Fan Impeller slotting analysis for a tri-hub failure

Summary:

  • Finite element slotting analysis of Fan impeller assembly
  • FE Modeling done in Hypermesh using 10–node Tetrahedron Elements and carried out further Stress Analysis.
  • Model size: Around 100000 elements
  • Material used : Aluminum alloy 6061-T6 per AMS4117
  • The optimum size of the slots were arrived at, to cause the tri-hub failure of the fan impeller.

Simulation of Containment Tri-Hub

Summary:

  • Containment Analysis for simulating tri hub failure in transient domain.
  • Hypermesh is used for preprocessing and LS-Dyna is used for transient analysis.
  • Nozzle 2nd stage, Turbine 2nd stage, Containment ring and Combustor assemblies are considered for containment analysis.
  • Tri-hub (3 pieces) of Turbine 2nd stage subjected to velocity 41,955 rpm and gravity
  • Tri-hub failure is simulated to predict rupture of stator and containment ring.
  • Deliverable are predicting energy absorbing capability of containment ring.

Low Cycle Fatigue Analysis of Mount Lug

Summary:

  • Low Cycle Fatigue Analysis of Mount Lug
  • FE Modeling done in Hypermesh using 10-node Tetrahedron Elements, contact elements.
  • Stress analysis carried out to estimate stress factors.
  • Fatigue analysis (Crack initiation and Crack propagation)
  • FE Model : 0.2 million DOF.
  • Fatigue life estimation, crack propagation after crack initiation, No. of Life cycles before component failure.

Optimization of a Gear-shifting Housing

Summary:

  • Generation of optimal design for stress, manufacturability, functionality and cost
  • Input – Rough concept
Key Challenges:
  • Limited packaging space
  • Manufacturability of the complex ribs and walls
Accomplishments
  • Mesh Generated using Hypermesh
  • Design optimized for weight using Optistruct
  • Reduced stress levels
  • Optimized the design with reduced weight and increased rigidity by providing adequate ribs.

Optimization of the Chassis of a Truck

Summary:

  • Generation of optimal strength and rigidity.
  • Input – Rough concept
Key Challenges:
  • Short Lead-time
  • Manufacturability of the complex ribs and walls
Accomplishments
  • Mid-surfaces were extracted and 2D mesh was generated in Hypermesh. Stress analysis was carried out for various loading conditions and the design was optimized for weight using Optistruct.
  • Design optimized for weight using Optistruct
  • Optimized the design of Chassis was achieved with reduced weight and increased rigidity.