GrabCAD 模型信息
Precision Turbojet Fan Blade & Axial Flow Rotor Component / Hassas Turbojet Fan Kanadı ve Eksenel Akışlı Rotor Bileşeni · 模型 60322
Precision-engineered turbojet fan blade and axial flow rotor component, designed for high-bypass turbofan engines, aerospace propulsion systems, fan stage airflow intake assemblies, and advanced aerodynamic testing facilities. Featuring a heavy-duty multi-blade fan drum integrated with precision-profiled twist-and-taper fan blades, a centralized high-speed drive shaft pass-through bore, and optimized aerodynamic airfoil geometries designed to maximize initial mass air intake, fan pressure ratio, and thrust efficiency under extreme centrifugal and rotational loads. Modeled with a strict focus on DFM (Design for Manufacturing) standards for 5-axis CNC milling, precision forging, electrochemical machining (ECM), and advanced titanium or composite alloy processing, ensuring tight blade profile tolerances, superior high-cycle fatigue resistance, and optimal dynamic balance. It serves as an essential baseline model for computational fluid dynamics (CFD) simulations, acoustic noise reduction evaluations, and advanced aerospace propulsion CAD libraries. Available Formats: .STEP (for universal CAD compatibility). Highly suitable for aerospace propulsion engineering, turbofan engine design, high-bypass fan simulations, advanced manufacturing research, and rapid mechanical prototyping.
- 格式
- STEP / IGES、STL、Rendering
- 分类
- 3D printing、Agriculture、Aviation
- 标签
- axial-、aerospace-component、jet-engine、turbofan、fan-blade
- 数据更新
- 2026-10-08T14:32:26Z
