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FEA Projects

SimFirst, an engineering consulting firm, was founded in 2018 to provide quality solutions in the Engineering and CAE fields.


Nuclear Applications

Problem Definition

Seismic analysis requested to check the conformance of valve as per ASME BPVC-III Rules for the construction of Nuclear Facilities components Division 1 – Subsection NC Class 2 Components.

Challenges

Seismic analysis, drafting standard format report

Conclusions

The spring loaded safety valve DS112 qualifies seismic evaluation requirement as per ASME BPVC III, Division 1-NC

CAD Model
Loading Conditions
Stress Linearization

Problem Definition

To check and optimize the strength of major parts of Hydraulic Test Bench for tension, compression & buckling condition.

Challenges

Identifying Loading & Boundary conditions for assembly in neutral position.

Conclusions
  1. For tension & compression loading, the equivalent von-Mises stress for all parts are below yield strength.
  2. For buckling condition, design load factor from ANSYS (Load Multiplier) is 12.
CAD Model
Total Deformation
Loading & Boundary Conditions
Result Plot
Defense Applications

Problem Definition

To find out the strength and integrity of pressure regulator valve assembly for shock in all three directions X, Y & Z.

Challenges

Shock analysis

Conclusions

Shock Analysis of valve in Longitudinal X, Horizontal Y and Vertical Z direction

  1. All parts have stresses below yield strength.
CAD Model
Loading Conditions – Shock Profile
Mode - 1
Equivalent Stress

Problem Definition

To find out the strength and integrity of pressure regulator valve assembly for Random Vibration in all three directions X, Y & Z.

Challenges

Random vibration profile

Conclusions
  1. Since total damage in valve for all three directions X, Y & Z for 2 hours is less than 1. Hence the valve assembly is safe for random vibration.
  2. Random Vibration – X, Y & Z Direction All parts have equivalent stress (3 sigma) less than yield strength.
CAD Model
Loading Conditions – Random Vibration
Mode - 1
Fatigue Damage for 2 hours
Equivalent Stress
Oil & Gas Applications

Problem Definition

Optimization of Electrical Actuator Worm Gear Housing Assembly for applied torque.

Challenges

Solving actual loading condition & splitting forces on various parts.

Conclusions

Shock Analysis of valve in Longitudinal X, Horizontal Y and Vertical Z direction

  1. The total deformation of housing and cover is slightly increased but it is within acceptable range.
  2. The total weight reduction in existing assembly is 5.88 kg based on stress limits in housing & cover.
CAD Model
Optimization Results
Loading & Boundary Conditions
Optimized Regions Housing
Other Projects - Valve Analysis
  1. 24” ANSI 600 Ball Valve Testing Analysis as per ASME
    • Evaluate Body & Adaptor for hydro test as per ASME BPVC.VIII.2-2017 & external axial load & bending moment
    • To identify strain gauging locations on the assembly.
  2. Safety valve Pressure Integrity Analysis (CRN)
    • Stress evaluation of safety valve model 900 as per ASME guidelines for CRN (Canadian Registration Number) certification.
  3. 6” ANSI 600 Dual Chamber Senior Orifice Fitting ASME Analysis
    • Evaluation of orifice fitting as per ASME BPVC.VIII.2-2017 Part 5 at maximum allowable working pressure P (1500 PSI) and working temperature between (-20 to 100F) for Protection Against Plastic Collapse and Protection Against Local Failure.
  4. Seismic analysis of 30”x30” ANSI 300 Ball Valve as per Euro Code EN 1998-1

    To evaluate 30”x30” ANSI 300 Ball Valve assembly as per Euro Code EN 1998-1 for seismic requirement

Automotive

Problem Definition

To optimize the snap fit of car roof rail for force requirement of snapping & unsnapping 6.5 kg (max) & 11 kg (min) respectively.

Challenges

Shock analysis

Conclusions
  1. The force required for snapping & unsnapping will be approximately 8.2 kg & 12.9 kg.
  2. For snapping & unsnapping, the equivalent strain in all the components are below break limit.
CAD Model
Unsnapping
Loading & Boundary Conditions
 
Location Total Deformation (mm) Snapping Force (kg) Unsnapping Force (kg)
4 1.62 8.2 12.9

Problem Definition

To check the strength of all parts of lift tackle for lifting Jaguar engine.

Challenges

CAD Modeling and mapping with actual model. (Reverse Engineering)

Conclusions
  1. The FOS of Lifter assembly (CASE-A) is almost 1.6 for 1000 kg loading with E250 material.
CAD Model
Equivalent (von-Mises) Stress Plot of Plate
Loading & Boundary Conditions
Total Deformation