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Precision Medical Devices
Precision Machining of Aero Engine Turbine Disks

Pre-processing

Processed
Difficult
Processing challenges
High-temperature alloys exhibit high hardness and cutting forces; thin-walled structures are prone to deformation, requiring IT5 dimensional accuracy.
Solve
Solutions
Utilize dedicated ceramic cutting tools with a high-pressure cooling system, optimize cutting parameters, and design specialized flexible fixtures to minimize clamping deformation.
Fruit
Processed Results
- • Chamfer turbine blade root fillets to prevent stress concentration.
- • Remove burrs from internal cooling channels to ensure smooth airflow.
- • Precision deburring of the tip sealing surface, roughness Ra0.4
- • Non-destructive machining of superalloys
- • No surface cracks detected via fluorescent penetrant inspection.
- • Batch Pass Rate: 99.1%
Technical Specifications
| Materials | Nickel-based superalloy Inconel 718 |
| Blade Thickness | 0.8-2.5mm |
| Surface Roughness | Ra0.4-Ra0.8 |
| Deburring rate | ≥99.5% |
Need precision machining?
Submit your drawings, 3D files, or product requirements. Our engineering team will provide a professional machining solution.
