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Aerospace Bracket Optimization
Weight reduction of 32% through topology optimization.
FEA & Simulation2024
This project involved optimizing an aerospace bracket using finite element analysis. The goal was to reduce weight while maintaining structural integrity under high vibration and load conditions.
We performed topology optimization, validated with nonlinear static analysis, and achieved a 32% weight reduction without compromising safety factors. The final design passed all certification tests.
Software used: ANSYS Workbench, SolidWorks
Results: 32% weight savings, 15% cost reduction in manufacturing.
Key Deliverables
- FEA report
- Optimized CAD model
- Stress plots
Technologies Used
ANSYS WorkbenchSolidWorksMATLABPython
Project Impact & Results
- 32% weight reduction achieved through topology optimization
- 15% reduction in manufacturing cost
- Successfully passed all certification tests
- Reduced stress concentration by 40% in critical areas