GrabCAD 模型信息
Alcoa Challenge · 模型 308343
The component has been created using topology optimization and FEA reanalysis. High stiffness in loads direction will avoid any resonant frequencies problem in operation. The mass has been reduced of around 50% but it could be reduced even more penalising the stiffness.
- 格式
- Rendering、STEP / IGES
- 分类
- Aerospace、Components、Industrial design
- 标签
- airplanebearingbracket
- 数据更新
- 2026-10-28T14:20:15Z
