Determination of Effect Angular Poisoning of Legs on the Structural Stability of Pressure Vessel by Using Non-linear Finite Element Analysis (FEA)

DOI : 10.17577/IJERTV2IS3236

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Determination of Effect Angular Poisoning of Legs on the Structural Stability of Pressure Vessel by Using Non-linear Finite Element Analysis (FEA)

Amit M. Patil Dr. R.S Bindu

Mechanical Engg. Department Mechanical Engg. Department

D.Y Patil College of Engineering D.Y Patil College of Engineering

Abstract

The objective of the pressure vessel is to have production of phenol and acetone. Cumene process is an industrial process of producing phenol (C6H5-

OH) and acetone (CH3-CO-CH3) from benzene (C6H6) and propene (C3H6). The term stems from isopropyl benzene or cumene (C6H5-CH (CH3)2), the intermediate material during the process. With the

help of this process two relatively cheap materials, benzene and propene are converted into two more valuable products such as phenol and acetone. For this process other required reactants are oxygen from air and small amounts of a free radical initiator. Most of the worldwide production of phenol and acetone are now based on this method.

The pressure vessel is being designed to implement the cumene process. The process is extremely sensitive to pressure and temperature conditions and requires a lot of control systems to monitor it. These control systems are to be placed below the vessel for effective monitoring. The current range of Pressure Vessels in the market of AZ series come either in skirt support or supported by 8 legs equidistance from each other. However, a custom made pressure vessel has been ordered for the cumene process. The custom made vessel has to have a lot of controls for the cumene process; hence 8 legs are not feasible. Six legs support with a non- symmetric distribution was tried out initially. However the current requirement is to have more floor space.

  1. Introduction

    Type of support used depends on the orientation and pressure of the pressure vessel. Support from the pressure vessel must be capable of withstanding heavy loads from the pressure vessel, wind loads and seismic loads. Pressure on pressure vessel design is not a consideration in designing support. Temperature can be a consideration in designing the support from the

    standpoint of material selection for the different thermal expansion.

  2. Need of Work

    It is observed that although a lot of work has been done in the field of pressure vessel. The current range of Pressure Vessels in the market of AZ series come either in skirt support or supported by 8 legs equidistance from each other. Six legs support with a non- symmetric distribution was tried out initially. However the current requirement is to have more floor space.

    It is decided to improvise on the design and introduce angular supports. It has an advantage of increased floor space to mount the controls.

  3. Objective of Work

    Typically most of the pressure vessel are either skirt or leg supported and observation is that legs are primarily vertical. However in case vertical expansion of the vessel either due to thermal expansion or due to vertical loading the legs are susceptible to buckling.

    Hence, objective of this work is to determine whether creating an angle in the legs in combination with unsymmetrical distribution affects the structural stability of the system.

    Figure 1 Vertical drum on inclined leg support

  4. Methodology

    1. Material Selection

      According to ASME code for manufacturing of pressure vessel number of materials are specified but the selection depends purely upon nature of application. In accordance with number of material selection factors and rules and regulation led down by ASME code specifications material need to be decided. Since this work primarily focus on the analysis of vertical leg supports. Finally end user will decide which material to be used. The material used for this vessel is structural steel and its properties are listed below.

      Table 1

      Sr .

      No.

      Material

      Structural Steel

      1

      Youngs Modulus (Mpa)

      2e5

      2

      Density Kg/ m3

      7850

      3

      Poissons Ratio

      0.3

      4

      Yield Strength (Mpa)

      250

      5

      Tensile Strength (Mpa)

      460

      .

    2. Geometry Modelling

      The vessel geometry modelling has been done in Ansys

      12.01 workbench itself.

        1. Mesh Generation

          Meshing has been done by using the method of Tetrahedron. In Tetrahedron method the component is been divided into small triangle on its surface which gives no of nodes and elements of that component. The meshing has been done by changing the mesh size of the various component of the pressure vesssel. Due to change in the density of the meshing, it results in the variation of the no of nodes and elements of the meshed parts.

