Design and Analysis of a Connecting Rod

DOI : 10.17577/IJERTV5IS100142

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Design and Analysis of a Connecting Rod

Sebastian Antony, Arjun A., Shinos T. K

    1. ech. Mechanical Dept.

      Muthoot Institute of Technology and Science Ernakulam, India

      Anoop P.

      Assistant Professor, Mechanical Dept.

      Muthoot Institute of Technology and Science Ernakulam, India

      Abstract The main function of a connecting rod is to convert linear motion of piston to rotary motion of crank. It is the main component of an internal combustion (IC) engine and is the most heavily stressed part in the engine. During its operation various stresses are acting on connecting rod. The influence of compressive stress is more in connecting rod due to gas pressure and whipping stress.

      The objective of this study is to carry out a FEA analysis of a connecting rod and obtain its stress distribution on application of the force.

      Geometry of connecting rod used for FEA, its generation, simplifications and accuracy is done by using Catia. Mesh generation, the load application, particularly the distribution at the contact area, factors that decide application of the restraints and validation of the FEA model are also discussed. FEM was used to determine structural behavior under static load condition (static FEA).

      KeywordsConnecting Rod, Catia, Ansys, FEA

      1. INTRODUCTION

        In modern automotive internal combustion engines, the connecting rods are most usually made of steel for production engines, but can be made of aluminium (for lightness and the ability to absorb high impact at the expense of durability) or titanium (for a combination of strength and lightness at the expense of affordability) for high performance engines. They are not rigidly fixed at either end, hence the angle between the connecting rod and the piston changes as the rod moves up and down and rotates around the crankshaft. Connecting rods are manufactured by means of forging.

        Being one of the most integral parts in an engines design, the connecting rod must be able to withstand tremendous loads and transmit a great deal of power. In a reciprocating piston engines, connecting rod connects the piston to the crank or crankshaft. Together with the crank, they form a simple mechanism that converts reciprocating motion into rotating motion.

        As the connecting rod is rigid, it may transmit either a push or a pull and so the rod may rotate the crank through both halves of a revolution, i.e. piston pushing and piston pulling.

        The small end is attatched to the piston pin and the big end connects to the bearing journal on the crank. Typically there is a pinhole bored through the bearing and the big end of the connecting rod so that pressurized lubricating motor oil squirts out onto the thrust side of the cylinder wall to lubricate the travel of the pistons and piston rings.

      2. FINITE ELEMENT ANALYSIS

        1. Design

          The connecting rod is designed using CATIA V5 6R 2014 according to the specifications given below.

          Parameter

          Value

          Length of connecting rod

          150

          Outer diameter of big end

          56

          Inner diameter of big end

          48

          Outer diameter of small end

          32

          Inner diameter of small end

          24

          Table 1: Dimensions of Connecting Rod

          Fig 1: Catia Model of Connecting Rod

        2. Meshing

          The connecting rod model is imported to the ANSYS (mechanical APDL 14.5) by converting the Catia file into .anf extension file format. The element type selected is solid185. After successful import of model material property is defined. The materials and their properties used and necessary for the analysis is given in table 2.

          Material

          Youngs modulus (GPa)

          Poissons ratio

          Density (Kg/mm3)

          Steel

          200

          .303

          8050

          Aluminium

          69

          .334

          2700

          Table 2: Material Properties

          After defining the element type and material property, meshing is done. Meshing is probably the most important part in analysis. Meshing means to create a mesh of some grid- points called 'nodes'. It's done with a variety of tools & options available in the software. The results are calculated by solving the relevant governing equations numerically at each of the nodes of the mesh. For the design under consideration, finite element mesh is generated using tetrahedral mesh type taking fine size to 1mm and minimum edge length as 0.1mm with 50730 nodes.

          Fig 2: Meshed Model Of Connecting Rod

        3. Load Analysis

          1. Compressive Loading:

            Crank End: p = 37.66 MPa Piston pin End: p = 69.98 MPa

          2. Tensile Loading:

        Crank End: p = 41.5 MPa Piston pin End: p = 77.17 MPa

        Since the analysis is linear and elastic, for static analysis the stress, displacement and strain are proportional to the magnitude of the load. Therefore, the result obtained from FEA is applied to several elastic load carries in a proportional manner.

        1. Compression at Bigger end

          For the analysis of connecting rod, a compressive force of magnitude 37.66MPa is applied on the bigger end, keeping the smaller end fixed.

          Fig.3: Total Deformation of Steel

          Fig.4: Total Deformation of Aluminium

          Fig.5: Von-Mises Stress of Steel

          Fig.6: Von Mises Stress of Aluminium

        2. Tension at bigger end

          A tensile force of magnitude 41.15 MPa is applied at the bigger end while keeping the smaller end remain fixed.

