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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 07 Issue: 03 | Mar 2020 www.irjet.net p-ISSN: 2395-0072
© 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 3496
Feasibility Analysis and Structural evaluation of Connecting rod.
Balasaheb Vikhe1, Sagar Walhekar2
1Balasaheb Vikhe, Dept. of Mechanical Engineering, SVIT Nashik, Maharashtra, India.
2Sagar Walhekar, Dept. of Mechanical Engineering, SVIT Nashik, Maharashtra, India.
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - This paper contain to check feasibility of
process changed from forging to casting and Structural
evaluation of connecting rod with Aluminium alloy(Al6063-
T6) material. The main objective finding out effective design
of connecting rod with minimum cost and weight.
Conventionally material used for connecting rod is stainless
steel through the forging process, as this method provides
low productivity and higher productioncost.The3Dmodelis
prepared by using Pro-E creo4.0 and discretization is
prepared by using Hypermesh while FEM is solved by using
Optistruct Hypermesh13.0.
Key Words—Connecting rod, CAD, FEA, Static analysis,
Modal Analysis
1. INTRODUCTION
The Connecting rod are used generally used in all IC
engines acting as an integral part between the piston
and crankshaft. It is transfers motion from piston to
crankshaft and convert the piston linear motion to
crankshaft rotary motion. While connecting rod small
end is connected to piston and bigger end is connected
to the crankshaft.
StainlesssteelConnectingrodsgenerallymanufacturing
by Forging process. Disadvantages of using steel is that
the material is extremely heavy, Costly, manufacturing
process time consuming, higher production cost which
consumes more power.
There are two forces acting on connecting rod are
buckling load due to gas pressure and lateral bending
due toinertiaforces.Connectingrodmustbewithstand
a cyclic loading during high compressive loads due to
combustion and high tensile loads due to inertia.
A connecting rod canbeoftwotypesH-beamorI-beam
or a combination of both depending on application.
2. METHODOLOGY
The objectives involved are:-
2.1 CAD Modeling
2.2 Finite Element Meshing
2.3 Boundary Conditions
2.1 CAD Modeling
The Fig.1 shows representation of Connecting rod. The
CAD Model of I section connecting rod specification is
Length-100mm Piston end dia-14mm, Crankshaft end
dia- 20mm and thickness 10mm.
Fig.-1: Schematic Diagram of Connecting rod
2.2 Finite Element Meshing
The cad data in .stp format is imported in Hypermesh
for the preparation of FE model. Then geometry
cleanup was done byusing options like‘geom.Cleanup’
and ‘defeature’ to modify the geometry data and
prepapre it for meshing operation. Mesh model is
prepared by using Hypermesh 13.0. 8-node Hex 3D
solid elements are used to model of Connecting rod.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 07 Issue: 03 | Mar 2020 www.irjet.net p-ISSN: 2395-0072
© 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 3497
Fig.-2: FEM Model
The element size selected for meshing is 2mm.
Connecting rod model is meshed with about 10713
nodes 8176 elements.
2.3 Loading Conditions
Connecting rod small end is connected to piston and
bigger end is connected to the crankshaft. There are
two forces acting on connecting rod are buckling load
due to gas pressure and lateral bending due to inertia
forces. Connecting rod must be withstand a cyclic
loading during high compressive loads due to
combustion and high tensile loads due to inertia.
The following loads on Connecting rod-:
1) Tensile loading
2)Compressive loading
Fig.-3: Compressive loading Fig.-4: Tensile loading
3. RESULTS AND DISCUSSION
All machine component analysis, a component must be
designed such that the stresses observing during
operation will not exceed material limits. The material
limits are determined by material properties andsome
known deformation theories. Analysis has to conclude
whether the component is safe or fail comparing the
max stress value with yield or ultimate stress.
FEA analysis is to find out the total amount of stresses
and displacement, Modal Natural frequencies, Mode
shapes of Connecting rod.
3.1 Static Analysis Results
Non-Linear Static analysis used to determine the
displacements,stresses,strainsandforcesinstructures
or components cause by static loads. The solver used
for analysis Optistruct Hypermesh.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 07 Issue: 03 | Mar 2020 www.irjet.net p-ISSN: 2395-0072
© 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 3498
3.1.1 Tensile loading
Fig.-5: Tensile loading Contour plot
Results:-
1. Maximum Displacement = 0.15mm.
2. Max. Principal stress = 187MPa.
3.1.2 Compressive loading
Fig.-6: Compressive loading Contour plot
Results:-
1. Maximum Displacement = 0.15mm.
2. Max. Principal stress = 122MPa.
4. CONCLUSIONS
TheMax.PrincipalstressesobservedonConnectingrod
during Tensile andCompressiveloadingislessthanthe
yield strength of material hence, connectingrod design
is safe against load.
