IRJET- Design, Development and Testing of CFRC Tie Rod

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 08 | Aug 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 369
Design, Development and Testing of CFRC Tie Rod
Akash Salokhe1, Dr. A.P. Tadamalle2
1PG Student, Dept. of Mechanical Engineering, Sinhgad College of Engineering, Vadgaon bk, Pune 411041.
2Professor, Dept. of Mechanical Engineering, Vadgaon bk, Pune 411041.
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Abstract - Design of suspension components in an automotive is very critical as they are constantly under varying loads. The
tie rod is an important part of suspension system. It connects the steering to the suspension in order to transform the motion.
Buckling of tie rod is commonly occurring failure mode. Tie rod is made up of steel or alloy steel. Current material of tie rod is
replaced with carbon/epoxy composite material. Strength to weight ratio of steel and alloy steel are less as compared with
carbon fiber reinforced composites. Replacement of current material of tie rod with composite material leads to reduction in
weight of vehicles hence increase in economy. Properties of carbon/epoxy composite material are calculated by
micromechanical analysis. Ratio of reinforcing material to matrix material is taken as 70:30. The tie rod is modeled by using
CATIA. Critical buckling load results and total deformation results are obtained using ANSYS. Using filament winding technique,
the composite rods are fabricated. The buckling test is carried out on UTM. Finally, it has been found that carbon composite
material found out to be best replacement for steel rod.
Key Words: Tie rod, Carbon fiber, Buckling, FEA
1. INTRODUCTION
Tie rod get fail due to fluctuating forces during steering and bumping of vehicle. Failure of tie rod may cause instability of
vehicle and leads to an accident. Also, the indications given by the tie rod before failure are very less. Faulty tie rods can
negatively affect a car’s front-end alignment which may result in uneven wear of the inner and outer edge of a vehicle tire.
Moreover, as tie rod ends are Subjected to wear, it can slacken and loose gradually thereby, resulting in failure which may
affect the driver’s ability to steer and control the car. Hence a tie rod should be designed in such a way that it should not get
fail under any circumstances. Effort has been taken for improving performance of tie rod but these efforts either lead to
increase in material cost, manufacturing of component and weight of component. To achieve required strength along with
minimum cost and weight of component, appropriate material and manufacturing technique must be selected. The
composite material has superior mechanical properties. composites are light in weight. Also, one of the best characteristics
of compositematerialisstrengthofcompositecanbeobtained in any specific direction
1.1. PROBLEM STATEMENT
Tie rods is an integral part of vehicle’s steering system. Tie rod get fail due to varying forces and bumping of vehicle during
steering. Tie rod is mostly subjected to compressive stresses. Buckling of tie rod under compressive stresses leads to
uneven tire wear. So, research work is aimed to assess strength and compare performance of carbon fiber reinforced
composite (CFRC) material with existing material of tie rod.
2. LITERATURE REVIEW
Ikpe Aniekan Essienubong et al. have carried out static analysis of tie rod to determine resulting buckling displacement.
First, the load case scenarios were discussed. The maximum and minimum loads and their nature (tensile or compressive)
acting on tie rod were obtained using ADAMS software. The maximum load was of 18.5 KN compressive and 13.6 KN
tensilenature.
Owunna Ikechukwu et al. have investigated tie rod failure in relation with forces which acts on the suspension system. The
various causes of tie rod failure and factors affecting the tie rod performance were investigated McPherson suspension
model was simulated in ADAMS software and maximum tensile and compressive stress values were obtained. Various load
case scenarios were discussed, and corresponding values of loads were obtained using ADAMS software. Reverse Brake
and Bump scenario for compressive load and Cornering and Bump scenario for tensile load were found to have the most
severe impacts on the tie rod during its service life, coupled with other factors such as Fatigue, Corrosion, poor
manufacturing route, misalignment, service loading, though not too severe as the compressive and tensile forces. Rod
manufacturers must pay attention to these forces as well as the material properties during design, as this is one of the ways
to make the tie rod less prone to buckling or fracture and failure.

