GrabCAD 模型信息
Jet Engine Exhaust Cover – Concept Mechanical Design · 模型 59400
This project presents a conceptual jet engine exhaust cover designed to provide structural protection and thermal shielding for the turbine exhaust section. DESIGN OVERVIEW The model features a cylindrical outer casing with radial fin structures distributed circumferentially. The fins are designed to simulate thermal dissipation elements while maintaining structural rigidity. The rear section integrates a reinforced mounting flange with bolt-hole patterns, indicating potential attachment to an exhaust or turbine housing structure. KEY FEATURES - Radial fin configuration for heat dissipation concept - Reinforced cylindrical shell structure - Bolt-pattern rear mounting interface - High-temperature resistant conceptual material (metal alloy) - Detailed mechanical surface modeling ENGINEERING CONSIDERATIONS - Designed with thermal expansion and high-temperature exposure in mind - Radial geometry supports airflow interaction and heat management - Concept applicable for turbine exhaust shielding or protective casing - Geometry suitable for CNC machining or casting manufacturing process SOFTWARE USED (Solidworks) PROJECT TYPE Mechanical Concept Design – Aerospace Inspired Component
- 格式
- SOLIDWORKS、Rendering
- 分类
- Aerospace、Aviation、Machine design
- 标签
- aviation、cad model、3d modeling、solidworks、engine component、exhaust、mechanical design、turbine、aerospace、jet engine
- 数据更新
- 2026-10-08T13:08:28Z
