Titanium Turbine Blade
This titanium alloy turbine blade is a high-temperature resistant aerodynamic component for gas turbines, aero-engines and industrial power generation turbomachinery. Monolithically machined from solid aerospace grade titanium billet, it features complex twisted 3D airfoil, smooth curved surface and integrated mounting base. The integrated forming delivers micron-level precision on airfoil profile, outstanding surface finish and stable structural strength, sustaining long-term operation under high temperature, high pressure and high-speed airflow working environments.
- Machining Process: 5-axis linkage CNC milling, precision micro-deburring, surface passivation & polishing, dimensional contour inspection
- Material: Aerospace Grade Ti-6Al-4V Titanium Alloy
- Accuracy: ±0.005 mm
- Surface Finish: Brushed matte finish, mirror polishing optional
- Features: High temperature resistance, lightweight high tensile strength, corrosion & oxidation resistant, precise aerodynamic profile
Five-Axis Machining of Twisted Turbine Airfoils
The titanium turbine blade is machined from a solid aerospace-grade titanium billet, combining the twisted airfoil, transition radius and mounting base in one continuous structure. This production route avoids welded joints between the blade and root, reducing weak points under centrifugal force, pressure fluctuation and repeated thermal loading.
Full five-axis simultaneous machining allows the cutting tool to follow the airfoil from leading edge to trailing edge while maintaining the specified twist, chord and thickness distribution. Controlled roughing removes material without placing excessive stress on thin blade sections. Finish milling then refines the pressure side, suction side and edge geometry to achieve an airfoil contour tolerance of ±0.005 mm under confirmed inspection conditions.
Surface Control for High-Speed Gas Flow
Small deviations in blade curvature can change local airflow, pressure distribution and rotor balance. Toolpaths are developed around the aerodynamic surface rather than treating the blade as a standard prismatic component. Fine-step milling and precision deburring reduce cutter marks along the gas-flow direction, while optional polishing improves the finish on critical aerodynamic areas.
The integrated mounting base receives the same datum control as the airfoil. This maintains the relationship between the blade profile, root geometry and fastening features during rotor assembly. Three-dimensional CMM inspection or full-profile scanning can compare the machined surface with the approved digital model, revealing local contour deviations that conventional gauges cannot fully capture.
Titanium combines low density with high tensile strength and resistance to cyclic loading. The reduced blade mass lowers rotor inertia, while the material retains the rigidity needed to withstand high-speed airflow and repeated rotational stress. Surface finishing and oxidation-control treatments can be selected according to the specified operating temperature and gas environment.
Core Advantages
- Excellent High-Temperature Resistance: Aerospace titanium alloy maintains stable mechanical strength under continuous high-temperature airflow, resisting thermal deformation and oxidation compared to regular steel alloys.
- Ultra-Precise Twisted Airfoil Profile: Full 5-axis linkage machining perfectly replicates complex twisted curved airfoil geometry with micron-level accuracy, reducing airflow turbulence loss and boosting overall turbine power efficiency.
- Lightweight & High Structural Rigidity: Low-density titanium raw material cuts blade overall weight to lower rotor rotation inertia, while retaining strong tensile strength to withstand high-speed airflow impact without bending or cracking.
- Integrated Base & Blade One-Piece Forming: Airfoil and mounting base are milled from a single titanium billet, eliminating assembly seams and welding defects, improving structural stability and service lifespan under cyclic high-load operation.
- Fully Customizable Aerodynamic Design: Custom airfoil twist angle, blade height, base mounting hole layout, overall thickness and surface roughness are all available according to your turbomachinery technical drawings.
Common Applications
Final inspection covers airfoil contour, blade thickness, root dimensions, mounting features and surface condition. Each titanium turbine blade can also receive 3D profile comparison and visual edge checks before release, helping maintain consistent geometry across matched rotor sets and recurring production batches.
Specification Table
| Parameter | Details |
| Raw Material | Aerospace Grade Ti-6Al-4V Titanium Alloy |
| Machining Process | 5-axis simultaneous CNC milling, micro deburring, surface passivation & polishing, 3D contour scanning inspection |
| Dimensional Tolerance | Ultra-precision ±0.005 mm for airfoil curved profiles |
| Surface Finish | Standard brushed matte finish, high-gloss mirror polishing (Optional) |
| Blade Size Range | Custom per aerodynamic drawings, common height range: 20mm–250mm |
| Contour Twist Angle | Fully customizable based on turbine aerodynamic parameters |
| Continuous Working Temperature | -50℃ ~ +550℃ |
| Quality Control | Full 3D CMM airfoil scanning inspection, surface roughness testing, material hardness test, airflow contour precision verification |
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