Turbine blade manufacturing - grinding, polishing, finishing

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Airfoil finishing and airfoil polishing are critical process steps in the production of turbine blades, compressor blades, guide vanes and other aerofoil components for aerospace and power generation. After milling, forging or casting, the airfoil profile often requires controlled grinding, deburring and polishing to remove machining marks, blend transitions and improve surface quality before final inspection, coating or assembly.

IMM Maschinenbau offers both CNC and manual solutions for airfoil finishing, depending on part size, geometry and production volume. Our systems are used for the controlled processing of turbine blade surfaces, leading and trailing edges, platform transitions and radius areas. Wet processing, stable machine kinematics and programmable process parameters help achieve repeatable results on titanium, nickel-based alloys, cobalt alloys and stainless materials.

For customers requiring high repeatability, CNC airfoil finishing offers clear advantages. With the IMM SPE and MTS platforms, process parameters such as feed rate, cutting speed and contact pressure can be controlled and reproduced with high consistency. This supports automatic precision finishing of turbine blade airfoil surfaces, including the reliable removal of machining marks and the polishing of complex contours that are difficult to achieve consistently by manual methods alone.

For complex turbine blade geometries and recurring airfoil families, CAD/CAM-supported programming helps create repeatable finishing processes from the actual part geometry. The IMM workflow is based on Mastercam, which is included in the package, and extended by a dedicated add-on for turbine blade and airfoil finishing.

In the documented workflow for IMM SPE and MTS, the blade is aligned to the machine coordinate system, prepared as individual surfaces such as convex, concave, leading edge and trailing edge, and programmed as defined finishing operations. Multi-axis toolpaths are generated normal to the actual freeform surface, with selectable polishing directions such as root to tip or leading edge to trailing edge.

A key advantage is the controlled adjustment of local process parameters along the blade surface. Feed rate, pressure, spindle speed and axis offsets can be assigned through a definable point matrix, while simulation and NC-code generation support process verification before production. This gives programmers a familiar CAM foundation instead of requiring them to move into a completely separate software world.

After milling, turbine blades usually require additional abrasive finishing to remove scallop marks, stabilize edge geometry and improve surface quality.

Typical target roughness values include:

•  Steam turbine blades: Ra 1.2 µm to 0.6 µm (≈ 47 µin to 24 µin)
   
• gas turbine blades and vanes:  Ra 0.6 µm to 0.4 µm (≈ 24 µin to 16 µin)
   
• aircraft engine blades:  Ra 0.4 µm and below (≤ 16 µin)
   

Using a two-step abrasive process, superfinished surfaces down to Ra ≤ 0.05 µm (≈ 2 µin) can be achieved under production conditions, with Ra ~0.03 µm (≈ 1.2 µin) demonstrated during customer acceptance tests. 

Compared with manual polishing, CNC turbine blade finishing offers significantly higher repeatability — for example with systems such as the SPE 6 CNC turbine blade finishing and polishing machine. In aerospace turbine blade manufacturing, stable leading edge geometry and repeatable surface roughness are critical for aerodynamic efficiency and coating adhesion. CNC belt grinding systems support these requirements by maintaining defined contact pressure and reproducible stock removal.

Production benefits include:

• stable stock removal across multiple blade rows
   
• highly reproducible surface quality
   
• reduced manual grinding effort
   
• shorter milling cycles through balanced stock removal
   
• easy programming through offline software
   
• controlled polishing of leading and trailing edges
   
• coolant-based processing for thermal protection and dust control

• accurate and consistent removal of casting layers and patches on cast gas turbine blades and vanes

Belt grinding and polishing are established processes in aerospace and energy manufacturing and are widely documented in engineering literature. For example, the reference work Aerospace Manufacturing Processes by Pradip K. Saha (CRC Press) describes belt grinding as a key method for achieving precise and repeatable surface finishes on turbine blades. This applies to both aircraft engine blades and industrial gas and steam turbine blades. 

The process is particularly valued for its combination of high material removal rates, controlled surface quality, and suitability for complex geometries. In modern production environments, CNC belt grinding machines are used to ensure consistent results across a wide range of aerospace components, including turbine blades made from titanium and nickel-based alloys.

IMM Maschinenbau GmbH is referenced in this publication, underlining its proven expertise in turbine blade grinding and polishing technology. 

 Depending on blade size, geometry and production volume, different machine concepts are used. 

Learn more about the SPE 6 CNC turbine blade finishing machine for blades up to approx. 550 mm.

For:

• aircraft engine blades
   
• compressor blades
   
• highly twisted gas turbine blades

For larger turbine blades and vanes, explore the MTS 6 CNC turbine blade grinding machine.

For:

• large industrial gas turbine blades

• large aircraft engine fan blades; near net forged fan blades and metallic leading edge sheaths
   
• large steam turbine blades
   
• heavy compressor blades

For manual finishing and repair work, see the 72713 belt grinding machine.

For:

• repair work
   
• manual edge correction
   
• flexible abrasive finishing

The finishing process must preserve blade geometry while improving surface roughness.

Particularly critical are:

• leading edge radii
   
• trailing edge thickness
   
• platform transitions
   
• twisted airfoil sections
   

Integrated measuring systems such as Hexagon 3D inspection can validate profile stability directly after grinding.

In industrial production environments, two-step abrasive finishing can significantly reduce downstream superfinishing operations.

First, milling marks are removed using structured abrasive belts such as A45.

In the second step, ultra-fine Trizact belts such as A16 generate superfinished surfaces while maintaining stable blade geometry.

Such process layouts can replace downstream brush finishing in selected blade manufacturing environments.

View turbine blade customer references.

In turbine blade manufacturing, both robotic polishing systems and CNC belt grinding machines are used for finishing operations. Robotic systems are often associated with flexible force control, while traditional CNC machines are considered rigid.

However, modern CNC turbine blade finishing systems combine both approaches. Machines such as the SPE 6 CNC and MTS 6 CNC integrate active force control systems, allowing constant and controlled contact pressure during grinding and polishing.

This enables the machine to compensate for casting or forging tolerances and ensures uniform material removal across complex blade geometries — similar to robotic systems, but within a fixed and highly accurate machine coordinate system. The same principle also supports stable finishing of milled blade components and SPF-formed parts.

Unlike robotic cells, CNC systems operate in a defined coordinate environment, eliminating the need for complex measurement and compensation systems. This results in higher positional accuracy, improved repeatability and more stable process control.

As a result, CNC belt grinding machines combine:

• precise positioning and repeatability of CNC machine tools
• adaptive force control for consistent polishing pressure
• stable and reproducible surface finishing results

IMM also offers robotic grinding and polishing solutions for suitable components. For automated airfoil polishing, however, CNC-based processing is generally preferred because the fixed machine coordinate system offers higher positional accuracy and reduces intermediate measuring effort compared with robotic cells.  

This significantly reduces the traditional trade-off between rigid CNC machining and flexible robotic polishing, making CNC the preferred solution for many aerospace and energy turbine blade applications. 

Programmable force-controlled finishing (H1, S, F): 

In addition to conventional CNC parameters such as cutting speed (S) and feed rate (F), modern CNC turbine blade finishing machines also use contact pressure (H1) as a fully programmable feedback-controlled process parameter.

This allows grinding and polishing operations to be defined, controlled and reproduced with CNC-level precision. The result is a stable, quantifiable and repeatable finishing process, independent of operator influence.

While robotic systems rely on adaptive force control, CNC-based force feedback allows defined and continuously controlled process parameters within a fixed machine coordinate system. This results in higher process stability, improved repeatability and reduced variability in turbine blade finishing. The system does not just react to the process — it actively controls it.