Raelvim Gonzalez Henriquez et al. have given an overview of filament winding process and the discussed technology to
produce fibre reinforced composites. An overview of process parameters that influence the mechanical properties of
filament wound composites is provided. Moreover, general design and fabrication considerations related to composite
product performance are explored, followed by mechanical testing of filament-wound structures for quality control (QC).
Autar K. Kaw has given a brief introduction of composite materials and their classification. Fibre properties of various
materials such as steel, aluminium, carbon, glass, Kevlar and matrix material such as epoxy, were compared. The
applications of composite materials along with their manufacturing technique were discussed in detail. Micro mechanical
analysis of lamina has carried out to find out to the engineering constants unidirectional/bidirectional lamina in terms of
the stiffnessand compliance parameters of the lamina.
3. METHDOLOGY
The methodology developed is as shown in fig.,
Fig-1: Methdology
4. THEROTICAL ANALYSIS OF TIEROD
The properties of carbon/epoxy composite are derived using theoretical calculations. New carbon/epoxy-steel composite
material properties are obtained, and new materialis created in ANSYS 14.5 material data source. This material is assigned for
the tie rod model. Critical buckling load results are obtained for new material and aluminum alloy and steel.
4.1. Micromechanical analysis
A composite material consists of two or more constituents; thus, the analysisand designofsuchmaterials is differentfrom
thatforconventionalmaterialssuchasmetals.
Here, reinforcing material is taken as Carbon fiber and matrix material is taken as epoxy resin. Carbon fiber is a material
consistingoffibersabout3-15μmindiameterandcomposed mostlyofcarbonatoms.Thecrystalalignmentgivesthefiber high
strength-to-volume ratio. Carbon fibers show high stiffness, high tensile strength, low weight, high chemical resistance,
high temperature tolerance and low thermal expansion. Epoxy resin has high flexibility and low viscosity. Also, it is easily
available.Thereactivityofresincaneasilybe adjusted as per the demands using combination of both resign and hardeners.
Problem Statement
Literature survey
Theoretical analysis of tie rod
Buckling analysis of tie rod
Manufacturing of CFRC tie
rod
Experimental testing and
Validation of result

The approach to analyze the mechanical behavior of composite structures is as follows:
1) Find the average properties of a composite ply from the individual properties of the constituents. Properties include
stiffness, strength, thermal, and moisture expansion coefficients. Note that average properties are derived by considering
the ply to be homogeneous. At this level, one can optimize for the stiffness and strength requirements of a lamina. This is
called the micromechanics of a lamina.
2) Develop the stress–strain relationships for a unidirectional/bidirectional lamina. Loads may be applied along the
principal directions of symmetry of the lamina or offaxis. Also, one develops relationships for stiffness,thermal and moisture
expansion coefficients, and strengths of angle plies. Failure theories of a lamina are based on stresses in the lamina and
strength properties ofa lamina.This iscalled the macromechanics of a lamina.
A structure made of composite materials is generally a laminate structure made of various laminas stacked on each other.
Knowing the macromechanics of a single lamina, one develops the macromechanics of a laminate. Stiffness, strengths, and
thermal and moisture expansion coefficients can be found for the whole laminate. Laminate failure is based on stresses and
application of failure theories to each ply. This knowledge of analysis of composites can then eventually form the basis for
the mechanical design of structures made of composites.
So on the basis of above theory properties of composite material that is CFRC material in this case is obtained as below,
Volume fraction of fibre – 0.7 (70%) Volume fraction of matrix – 0.3 (30%) Volume of composites – 1 (100%) Density of
composite (Þc) is given by
Þc= ÞfVf + ÞmVm … (1)
Young’s modulus in longitudinal direction is given by,
E1 = EfVf + EmVm … (2)
Youngs Modulus in transverse direction is given by, (1/E2) = (Vf / Ef)+ (Vm/Em) … (3)
Major Poisson ratio(µ12) is given by,
µ12 = (µf Vf)+ (µmVm) … (4) Minor poisson ratio is given by,
µ21 = µ12*(E2/ E1) … (5)
So, the important properties of composite based on above equations are enlisted in the table 1.
Table-1: Properties of composite (carbon fiber and epoxy resin)
Sr.
No
Composite Properties Symbol Value unit
1 Young’s Modulus
(Longitudinal direction)
E1
170.3 Gpa
2 Young’s Modulus
(Transverse direction)
E2
9.7 Gpa
3 Major Poison’s ratio µ12 0.3 -
4 Minor Poisson’s ratio µ21 03 -
4.2. BUCKLING ANALYSIS OF TIE ROD
An eigen value buckling analysis is carried out for tie rod. A model of tie rod is created in CATIA V5 and then imported in
ansys. Fine meshing is selected for better accuracy. An eigenvalue buckling analysis predicts the theoretical buckling
strength of an ideal elastic structure. Eigenvalues are values of load at which buckling takes place. An eigenvalue buckling
analysis must be linked to static structural analysis. A static structural analysis determines the displacements, stresses,
strains, and forces in structures. The results calculated by the eigenvalue buckling analysis are buckling load factors that
scaleall of the loads appliedin the static structural analysis.

