Finite Element Analysis of a Diesel Generator Cylinder

DOI : 10.17577/IJERTV3IS030345

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Finite Element Analysis of a Diesel Generator Cylinder

Satya Thrinadh Balla1, Panchumarthy Phani Kumar2

1 4th Sem., M.Tech-CAD/CAM, Dept. of Mechanical Engg., SITE, Tadepalligudem, Andhra Pradesh, India.

2 Associate Professor, Dept. of Mechanical Engg., SITE, Tadepalligudem, Andhra Pradesh, India

Abstract This paper analyses a catastrophic cylinder failure of a four stroke 14v diesel generator of an electrical power plant when running to nominal speed of 600rpm.the rated power of the engine was 7.5MW and before failure had accumulated 80,000h in service operating mainly of full load. as result the piston and liner of cylinder were broken, the crank case main crank shaft bearings next to this cylinder were also damaged the mechanical properties of cylinder (aluminum alloy) including tensile properties and brinel hardness were evaluated . no signs of fatigue failure were identify in piston .a finite element model of the cylinder has shown that the most heavy loaded areas match the fractured zones

  1. INTRODUCTION

    Internal combustion engine failures due to cylinder anomalies are very destructive and hamper the failure diagnosis .once that failure has taken place ,usually liner, piston ,connecting rod and some times engine head are seriously damaged most failure of these elements are due to fatigue combined with another issue. Liner failure due to fatigue aggravated in wet type design by corrosion and hence stress corrosion and corrosion fatigue .another example is cylinder sleeve failure due to stress concentration cavities which appear during the manufacturing process, which contributes to reducing the resistance of the component, creating crack nucleation spots

    .in this case, bad cooling conditions during manufacturing could produce internal differences in the microstructer,providing another failure mechanism due to material fatigue failure in connecting rods to grooves at their small end, which are related to machining or assembling process, are also reported as crack origins bad design of the thread root radius, which produces stress concentration ,or forming laps which frequently occurs due to symmetrical metal flow during forming ,also contribute to accelerating connecting rod fatigue failure, in the case of piston failure, the faults are usually present in different piston parts :crown, ring grooves pin holes and skirt. The damage mechanism can have different origins but are mainly related to wear, high temperature and thermal, thermal mechanical fatigue piston pin fatigue failure due to a defective

    piston-pin carburization, which decrease the fatigue strength a lot, has also been highlighted as a possible failure cause all these failure make it highly advisable to develop a methodology for cylinder failure diagnosis. in this work root cause analysis protocol is followed to analyze the cylinder failure of a 14v diesel generator of 7.5MW nominal power running at 600 rpm

  2. DESCRIPTION

    In this work static and thermal analysis of the diesel generator cylinder is carried out. in the static analysis, the parameters such as the internal pressure .in the thermal analysis uniform temperature load is applied .in the designe,we need to design the generator cylinder in such way that it should withstand for pressure as well as temperature load conditions. both thickness and the material are studied for this designe.the present generator cylinders that being used in the four cylinder engines is having lower efficiency so the

  3. MODEL DEVELOPMENT USING CATIA

    Material Properties aluminum alloy

    The material used to manufacture above Diesel generator cylinder is aluminum alloy and its properties used for design and analysismodified designed engine cylinder is somewhat more efficient.

    Table 1: Material Properties

    Material

    Aluminum alloy

    Youngs Modulus

    7 x 104MPa

    Poisons Ratio

    0.34

    Thermal expansion

    33×10-6

    Density

    2.7 x 10-6Kg/mm3

    A. MODELLING AND MESHING

    The chosen problem is considered as 3-D solid model .with the dimensional parameters the structure is model in cattie v5 modeling software as shown in fig.1.the model meshed for further analysis using a meshing package hyper mesh 10 with hex mesh .the model consists of 33440 elements. Fig.2.shows the solid 45 element considered for meshing .fee model of the engine cylinder is shown in fig .3.appropriate boundary conditions are incorporated in the analysis. the solid 45 is defined by ten nodes having three degrees of freedom (UX

    UY and UZ)at each node translation in the nodal x,y and z directions .the element has Plasticity ,Creep Swelling, elasticity, Stress stiffing Large deflection, large strain, Adaptive descent Initial stress import capabilities.

