which the object will vibrate, dominating all the higher frequency modes..
5.6 FEA Eigen System
For the most basic problem involving a linear system elastic material the obeys hook’s law the matrix equation takes the form of a dynamic three a dimensional spring mass system. The generalized equation of motion is given as:
[M]*[U¨ ] + [C]*[U˙ ] + [K]*[U] = [F]
where,
[M] is mass matrix
[U¨ ] Second derivative Accerlation [U] Displacement
[U˙ ] velocity
[C] Damping matrix [K] Stiffens matrix [F] Force vector.
The general with nonzero damping is a quadratic eigenvalue problem. Howerver, for vibrational model analysis the damping is generally ignored leaving only the 1stand 3rdterms on the hand side:
[M][U¨ ] + [K][U] = 0
This is the general from of the eigen system encountered in structure engineering
using the FEM vibration sollutoin of the structure harmonic motion is assumed so that [U¨ ] is taken to equal λ[U],where λis an eigenvalue and the equation reduce to:
[M][U¨ ]λ+ [K][U] = 0
In construct , the equation for static problem is: [k] [U] = [F]
Which is expected when are terms having a time derivatives are set to zero.
5.7 FEA Steps for Modal Analysis
The Steps for model analysis using FEA is described as follows.
- Make simplified 3D model leaf spring in SolidWorks.
- Make and save above modal STEP format and importing in to HyperMesh.
- After importing modal provide material properties as table 3.1.
- After providing material properties Make mesh.
- After providing mesh input boundary condition one end fixed and other end X and Y axis displacement.
- After Solving the model for modal analysis and obtain mode shape as shown in fig 5.7 to 5.10.
Different mode shape having different natural frequencies as shown in fig. 5.6 to 5.10. Here first five shapes has been found.
Figure 5.6: First mode shape natural frequency using hyperMesh
Figure 5.7: Second mode shape natural frequency using hyperMesh
Figure 5.8: Third mode shape natural frequency using hyperMesh
Figure 5.9: Fourth mode shape natural frequency using HyperMesh
Figure 5.10: Fifth mode shape natural frequency using HyperMesh
Chapter 6
SizeOptimization
Size optimization is part of the field of optimal control theory. The typical problem is to find the shape which is optimal in that it minimizes a certain cost functional while satisfying given constraints. In many cases, the functional being solved depends on the solution of a given partial differential equation defined on the variable domain. Shape optimization problems are usually solved numerically, by using iterative meth- ods. That is, one starts with an initial guess for a shape, and then gradually evolves it, until it morphs into the optimal shape.
In mathematics and computer science, an optimization problem is the problem of finding the best solution from all feasible solutions. Optimization problems can be divided into two categories depending on whether the variables are continuous or dis- crete. An optimization problem with discrete variables is known as a combinatorial optimization problem. In a combinatorial optimization problem, we are looking for an object such as an integer, permutation or graph of a finite (or possibly countable infinite) set.
6.1 Continues optimization problem
The standard form of optimization problem is
42
minimization f(x) subjected to
gi(x)≤0 i= 1……m
hi(x)≥0 i= 1……n
where f(x): Rn −→R is the objective function to be minimized over the variable , gi(x)≤0 are called inequality constraints, and
hi(x)≥0 are called equality constraints.
By convention, the standard form defines a minimization problem. A maximization problem can be treated by negating the objective function.
6.2 Steps for Size Optimization
The Steps for optimization is described as follows.
- Make simplified 3D model leaf spring in SolidWorks.
- Make and save above model STEP format and importing in to HyperMesh.
- After importing model provide material properties as table 3.2.
- After providing material properties Make mesh.
- After providing mesh input boundary condition one end fixed and other end X and Y axis displacement is given. Loading conditions involves applying a load upper side at the centre of the bottom leaf.
- After boundary condition Make in analysis page optimization.
- In optimization constraints considered is stress and objective function mini- mization mass.
- After solving the model for size optimization and obtain reduction thickness as shown in fig 6.3.
6.2.1 Before optimization
See the Fig. 6.1 and 6.2 are the result of before optimization. The weight of the spring is 5.18 kg and thickness is 36 mm.
Figure 6.1: von misses stress in mono leaf spring using hyper mesh
Figure 6.2: Deflection in mono leaf spring using hyper mesh
6.2.2 After optimization
As shown in Fig. 6.3 is the result of After optimization. After five iteration weight in leaf spring reduced up to 5.01 kg and thickness 35 mm obtained. So 1 mm thickness reduction is Gained.
Figure 6.3: After Optimization mono leaf spring using hyper mesh
Chapter 7
Residual Stress Calculation
Residual stress is defined as “the stress resident inside a component or structure after all applied forces have been removed”. Compressive residual stress acts by pushing the material together, while tensile residual stress pulls the material apart.
Mathematically, compressive stress is negative and tensile stress is positive. Stresses can also be characterized as normal stresses that act perpendicular to the face of a material and shear stresses that act parallel to the face of a material. There is a total of 6 independent stresses at any point inside a material represented by σijwhere i is the direction that the stress is acting and j is the face the stress is acting on.