REFERENCES
[1] Nitin S Gokhale. “Practical Finite Element Analysis.”
(2008).
[2] V. B. Bhandari. “ Design of Machine Element,”

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IRJET - Feasibility Analysis and Structural Evaluation of Connecting ROD

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 03 | Mar 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 3496 Feasibility Analysis and Structural evaluation of Connecting rod. Balasaheb Vikhe1, Sagar Walhekar2 1Balasaheb Vikhe, Dept. of Mechanical Engineering, SVIT Nashik, Maharashtra, India. 2Sagar Walhekar, Dept. of Mechanical Engineering, SVIT Nashik, Maharashtra, India. ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - This paper contain to check feasibility of process changed from forging to casting and Structural evaluation of connecting rod with Aluminium alloy(Al6063- T6) material. The main objective finding out effective design of connecting rod with minimum cost and weight. Conventionally material used for connecting rod is stainless steel through the forging process, as this method provides low productivity and higher productioncost.The3Dmodelis prepared by using Pro-E creo4.0 and discretization is prepared by using Hypermesh while FEM is solved by using Optistruct Hypermesh13.0. Key Words—Connecting rod, CAD, FEA, Static analysis, Modal Analysis 1. INTRODUCTION The Connecting rod are used generally used in all IC engines acting as an integral part between the piston and crankshaft. It is transfers motion from piston to crankshaft and convert the piston linear motion to crankshaft rotary motion. While connecting rod small end is connected to piston and bigger end is connected to the crankshaft. StainlesssteelConnectingrodsgenerallymanufacturing by Forging process. Disadvantages of using steel is that the material is extremely heavy, Costly, manufacturing process time consuming, higher production cost which consumes more power. There are two forces acting on connecting rod are buckling load due to gas pressure and lateral bending due toinertiaforces.Connectingrodmustbewithstand a cyclic loading during high compressive loads due to combustion and high tensile loads due to inertia. A connecting rod canbeoftwotypesH-beamorI-beam or a combination of both depending on application. 2. METHODOLOGY The objectives involved are:- 2.1 CAD Modeling 2.2 Finite Element Meshing 2.3 Boundary Conditions 2.1 CAD Modeling The Fig.1 shows representation of Connecting rod. The CAD Model of I section connecting rod specification is Length-100mm Piston end dia-14mm, Crankshaft end dia- 20mm and thickness 10mm. Fig.-1: Schematic Diagram of Connecting rod 2.2 Finite Element Meshing The cad data in .stp format is imported in Hypermesh for the preparation of FE model. Then geometry cleanup was done byusing options like‘geom.Cleanup’ and ‘defeature’ to modify the geometry data and prepapre it for meshing operation. Mesh model is prepared by using Hypermesh 13.0. 8-node Hex 3D solid elements are used to model of Connecting rod.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 03 | Mar 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 3497 Fig.-2: FEM Model The element size selected for meshing is 2mm. Connecting rod model is meshed with about 10713 nodes 8176 elements. 2.3 Loading Conditions Connecting rod small end is connected to piston and bigger end is connected to the crankshaft. There are two forces acting on connecting rod are buckling load due to gas pressure and lateral bending due to inertia forces. Connecting rod must be withstand a cyclic loading during high compressive loads due to combustion and high tensile loads due to inertia. The following loads on Connecting rod-: 1) Tensile loading 2)Compressive loading Fig.-3: Compressive loading Fig.-4: Tensile loading 3. RESULTS AND DISCUSSION All machine component analysis, a component must be designed such that the stresses observing during operation will not exceed material limits. The material limits are determined by material properties andsome known deformation theories. Analysis has to conclude whether the component is safe or fail comparing the max stress value with yield or ultimate stress. FEA analysis is to find out the total amount of stresses and displacement, Modal Natural frequencies, Mode shapes of Connecting rod. 3.1 Static Analysis Results Non-Linear Static analysis used to determine the displacements,stresses,strainsandforcesinstructures or components cause by static loads. The solver used for analysis Optistruct Hypermesh.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 07 Issue: 03 | Mar 2020 www.irjet.net p-ISSN: 2395-0072 © 2020, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 3498 3.1.1 Tensile loading Fig.-5: Tensile loading Contour plot Results:- 1. Maximum Displacement = 0.15mm. 2. Max. Principal stress = 187MPa. 3.1.2 Compressive loading Fig.-6: Compressive loading Contour plot Results:- 1. Maximum Displacement = 0.15mm. 2. Max. Principal stress = 122MPa. 4. CONCLUSIONS TheMax.PrincipalstressesobservedonConnectingrod during Tensile andCompressiveloadingislessthanthe yield strength of material hence, connectingrod design is safe against load. REFERENCES [1] Nitin S Gokhale. “Practical Finite Element Analysis.” (2008). [2] V. B. Bhandari. “ Design of Machine Element,”