GrabCAD 模型信息
Precision Axial Turbine Compressor Blade & Jet Engine Airfoil Rotor Assembly / Hassas Eksenel Türbin Kompresör Kanadı ve Jet Motoru Aerodinamik Rotor Montajı · 模型 60323
Precision-engineered axial turbine compressor blade and jet engine airfoil rotor assembly, designed for aerospace propulsion systems, high-speed gas turbine stages, dynamic airflow compression, and advanced aerospace testing setups. Featuring a heavy-duty multi-stage cylindrical rotor drum integrated with hundreds of precision-profiled aerodynamic compressor blades, a centralized high-speed shaft pass-through bore, and optimized twist-and-taper airfoil geometries designed to maximize air compression efficiency and mass flow rate under extreme centrifugal and aerodynamic loads. Modeled with a strict focus on DFM (Design for Manufacturing) standards for 5-axis CNC milling, precision electrochemical machining (ECM), and titanium/nickel-based superalloy processing, ensuring tight aerodynamic profile tolerances, superior high-cycle fatigue resistance, and optimal dynamic balance. It serves as an essential baseline model for computational fluid dynamics (CFD) simulations, aerodynamic performance evaluations, and advanced aerospace propulsion CAD libraries. Available Formats: .STEP (for universal CAD compatibility). Highly suitable for aerospace propulsion engineering, gas turbine compressor design, high-speed fluid dynamics simulations, advanced manufacturing research, and rapid mechanical prototyping.
- 格式
- STL、STEP / IGES、Rendering
- 分类
- 3D printing、Aerospace、Aviation
- 标签
- gas-turbi、aerospace-component、jet-engine、compressor-blade
- 数据更新
- 2026-10-09T10:49:16Z