          The result of this mesh density change affects the value of the stress and deformation of the component. For fine meshing that is for small mesh size the values of no of nodes and elements are high but as the element size is gradually increased it result in increase in the value of no of nodes and elements. For small variation in mesh size that is of 1E-03 m the values are showing small variation in no of nodes and elements and also it shows the same amount of variation in the values of stress and deformation for the given mesh size. But for large variation in mesh size the values of no of nodes and elements are also vary in large amount.

        2. Boundary Condition

          In case of FEA analysis on has to make sure that the boundary condition applied for particular analysis must be correct or it may cause misleading results.

          The nature of analysis will decide the boundary conditions need to be applied. As in this work the leg supports are more important from analysis point of view and sine pressure vessel is vertically standing on ground the following boundary conditions were applied.

          1 .Wind load acting on the vessel

          1. Internal pressure of the vessel

          2. All the supports need to be fixed to the ground

        3. Structural Analysis

      The Ansys 12.01 workbench will give the results in terms of the maximum deformation as well as the stress subjected by the pressure vessel assembly.

      Here, in this work there will be small increment in the angular positioning of legs by 1 degree upto 30 degree. This increment will result in the considerable amount of deformation as well as stress in the leg supports. The tabular results for stress and deformation for 1 to 30 degree are as shown in Table 2. The nature of this analysis is based upon Section VIII Division 1 for the targeted compliance of the stress values in the pressure vessel assembly.

      Figure 2 3D Model

      Figure 2 Meshing

      Figure 4 Total Deformation

      Figure 3 Boundary Condition

      Figure 5Von Mises Stress

      Table 2 Stress and deformation values for no. of angles

      60 Angle Vs Von Mises Stress

      Von mises Stress (Mpa)

      Von mises Stress (Mpa)

      50

      50

      48.757

      28.709

      Angle

      Von Mises Stress (Mpa)

      Total Deforma tion(mm

      )

      No. of Nodes

      No.of Element s

      1

      25.702

      0.125

      99795

      48693

      2

      0.158

      99635

      48700

      3

      29.127

      0.140

      95532

      46172

      4

      33.312

      0.178

      99909

      48907

      5

      39.280

      0.147

      99514

      48584

      6

      40.827

      0.144

      100505

      49023

      7

      44.336

      0.149

      99807

      48784

      8

      48.757

      0.151

      100373

      48982

      9

      48.188

      0.155

      99928

      48816

      10

      47.196

      0.158

      101329

      49619

      11

      52.103

      0.165

      100512

      49345

      12

      54.729

      0.172

      101560

      49783

      13

      58.183

      0.166

      100882

      49291

      14

      65.696

      0.118

      102215

      50113

      15

      49.538

      0.196

      101291

      49571

      16

      49.282

      0.202

      101728

      49712

      17

      54.798

      0.210

      101942

      49847

      18

      49.087

      0.217

      101902

      49750

      19

      63.028

      0.224

      102404

      50078

      20

      59.741

      0.230

      103396

      50628

      21

      70.871

      0.237

      102390

      50134

      22

      74.037

      0.243

      103947

      51031

      23

      80.392

      0.250

      103571

      50714

      24

      82.293

      0.257

      103721

      50681

      25

      84.569

      0.264

      104716

      51251

      26

      88.839

      0.271

      104830

      51303

      27

      92.682

      0.278

      105381

      51571

      28

      10.95

      0.285

      105956

      51724

      29

      105.38

      0.293

      107247

      52557

      30

      107.74

      0.301

      107039

      52327

      Angle

      Von Mises Stress (Mpa)

      Total Deforma tion(mm

      )

