Product Specifications
| Material | Inconel 718, Inconel 625, GH4169, René 41 | Blade Count | 7–31 blades (open / semi-closed / closed) | ||
| Process | 5-Axis CNC Simultaneous Machining + EDM | Working Temp | Up to 1,000°C continuous service | ||
| Tolerance | ±0.005mm (blade profile), ±0.003mm (bore) | Certification | AS9100D / ISO 9001:2015 / BV | ||
| Surface Finish | Ra ≤ 0.8μm (flow path), Ra ≤ 0.4μm (seal faces) | Inspection | HEXAGON CMM + KEYENCE 3D Microscope + Full FAI | ||
| Max Diameter | Up to Ø650mm | Lead Time | Prototype: 15–25 days | Production: TBD by volume | ||
The advantages of the product
Application Scenarios
Turboshaft Engines: Helicopter Main Engines – Bell, Sikorsky, Airbus Helicopter Platforms
Auxiliary Power Unit (APU): Centrifugal Compressors for Rotorcraft
Unmanned Aerial Vehicles/Electric Vertical Takeoff and Landing Vehicles (eVTOL): Next-Generation Electric and Hybrid Propulsion Compressor Impellers.
Ground Test Stands: Engine Test Stands with Flight Equivalent Specifications
Turbine Mechanical Components
FAQ