
The SPE 6 CNC is a high-precision machine tool for turbine blade grinding, polishing and finishing in aerospace and power generation applications. It is designed for aircraft engine turbine blades, compressor blades, industrial gas turbine blades, steam turbine blades, guide vanes and buckets.
Using six interpolating CNC axes and a pressure-controlled floating axis, the SPE keeps the abrasive belt perpendicular to the turbine airfoil surface. This ensures repeatable stock removal, excellent surface quality and high profile accuracy on complex blade geometries.
Typical applications include turbine blade manufacturing after milling, edge polishing, coating preparation, aerofoil finishing and controlled removal of surface irregularities on titanium and nickel-based blades.
The SPE 6 CNC enables highly repeatable grinding, polishing and finishing of industrial gas turbine blades used in power generation and heavy-duty turbomachinery.
Its rigid CNC machine concept ensures stable blade positioning, constant material removal and excellent surface quality even on large compressor and guide vane profiles.
Compared with robotic finishing systems, fixed workpiece coordinates improve process stability and reduce correction effort.
The SPE 6 CNC is designed for repeatable turbine blade finishing where profile accuracy, edge quality and controlled abrasive pressure are critical.
The six interpolating axes and programmable floating pressure axis ensure that the contact wheel remains perpendicular to the blade surface throughout the full airfoil geometry.
This is particularly important for turbine blade manufacturing after milling, where constant stock removal directly affects aerodynamic quality and coating performance.
Benefits of the SPE process include:
- Constant quality of blades
- Impeccable surface quality
- Highly reproducible and repeatable process
- Easy to program by means of off-line software
- Significant savings in a 5-axis milling process through balancing of process.
- Work relief in particular with heavy blades.
- Precise polishing and profiling of leading and trailing edges
- Perfect solution for turbine blades manufacturing

Gas turbine compressor blade in SPE machine tool.
This abrasive finishing reference documents typical turbine blade production requirements where repeatable stock removal, edge stability and reproducible surface quality are critical. Similar finishing principles are applied on the SPE 6 CNC platform.
3M - GE Vernova turbine blade finishing case study (pdf)
DownloadThe SPE 6 CNC enables highly repeatable polishing and finishing of aircraft engine turbine blades, compressor airfoils and small aero engine blades.
Typical applications include:
Using narrow contact wheels, the SPE processes:
Unlike robotic polishing systems, the SPE is based on a rigid CNC machine tool concept with a fixed coordinate system.
This offers major advantages for turbine blade production:
For turbine OEM production this results in higher repeatability and process stability.

SPE airfoil grinding and polishing machine tool.
The SPE is designed for complex airfoil geometries and demanding finishing tasks on turbine blade surfaces.
Its axis arrangement allows precise grinding and polishing of:
The machine is also suitable for polishing and finishing coated blades, including thermal barrier coatings (TBC) and steam turbine blade coatings (STBC), with controlled contact pressure and consistent surface quality.
The SPE process reduces roughness values and improves profile consistency.
Integrated measuring solutions support:

The SPE turbine blade finishing machine is suitable for a wide range of aerospace and energy materials:
The wet belt grinding process ensures cooling of the blade surface, reduces the risk of thermal damage and helps contain harmful grinding dust.
One of the major benefits of the SPE process is the improvement of blade surface quality after upstream milling.
Typical improvements:
A typical compressor blade example achieves a surface improvement from Ra 3.2 to Ra 0.5.
Typical surface roughness requirements in turbine blade manufacturing range from Ra 1.2 µm (47.2 µin) to Ra 0.6 µm (23.6 µin) for steam turbine blades, and from Ra 0.6 µm (23.6 µin) down to Ra 0.4 µm (15.7 µin) for gas turbine blades, guide vanes and aircraft engine blades.
Under production acceptance conditions, the SPE 6 CNC achieved surface finishes down to Ra 0.12 µin (0.003 µm) using a two-step abrasive process.
The first step removes milling marks using structured abrasive belts such as A45, followed by ultra-fine finishing with A16 Trizact belts to obtain super-finished blade surfaces while maintaining profile accuracy.
Such a process can reduce or eliminate downstream finishing operations in selected turbine blade production environments.
The SPE 6 CNC uses Siemens Sinumerik One control and supports fast NC program creation through CAD/CAM software.
Advantages include:

Trailing edge finishing of turbine blade in wet CNC grinding process

Blade profile measurement using Hexagon 3D Form Inspect after polishing

Polishing and finishing radius, transition and tri-plane surface of a turbine blade.

Integrated CMM blade measurement inside SPE 6 CNC machine

Highly twisted gas turbine blade finishing during 6-axis interpolation

Hexagon 3D inspection result after turbine blade polishing on SPE 6 CNC
Turbine blade polishing is typically performed on CNC grinding and polishing machines such as the SPE 6 CNC or for larger blades the MTS 6 CNC.
After milling, turbine blades are usually ground, polished and finished to reduce scallop marks, improve roughness values and optimize aerodynamic surfaces.
Wet belt grinding helps cool the workpiece, protects sensitive alloys against overheating, improves surface quality and contains harmful grinding dust.
Yes. The SPE is suitable for the controlled finishing and polishing of coated turbine blades, including TBC and STBC applications.
CNC turbine blade polishing allows highly repeatable surface finishing with tight tolerance control, typically reducing roughness and preserving blade geometry within narrow specification limits.
Typical surface roughness requirements in turbine blade manufacturing range from Ra 1.2 µm to Ra 0.4 µm depending on blade type and application.
Steam turbine blades are typically finished to Ra 1.2–0.6 µm, while gas turbine blades, guide vanes and aircraft engine blades often require Ra 0.6–0.4 µm.
Under production acceptance conditions, the SPE 6 CNC achieved surface finishes down to Ra 0.12 µin (0.003 µm) using a two-step abrasive finishing process with A45 and A16 structured abrasive belts.
Yes. The SPE 6 CNC can achieve very fine turbine blade surface finishes under production acceptance conditions using a two-step abrasive process.
In the first step, milling marks are removed using structured abrasive belts such as A45. In the second step, ultra-fine finishing with A16 Trizact belts produces superfinished blade surfaces while maintaining stable blade geometry.
Surface finishes down to Ra 0.12 µin (0.003 µm) have been achieved in production acceptance conditions. Such results can reduce or eliminate downstream superfinishing operations in selected turbine blade manufacturing environments.
The SPE 6 CNC processes complex aircraft engine blades with repeatable geometry control, stable edge finishing and fine surface quality for demanding aerospace applications.
This process demonstrates why highly twisted industrial gas turbine blades are difficult to finish manually.
The SPE maintains constant abrasive orientation across the full blade profile by simultaneous CNC interpolation.
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