      No. of Nodes

      No.of Element s

      1

      25.702

      0.125

      99795

      48693

      2

      28.709

      0.158

      99635

      48700

      3

      29.127

      0.140

      95532

      46172

      4

      33.312

      0.178

      99909

      48907

      5

      39.280

      0.147

      99514

      48584

      6

      40.827

      0.144

      100505

      49023

      7

      44.336

      0.149

      99807

      48784

      8

      48.757

      0.151

      100373

      48982

      9

      48.188

      0.155

      99928

      48816

      10

      47.196

      0.158

      101329

      49619

      11

      52.103

      0.165

      100512

      49345

      12

      54.729

      0.172

      101560

      49783

      13

      58.183

      0.166

      100882

      49291

      14

      65.696

      0.118

      102215

      50113

      15

      49.538

      0.196

      101291

      49571

      16

      49.282

      0.202

      101728

      49712

      17

      54.798

      0.210

      101942

      49847

      18

      49.087

      0.217

      101902

      49750

      19

      63.028

      0.224

      102404

      50078

      20

      59.741

      0.230

      103396

      50628

      21

      70.871

      0.237

      102390

      50134

      22

      74.037

      0.243

      103947

      51031

      23

      80.392

      0.250

      103571

      50714

      24

      82.293

      0.257

      103721

      50681

      25

      84.569

      0.264

      104716

      51251

      26

      88.839

      0.271

      104830

      51303

      27

      92.682

      0.278

      105381

      51571

      28

      10.95

      0.285

      105956

      51724

      29

      105.38

      0.293

      107247

      52557

      30

      107.74

      0.301

      107039

      52327

      44.336

      40.827

      49.188

      47.196

      40 33.312

      29.

      28.709 127

      30

      20 25.702

      10

      0

      39.28

      0 5 10 15

      Angle

      0.148

      0.148

      0.158

      0.155

      0.158

      0.155

      0.147 0.149

      0.151

      0.144

      0.147 0.149

      0.151

      0.144

      Total Deformation (mm)

      Total Deformation (mm)

      Figure 6 Angle Vs Von Mises Stress

      Angle Vs Total Deformation

      0.200

      0.158

      Angle Vs Total Deformation

      0.200

      0.158

      0.150

      0.140

      0.150

      0.140

      0.100 0.125

      0.050

      0.000

      0

      0.100 0.125

      0.050

      0.000

      0

      5

      5

      Angle 10

      Angle 10

      15

      15

      Figure 7 Angle Vs Total Deformation

      .

  5. Conclusion

    The table 2 shows the various values of stress and deformation irrespective of the change in the angle. We have plotted 2 graphs as shown in Figure 6 Angle Vs Von Mises Stress and Figure7Angle Vs Total Deformation for a instance both graph are plotted up to first 10 results.

    The first graph will lead the information that with corresponding increase in the angle the value of the stress in the vessel is also having gradual increase.

    Similarly, for corresponding change in the angle deformation is also increasing. On the other hand if we se e that Table 2 will show that at 30 degree the Von Mises Stress around the leg support is 107.74 Mpa and which is maximum but less than the yield strength and tensile strength resulting into safe design.

  6. References

  1. K.Magnucki, P.Stasiewicz, W. Szyc, Flexible saddle support of a horizontal cylindrical pressure vessel, International Journal of Pressure Vessels and Piping, Vol. 80, pp. 205-210, 2003.

  2. Shafique M.A. Khan, Stress distribution in horizontal pressure vessel and the saddle supports, International Journal of Pressure Vessels and Piping, Vol. 87, pp. 239- 244, 2010.

  3. Troy Alvin Smith, Analysis of axisymmetric shell structures under axisymmetric loading by the exibility method, Journal of Sound and Vibration, Vol. 318, pp. 428-460, 2008.

  4. E. Gutman, J. Haddad, R. Bergman, Stability of thin walled high-pressure vessels subjected to uniform corrosion, International Journal of Pressure Vessels and Piping, Vol. 38, pp. 43-52, 2000.

  5. Prof. R. M. Tayade, Mr. Vinay Patil, Imran M. Jamadar,

    Structural Analysis of Inclined Pressure vessel Using FEM, International Journal of Engineering Research &Technology (IJERT), ISSN: 2278-0181, 2012.

  6. L. P. Zick, Stresses in large horizontal cylindrical vessels pressure vessels on two saddle supports, The welding journal research supplement, pp.959-970, 1951.

    International Journal of Engineering Research & Technology (IJERT)

    ISSN: 2278-0181

    Vol. 2 Issue 3, March – 2013

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