GrabCAD 模型信息
Precision Turbojet Exhaust Nozzle & High-Temperature Afterburner Component / Hassas Turbojet Egzoz Lüle Çıkışı ve Yüksek Sıcaklık Art Yakıcı Bileşeni · 模型 60319
Precision-engineered turbojet exhaust nozzle and high-temperature afterburner component, designed for aerospace propulsion systems, gas turbine exhaust assemblies, thrust vectoring channels, and experimental jet motor test beds. Featuring a complex multi-stage cylindrical housing integrated with convergent-divergent exhaust profiles, structural mounting flanges, and an outer thermal shielding layer containing precision-perforated cooling matrix patterns. This intricate geometry is engineered to accelerate high-velocity exhaust gases, manage extreme thermal gradients, and withstand high-frequency acoustic and gas-dynamic pressures under maximum thrust conditions. Modeled with a strict focus on DFM (Design for Manufacturing) standards for advanced multi-axis CNC milling, sheet metal stamping, laser drilling, and high-temperature superalloy processing from nickel-based superalloys (such as Inconel) or titanium alloys, 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-structural FEA analyses, and advanced aerospace propulsion CAD libraries. Available Formats: .STEP (for universal CAD compatibility). Highly suitable for aerospace propulsion engineering, gas turbine exhaust design, high-temperature thermal simulations, advanced manufacturing research, and rapid mechanical prototyping.
- 格式
- STL、STEP / IGES、Rendering
- 分类
- 3D printing、Aerospace、Aviation
- 标签
- aerospace、turbojet、jet-engine、afterburner、exhaust-nozzle
- 数据更新
- 2026-10-10T08:52:50Z