          Fig.7: Total Deformation of Steel

          Fig.8: Total Deformation of Aluminium

          Fig.9: Von-Mises Stress of Steel

          Fig.10: Von Mises Stress of Aluminium

        3. Compression in Smaller End

          A compressive load of magnitude 69.98 MPa is applied at the smaller end keeping the bigger end fixed.

          Fig.11: Total Deformation of Steel

          Fig.12: Total Deformation of Aluminium

          Fig.13: Von-Mises Stress of Steel

          Fig.14: Von Mises Stress of Aluminium

        4. Tension in Smaller End

        A tensile force of 77.17 MPa is applied at the smaller end while keeping the bigger end remains fixed.

        Fig.15: Total Deformation of Steel

        Fig.16: Total Deformation of Aluminium

        Fig.17: Von-Mises Stress of Steel

        Fig.18: Von Mises Stress of Aluminium

      3. RESULTS AND DISCUSSIONS

        Method loading

        of

        Load applied (MPa)

        Maximum displacement (mm)

        Maximum stress (N/mm2)

        Compressive bigger end

        at

        41.15

        0.012

        2490.87

        Tensile at bigger end

        37.66

        0.007

        1605.51

        Compressive small end

        at

        77.17

        0.005

        2044.90

        Tensile smaller end

        at

        69.98

        0.003

        1267.33

        Method loading

        of

        Load applied (MPa)

        Maximum displacement (mm)

        Maximum stress (N/mm2)

        Compressive bigger end

        at

        41.15

        0.012

        2490.87

        Tensile at bigger end

        37.66

        0.007

        1605.51

        Compressive small end

        at

        77.17

        0.005

        2044.90

        Tensile smaller end

        at

        69.98

        0.003

        1267.33

        Material: Steel

        Method loading

        of

        Load applied (MPa )

        Maximum displacement (mm)

        Maximum stress (N/mm2)

        Compressive bigger end

        at

        41.15

        0.055

        3611.37

        Tensile at bigger end

        37.66

        0.034

        2655.57

        Compressive small end

        at

        77.17

        0.016

        1999.21

        Tensile smaller end

        at

        69.98

        0.008

        1177.86

        Method loading

        of

        Load applied (MPa )

        Maximum displacement (mm)

        Maximum stress (N/mm2)

        Compressive bigger end

        at

        41.15

        0.055

        3611.37

        Tensile at bigger end

        37.66

        0.034

        2655.57

        Compressive small end

        at

        77.17

        0.016

        1999.21

        Tensile smaller end

        at

        69.98

        0.008

        1177.86

        Material: Aluminium

        Comparison of von mises stress variation for the two materials are as shown below,

        4000

        3500

        3000

        maximum 2500

        Buckling and bending stresses, non symmetric shape of connecting rod, Flash and bolt holes was eliminated while analysis. We could conclude that the influence of compressive stress is more in connecting rod due to gas pressure and whipping stress as shown. The piston region suffers tensile stress due to inertia loads. The more stressed part of the rod is being shown using von misses stress plot.

      4. CONCLUSION

It was observed that connecting Rod made up of Aluminium has higher intensity of stress induced as compared to connecting Rod made up of Steel. Also there is a great opportunity to improve the design. Hence steel is a better choice for connecting rods.

REFERENCE

  1. Hippoliti, R., 1993, FEM method for design and optimization of connecting rods for small two-stroke engines, Small Engine Technology Conference, pp. 217-231.

  2. Serag, S., Sevien, L., Sheha, G., and El-Beshtawi, I., 1989, Optimal design of the connecting-rod, Modelling, Simulation and Control, B, AMSE Press, Vol. 24, No. 3, pp.49-63.

  3. Mukesh Kumar, Veerendra Kumar Finite Element Analysis of I.C Engine Connecting Rod: A Review,International Journal Of Engineering Sciences & Research Technology July, 2014

  4. Kuldeep B, Arun L.R, Mohammed Faheem Analysis and optimization of Connecting rod using Alfasic Composites,International Journal of Innovative Research in Science, Engineering and Technology;Vol. 2,

    Issue 6, June 2013

  5. Abhinavgautam, K Priya Ajit Static Stress Analysis of Connecting Rod Using FEA Approach, Journal of Mechanical and Civil Engineering (IOSR-JMCE) Volume 10, Issue 1 (Nov. – Dec. 2013)

stress in N/mm2

steel

2000

1500

1000

500

0

compressive

aluminium

load type

Graph 1: Load applied at The Bigger End

2500

maximum stress in N/mm2

steel

2000

1500

1000

500

0

aluminium

compressive tensile

load type

Graph 2: Load applied at smaller End

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