One of the most crucial components of a working engine system is its engine blades, such as turbine or compressor blades. A turbofan engine, for example, has many parts: at the front, the fan draws in the air and directs it into the compressor, which is composed of several blades arranged in a row and decreasing in size towards the end of a narrowing tube. Using a rotational movement, the suction air is compressed to up to a thirtieth of its volume, which in turns compresses and heats the gas. The air is then fed into the combustion chamber where it is mixed with injected kerosene and burned. The resulting energy propels the high-pressure turbine where the turbine blades driving the compressor are installed. The downstream low-pressure turbine is also set in motion using this energy. The low-pressure turbine consists of longer turbine blades and is directly connected to the fan. The turbine ensures that the fan rotates. The fan not only sucks the air into the interior, but past the compressor and the turbine. The cold air, which is fed past the interior, generates the greatest propulsive force. The process inside the engine merely ensures that the engine remains running. So the exhaust gas flow produces 20% of the propulsion and the fan, 80%. Both the turbines and compressor blades are subject to high temperatures and pressures. Manufacturers have therefore implemented strict regulations for the production and processing methods used.

A turbine blade pre- and post-processing

The engine blades used in the aerospace industry are usually made of materials that are difficult to machine and have a low tolerance that must be met to obtain the ideal air flow and maximum wear resistance. These components are exposed to extreme temperatures of up to 1,000°C. This means that the blade surfaces also have to be of the highest quality and optimally adapted to the conditions in the engine. OTEC has developed a special process to improve the efficiency and safety of engine blades and produce fewer defects.

Smoothing the air foil, i.e. the blade body, has a positive impact; depending on the required result, the surface can be smoothed to values of up to Ra < 0.2 μm in a few minutes, increasing blade efficiency. The material is removed evenly and only a minute amount is taken from the surface. Repairing the leading and trailing edges with precision rounding can reduce the quantity of rejected parts. The upstream machining process, e.g. blasting, can damage these edges. OTEC’s method enables them to be rounded to a given radius and hence repaired. The rounding process is very precise and involves minimal material removal.

Results after rounding the blade edges in the stream finishing process

Deburring the root helps to improve safety by preventing the blade from becoming caught in the disc. Surface treatment not only prolongs the service life of the blades but increases their efficiency. This is also the ideal preparation for coating the components. Smoothing and rounding the engine blades is possible in a single operation thanks to OTEC’s innovative stream finishing process.

In the stream finishing process, the blades are clamped into the machine and lowered into a container of abrasive. Processing is carried out by both the rotation of the container and the movement of the workpiece in the media flow. The flow to the blades in the machine is clocked, i.e. the alignment angle of the workpiece changes at frequent intervals. This means processing can be precisely aligned to specific points on the workpiece, achieving a smooth surface and precise rounding without altering the shape of the blade. An important benefit of OTEC’s process is the ultrashort machining times compared to conventional processes. Depending on the size and initial condition of the workpiece, the surface treatment of engine blades takes between 2 and 20 minutes. As the blades are clamped individually, no damage will occur to the workpiece surface. All processing steps can be carried out in one machine. The SF-5 stream finishing system can process up to five engine blades at once, ensuring high output and cost efficiency. Tests conducted after OTEC processing show positive results for residual stress, fatigue strength and fluorescence control.


Turbine blades are available in various designs, sizes and materials, including of nickel-titanium or tungsten-molybdenum alloys. They are forged, machined or manufactured with the new laser sintering process. All of them need a surface treatment after production, since the roughness is too large or the edges are too sharp.

Technical Advantage:


Homogeneous smoothing the surface, Ra 0.06 – 0.4 μm according to processing requirement.


Minimum effect on the shape of the blades


Rounding the edges to a defined dimension


High output (max. 5 blades at the same time)


Max. length of blade ~300mm


Max. diameter of blisk 500mm

Before processing


 After processing


Before processing

Ra0,54 μm

 After processing

 Ra0,06 μm

Before processing

Ra3,45 μm

 After processing

Ra0,20 μm

Processing time 100 min./cycle

Turbine blade root and turbine blisk

Before processing

Ra0,54 μm

 After processing

 Ra0,06 μm