Buckling analysis of steel material is carried out. Total deformation results and critical buckling load results are obtained.
TotaldeformationresultforsteelisshowninFig.2. The maximum deformation for 1 N force is 4.997 mm
Fig-2: Total deformation result for steel
Fig-3: Critical Buckling Load result for steel
The results calculated by the eigenvalue buckling analysis are buckling load factors that scale all of the loads applied in the
static structural analysis. The load multiplier is 39610. Hence critical buckling load for steel material is 39610 N. The critical
buckling load is shown in fig3.
The combined properties of composite material are obtained by using properties of steel and carbon/epoxy composite. The
combined properties of steel and composite are obtained by averaging method. Buckling analysis of CFRC and steel
composite material is carried out the total deformation results and critical buckling load results are obtained. Total
deformation result for carbon/epoxy and steel composite is shown in Fig.4. The maximum deformation for 1 N force is
5.4022𝑒 −6mm.
Fig-4: Total deformation result for CFRC and steel composite
The Eigen value buckling results for CFRC and steel composite are obtained and are shown in Fig.5. The load multiplier is
36639.HencethecriticalbucklingloadforCFRC and steel composite is 36639 N.

Fig-5: Critical buckling load result for CFRC and steel composite
 Stiffness of Materials
Stiffness is the extent to which an object resists deformation in response to an applied force. Stiffness is nothing but force per
unit deformation.
Mathematically, stiffness is given by,
𝐹 = 𝐾𝑋 … (6)
Where, F = applied force in N X = Deformation in mm
K = Stiffness in N/mm.
The stiffness of steel and composite materials is calculated theoretically.ThestaticdeformationobtainedinANSYS14.5
14.5 is used to obtain stiffness of material.
• Stiffness of steel material –
As discussed in section 4.2 from Fig. 2 the maximum deformation for steel is 4.997 𝑒 −6mm for 1 N force. Hence stiffness of
steel can be obtained using eq. 6 as,
1N = K 4.997 𝑒 −6mm
K = 200.120 KN/mm
Hence stiffness of steel material is 200.12 KN/mm.
• Stiffness of CFRC and steel composite–
As discussed in section 4.2 and from Fig. 4 the maximum deformation for Carbon/Epoxy and steel is 5.4022 𝑒−6mm for 1 N
force.HencestiffnessofCFRCandsteelcompositecan be obtained using eq.3.20 as,
1N = K 5.4022𝑒 −6mm K = 185.109 KN/mm
Hence stiffness of Carbon/Epoxy composite material is
185.109 KN/mm
 Weights of tie rod materials
Weight of material is given by,
𝑊 = 𝜌𝑉 gram
Where, 𝜌 = Density of material, g = Acceleration due to gravity V = Volume of rod =п 𝑅^2 H
R = Radius of rod = 8 mm

H = Height of rod = 200 mm
The weights of steel and composite material are found to be 307 grams and 125 gramsrespectively.
5. MANUFACURING OF CFRC TIE ROD
The manufacturing of CFRC tie rod is done by filament winding process as it has greater fiber orientation control. In filament
winding technique, fiber strands are loosened up and passed constantly to the resin tank. In resin tank, fiber strand are
impregnated totally with the resin.
Presently, these resin impregnated strands are passed onto a turning mandrel. These strands are twisted around the
mandrel in a controlled way and in a particular fiber orientation. The reason for choosing filament winding process is that
filament winding process ensures high degree of uniformity in fiber distribution, orientation, and placement. Fiber can be
oriented in specific direction. A tie rod is subjected to axial forces hence fibers can be oriented in such a way that maximum
strength can be obtained. Theactualrepresentationoffilamentwindingprocessisasshown in the fig.6.
Fig-6: Filament winding of carbon fiber
6. EXPERIMENTAL TESTING
For the validation of numerical result experimental testing is done. The Critical buckling load for new composite material is
obtained experimentally by using computerized universal testing machine MODEL STS 248. The testing was carried out at
Praj laboratories, Pune. Three sample specimens of composite were tested. The testing is carried out by referring standard
procedure.
Fig-7: Experimental setup
7. RESULT AND DISCUSSION
The FEA analysis is carried out to find critical buckling load for steel and composite tie rod. The experimental result for
composite tie rod is obtained totest the accuracy of analysis and experimental result.