    Fig.1 Solid model of diesel generator cylinder

    Fig 2: Finite Element model with boundary conditions diesel generator cylinder.

    Table 1: Mesh is created in Hyper mesh with following quality parameters

    Aspect Ratio

    4

    Length

    5

    Min. angle of hex

    40

    Max. angle of hex

    150

    Fig 3. Element solid-45

  4. DIESEL GENARATOR CYLINDER

    1. Static Analysis

      Static analysis was carried out to know the strength of the generator cylinder by applying the internal pressure

    2. Thermal Analysis

    Thermal analysis was carried out to know the thermal stress of the generator cylinder by applying uniform temperature.

  5. RESULTS & DISCUSSION

    1. Static Analysis:

      Static Analysis of Diesel generator cylinder made up with Aluminum alloy is performed. Displacements in X, Y and Z directions are shown in Fig.4, Fig.5 and Fig.6 respectively.Fig.7 shows stress in X direction. Stress in Y direction is shown in Fig 8. Fig.9 shows stress in Z direction and vanishes stress of the diesel generator cylinder shown in Fig.10.

      Table 2: Static Analysis of aluminum alloy

      Name

      Results as per Analysis

      Allowable stresses and deflection

      from the test results

      Reference figure

      Displacement in

      X-direction, mm

      0.141186

      7

      4

      Displacement in

      Y-direction, mm

      0.667215

      7

      5

      Displacement in

      Z-direction, mm

      0.667215

      7

      6

      Stress in X-

      direction, MPa

      172.643

      237

      7

      Stress in Y-

      direction, MPa

      245.236

      237

      8

      Stress in Z-

      direction, MPa

      245.236

      237

      9

      Von mises stress, MPa

      232.242

      237

      10

      Fig.4 Displacement in y-direction

      Fig.5 Displacement in x-direction

      Fig.6 Displacement in z-direction

      Fig.7 Stress in x-direction

      Fig.8 Stress in y-direction

      Fig.9 Stress in z-direction

      Fig.10 Vonmises stress

      Name

      Results as per Analysis

      Allwable stresses and deflection from the test results

      Reference figure

      Displacement in X-direction, mm

      0.24267

      7

      11

      Displacement in

      Y-direction, mm

      0.37182

      7

      12

      Displacement in

      Z-direction, mm

      0.37182

      7

      13

      Stress in X- direction, MPa

      674.414

      710

      14

      Stress in Y-

      direction, MPa

      589.621

      710

      15

      Stress in Z-

      direction, MPa

      589.621

      710

      16

      Von mises stress,

      MPa

      517.483

      710

      17

      Table 3: Thermal Analysis of Aluminum alloy

      Fig.11 Displacement in x-direction

      Fig.12 Displacement in y-direction

      Fig.13 Displacement in z-direction

      Fig. 14: Stress in x direction

      Fig.15 Stress in y-direction

      Fig.16: Stress in Z direction

      Fig.17 Vonmises stress

  6. CONCLUSION:

The following conclusions are drawn from the present work.

    1. The maximum deflection induced 0.66721 mm under 14 MPa loads which is within the allowable limits i.e.

      < 7mm.

    2. The maximum stress induced is 232.242 MPa which is less than allowable limits of 237 MPa. Hence the factor of safety is 1.0204.

    3. The maximum deflection induced 0.37182 mm under uniform temperature of 1400C load which is within the allowable limits i.e. < 7mm.

    4. The maximum stress induced is 517.483MPa which is less than allowable limits of 700 MPa. Hence the factor of safety is 1.352.

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