GrabCAD 模型信息
Precision Jet Engine Turbojet Outer Casing & High-Temperature Aerodynamic Shell Component / Hassas Jet Motoru Turbojet Dış Kabuğu ve Yüksek Sıcaklık Aerodinamik Gövde Bileşeni · 模型 60324
Precision-engineered turbojet outer casing and high-temperature aerodynamic shell component, designed for aerospace propulsion systems, gas turbine engines, bypass housings, and experimental jet motor assemblies. Featuring a heavy-duty cylindrical structural housing integrated with precision-machined connection grooves, mounting flanges, and an optimized internal flow channel designed to withstand extreme thermal gradients and operational gas pressures. Modeled with a strict focus on DFM (Design for Manufacturing) standards for advanced multi-axis CNC turning, deep drawing, structural welding, and high-temperature superalloy processing from nickel-based superalloys (such as Inconel) or stainless steels, ensuring tight wall thickness tolerances, leak-proof integrity, and optimal stress distribution. It serves as an essential baseline model for computational fluid dynamics (CFD) simulations, thermal stress evaluations, and aerospace propulsion CAD libraries. Available Formats: .STEP (for universal CAD compatibility). Highly suitable for aerospace propulsion engineering, gas turbine casing design, high-temperature structural simulations, advanced manufacturing research, and rapid mechanical prototyping.
- 格式
- STEP / IGES、STL、Rendering
- 分类
- 3D printing、Aerospace、Aviation
- 标签
- aerospace-component、turbojet、jet-engine、turbine-casing
- 数据更新
- 2026-10-08T14:32:00Z
