Fatigue Analysis of Adsorber - Peak In & Peak Out | Ratcheting | S-N Curve

3D Model with GAD - Peak In
3D Model with GAD - Peak In

Figure 1: 3D Model with GAD – Peak In

1. Executive Summary

Fatigue analysis of the Adsorber under cyclic pressure loading (0.47/0.02 MPa) per ASME VIII Div.2, Part 5. Both Peak In and Peak Out configurations evaluated. All components pass for 27,375 design cycles.

  • Shell, dishends, skirt, bolts: Infinite life
  • Nozzle N01: N ≈ 358K–362K cycles
  • Trunion Weld: damage factor 0.465 (Peak In)
  • Ratcheting: 299 & 304 vs 450 MPa – PASS
  • Hoop stress validated within 0.004%

2. Design Parameters

Parameter Value
Equipment Adsorber EIPL WO-232002
Design Code ASME VIII Div.1
Analysis Code ASME VIII Div.2 Part 5 (2021)
Design Temperature 200°C
Operating Temperature 177°C
Cyclic Pressure 0.47 / 0.02 MPa
Design Cycles 27,375
Material (Shell) SA-516 Gr.70 N
Material (Bolts) SA-193 Gr.B7
Element Type SOLID186 (20-node)
Software ANSYS Mechanical

3. Mesh & Model

Figure 2: Mesh — Peak In (361,130 elements)

Figure 2: Mesh – Peak In (361,130 elements)

Figure 3: Mesh – Peak Out

Metric Target Achieved Status
Aspect Ratio < 5.0 1.1694 PASS
Jacobian > 0.5 0.9996 PASS
Skewness < 0.70 0.4752 PASS
Element Quality > 0.1 0.4797 PASS

4. Boundary Conditions

Figure 4: LC-1 boundary conditions - Peak In

Figure 4: LC-1 boundary conditions – Peak In

Figure 5: Thermal loading - Peak Out

Figure 5: Thermal loading – Peak Out

5. Deformation Results

Figure 6: Total deformation – Peak In

Total deformation - Peak Out

Figure 7: Total deformation – Peak Out

6. Fatigue Results - Peak In

Figure 8: Solution combination stress range - Peak In

Figure 8: Solution combination stress range – Peak In

Component ΔSp Kf Salt N Damage Status
Shell 86.93 1.2 52.16 0.0 PASS
Nozzle A01 102.62 1.7 87.23 799,588 0.034 PASS
Nozzle N01 112.45 1.7 95.58 358,115 0.076 PASS
Trunion Weld 75.28 4.0 150.55 58,844 0.465 PASS
Top Dishend 90.66 1.2 54.39 0.0 PASS
Bottom Dishend 89.51 1.2 53.70 0.0 PASS
Skirt 19.06 1.7 16.20 0.0 PASS
Bolts N A01 24.50 1.2 14.70 0.0 PASS

7. Fatigue Results - Peak Out

Figure 9: Solution combination stress range – Peak Out

Component ΔSp Kf Salt N Damage Status
Shell 93.53 1.2 56.12 0.0 PASS
Nozzle N01 117.02 1.7 99.47 361,729 0.076 PASS
Trunion Weld 78.43 4.0 101.41 324,081 0.084 PASS
Top Dishend 90.50 1.2 54.30 0.0 PASS
Bottom Dishend 91.98 1.2 55.19 0.0 PASS

8. Ratcheting Assessment

Config Snk (MPa) SPS (MPa) Status
Peak In 299.32 450 PASS
Peak Out 303.79 450 PASS

9. Validation

Figure 10: Hoop stress validation

Figure 10: Hoop stress validation

Figure 11: Global equilibrium check

Figure 11: Global equilibrium check

Check Value
Hoop Stress Error 0.004%
Equilibrium Error 0.23%
Mesh Sensitivity 0.003%

10. Lessons Learned

Weld fatigue strength reduction matters most

Trunion Weld Kf=4.0 drives highest damage despite lower stress.

 

Both Peak In & Out must be evaluated

Peak In shows 5x higher trunnion damage than Peak Out.

 

Solution combination captures real fatigue

Only LC1−LC2 stress range drives crack initiation.

11. Conclusion

  • All components pass fatigue for 27,375 cycles
  • Trunion Weld governs: damage = 0.465
  • Ratcheting passes both configurations
  • Equipment safe for full design life

Download the Full Technical Case Study

The full technical report includes:

  • Detailed fatigue calculations using S-N curves and damage factors for all components
  • Stress range evaluation for Peak In and Peak Out configurations
  • Ratcheting assessment results with stress limits comparison
  • Load case combinations and cyclic pressure analysis methodology
  • FEA modeling approach, mesh quality, and boundary conditions
  • Validation checks including hoop stress, equilibrium, and mesh sensitivity
  • ASME Section VIII Division 2 fatigue and ratcheting code references

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