Residual stresses or locked-in stresses can be defined as those stresses existing within a body in the absence of external loading or thermal gradients. In other words residual stresses in a structural material or component are those stresses which exist in the object without the application of any service or other external loads.
Residual stress is usually defined as the stress which remains in mechanical parts which are not subjected to any outside stresses. Residual stress exists in practically all rigid parts, whether metallic or not (wood, polymer, glass,ceramic, etc). It is the result of the metallurgical and mechanical history of each point in the part and the part as a whole during its manufacture. It exists at different levels, generally divided into three, depending on the scale on which the stress is observed.
46
7.1 Factors that cause residual stresses
Residual stresses can be present in any mechanical structure because of many causes. Residual stresses may be due to the technological process used to make the compo- nent. Manufacturing processes are the most common causes of residual stress. Virtu- ally all manufacturing and fabricating processes such as casting, welding, machining, molding, heat treatment, plastic deformation during bending, rolling or forging intro- duce residual stresses into the manufactured object. Residual stress could be caused by localized yielding of the material, because of a sharp notch or from certain surface treatments like shot peening or surface hardening. Among the factors that are known to cause residual stresses are the development of deformation gradients in various sections of the piece by the development of thermal gradients, volumetric changes arising during solidification or from solid state transformations, and from differences
in the coefficient of thermal expansion in pieces made from different materials. Thermal residual stresses are primarily due to differential expansion when a metal is heated or cooled. The two factors that control this are thermal treatment (heating or cooling) and restraint. Both the thermal treatment and restraint of the component must be present to generate residual stresses.
When any object is formed through cold working, there is the possibility for the de- velopment of residual stresses.
A good common example of mechanically applied residual stresses is a bicycle wheel. A bicycle wheel is a very light and strong because of the way in which the com- ponents are stressed. The wire spokes are radial aligned and tightening the spokes Makes tensile radial stresses. The spokes pull the rim inward, creating circumfer- ential compression stresses in the rim. Conversely, the spokes pull the tubular hub outward. If the thin spokes were not under a proper tensile preloaded the thin wire spokes could not adequately support the load of the rider.
7.2 Residual stress Calculation in leaf spring
Residual stress calculation in different leaves of leaf spring has been described below. As shown in fig 7.1 one leaves of leaf spring and below calculation is done for single leaves spring.
For single leaf of spring, residual stress calculation method has been explained. Fig.7.1 is shows single leaf of spring.
CG of the leaves y = 28.80 mm
I = Moment of inertia about y-Axis
db3
I =
12
= 2.04e6mm4 (7.1)
Figure 7.1: Single Leaf of the Spring
WL2
M =
8
= 2.162e6N∗mm (7.2)
σ = M ∗ Y
I
= 305.22MPa (7.3)
Max.ResidualStress= YieldStress−305.22 = 852.77Mpa (7.4)
Table 7.1 shows bending stress and residual stress for all 10 leaves of leaf spring.
Table 7.1: Residual stress calculation
Leaves no. | y
mm |
L
mm |
M
N.mm |
Bending stress
(σ (MPa)) |
Residual stress (σmax(MPa)) | Residual stress (σmin(MPa)) |
1 | 46.78 | 1025 | 2.402e6 | 390.158 | 767.842 | -767.842 |
2 | 28.80 | 922.5 | 2.042e6 | 305.22 | 852.77 | -852.77 |
3 | 25.36 | 820 | 1.91e6 | 238.68 | 919.32 | -919.32 |
4 | 20.25 | 717.5 | 1.68e6 | 166.76 | 991.24 | -991.24 |
5 | 16.89 | 615 | 1.44e6 | 119.339 | 1038.661 | -1038.66 |
6 | 14.17 | 512.5 | 1.20e6 | 83.43 | 1074.57 | -1074.57 |
7 | 12.89 | 410 | 9.6e5 | 60.718 | 1097.282 | -1097.28 |
8 | 11.10 | 307.5 | 7.2e5 | 39.214 | 1118.786 | -1118.78 |
9 | 10.15 | 205 | 4.8e5 | 23.789 | 1134.211 | -1134.21 |
10 | 9.05 | 102.5 | 2.4e5 | 10.647 | 1047.353 | -1047.35 |
Chapter 8
Conclusion and future Scope
8.1 Conclusion
The design and static structural analysis of steel leaf spring and laminated composite leaf spring has been carried out. Comparison has been made between laminated composite leaf spring with steel leaf spring having same design and same load carrying capacity. From that 79.9 % mass reduction in composite material has been Gained for the same number of leaves. The fatigue life has been calculated using analytically as well as using ANSYS for steel leaf spring. The size optimization has been carried out for further mass reduction of composite leaf spring. From that 90 % mass reduction has been Gained using mono composite leaf spring compared to steel multi leaf spring.
8.2 Future Scope
- Non-linear analysis for leaf spring.
- Residual stress calculation using FEA.
- Manufacturing of composite leaf spring.
- Experimental results for composite leaf spring.
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