GrabCAD 模型信息
CF6 80C2 Turbofan Engine · 模型 128868
This model represents the CF6-80C2 high-bypass turbofan engine as a simplified single-part file, capturing the essential outer geometry and internal stage representation for conceptual design and visualization. The modeling process included: 1. Fan Section: A multi-blade fan was created using Swept Boss/Base and Circular Pattern to replicate aerodynamic fan blades around a central hub. 2. Compressor and Turbine Stages: Basic profiles of the low-pressure and high-pressure compressors and turbine blades were sketched using Revolve and Lofted Boss/Base, abstracting the internal flow path. 3. Combustor Section: A mid-section cylindrical chamber was added between compressors and turbines, modeled using Extruded Boss/Base and detailed with vent holes using Extruded Cut. 4. Nacelle and Outer Casing: The engine’s nacelle was constructed using Revolved Boss/Base and detailed with Fillet and Shell features to simulate a lightweight outer body. 5. Shaft Representation: A central shaft was modeled through the core using Extrude and Fillet to connect fan, compressors, and turbines. 6. Inlet and Exhaust Nozzles: Shaped using Lofted and Revolved Boss/Base features to represent inlet geometry and nozzle tapering.
- 格式
- SOLIDWORKS、Rendering
- 分类
- Aerospace、Aviation、Machine design
- 标签
- 未标注
- 数据更新
- 2026-10-15T13:22:30Z