Table 2 shows the tabular representation of experimental critical buckling load and compressive strength of sample
Table-2:Criticalbucklingloadandcompressivestrength of samples
Sr.
No. Specimen
Critical
Buckling
load (N)
Compressive
strength
(MPa)
1 Specimen 1 31879.4 158.491
2 Specimen 2 32242 160.294
3 Specimen 3 33780.6 167.943
Averagecritical bucklingloadistakenintoconsiderationfor comparison. The average critical buckling load is 32634 N.
Fig. 8 shows buckling load to weight ratio of steel and composite material. Buckling load to weight ratio is obtained by
dividing critical buckling load carrying capacity by weight of material. The Fig shows buckling load of carbon composite is
much higher relative to weight.
Fig-8: Buckling load to weight ratio for steel and composite material
Fig. 9 shows the stiffness of steel and CFRC material. In section 4.2 stiffness values are calculated. Stiffness of material
indicates resistancetodeformation.FromFig.9steel
Table 3 shows comparison between numerical and experimental value of critical buckling load.
Table-3: Comparison of Numerical and experimental results
Numerical value of
critical
buckling load N
Experimental value
of critical buckling
load N
Percentage
variation
36639 32634 10.93
The numerical value and the experimental value of critical buckling load have percentage variation 10.93. This variation
occurs because we do not consider the micro-voids during analysis of composite material
The critical buckling load for steel and CFRC material is obtained theoretically using software and experimentally by using
UTM.Thecomparisonbasedonstrengthanddensityis shown in Table 4.
Table-4: Numerical Results of critical buckling load for steel and CFRC
Sr.
No
Material
Critical
buckling
load (N)
Density
(Kg /m^3)
1 Steel 39610 7800
2
Carbon / Epoxy
and steel
composite
36639 2900

is having maximum stiffness while carbon fiber composites have nearly same stiffness value as steel. Direct co- relation can
be seen from stiffness and critical buckling load. As stiffness of material increase resistance to deformation increases.
Fig-9: Stiffness of steel and CFRC composite
The experimental and numerical values of critical buckling load are compared. The comparison of results shows that CFRC
material show higher value of strength to weight ratio as compared to steel. As weight of vehicle is directly related to fuel
consumption which in turn directly related to vehicle’s engine efficiency. Thus, by reducing weight we can increase the
efficiency. Also, with the decrease in weight of material, material cost also decreases.
8. CONCLUSION
The design, analysis and fabrication of inner end of tie rod using CFRC material has been done. The failure of tie rod
occurs when it is subjected to compressive and buckling loads. A polymer-based composites material is replacement for
steel alloy tie rod. Filament winding method is used for fabrication. Following conclusions can be drawn based on study: 1)
The FEA predicted result deviates by 10.93% from experimental result. 2) CFRC material shows very close stiffness to steel.
3) More than two times weight reduction can be possible by use of carbon/epoxy composite along with steel without
compromising much strength. 4) The steel tie rodcanbereplaced byCFRCmaterial withoutcompromising strength.
ACKNOWLEDGMENT
I would like to thank to my guide Dr. A. P. Tadmallefor his valuable guidance, support andcontinuousencouragement. Also, I
wouldlike tothank all thestaffmembers, friendsfor their kindful help.
REFERENCES
[1] Essienubong, A. I., Ikechukwu, O., Ebunilo, P. O., and Ikpe, E. E., 2016, “Static Analysis on a Vehicle Tie Rod to Determine
the Resulting Buckling Displacement,” Interna tional Journal of Industrial and Manufacturing Systems Engineering, 4,
pp. 16-24.
[2] Ikechukwu, O., Aniekan, I., Ebunilo, P. O., and Ikpe, I., 2016, “Investigation of a Vehicle Tie Rod Failure in Relation to the
Forces Acting on the Suspension System,” AmericanJournal ofEngineeringResearch,5, pp. 208- 217
[3] A.H. Falah, M.A. Alfares, A.H. Elkholy, Failure investigation of a tie rod end of an automobile steering system, Elsevier,
Engineering Failure Analysis 14, (2007),895– 902.
[4] Robert J. Pascarella, Michelle M. Vogler, Analysis of Tie Rod Separations in Motor Vehicle Crashes, SAE technical paper
series,(2008),1-7.
[5] Wayal, S. U., Deshmukh, S. S., and Katratwar, K., 2017, “Weight Optimization of Tie Rod Using FEM,” International
JournalofInnovationsinEngineeringand Science, 2, pp. 50-53.
[6] Patil, M. A., Chavan, D. S., and Kavade, M. V., 2013, “FEA of Tie Rod of Steering System of Car,” International Journal of
Application or Innovation in Engineering& Management, 2, pp. 2319-4847.

[7] Henriquez, G. R., and Mertiny P., 2017, “Filament Winding Application,” Comprehensive composite materials II, 3, pp.
556-577.
[8] Autor k. kaw, “Introduction to composite material and micromechanical analysis of composite material”in mechanics of
compositematerial,2ndedition.US, pp.1- 51sept. 2006.].

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