In addition, user-defined reports containing sections, labels and much more, support the interpretation and the understanding of the analysis results. At any time - i.e. also after measuring is completed - specific points on the object may be determined, and the deviations for these points can be documented in tables or evaluated statistically with repeated measurements of parts that are identical in construction. The available functions provide for creating standard measuring protocols at any time.
Various methods are available to align the measured data to the nominal geometry. Best-fit algorithms, applied to certain areas of the components, allow for analysing local geometry deviations but also visualize torsion or deformations of partial areas with respect to each other.
If the alignment is made to the aerodynamic part (airfoil) of the turbine blade, the actual deviations in these areas can be analysed. If, however, best-fit registration is performed to the root of the turbine blade, torsion of the airfoil with respect to the root can be detected.
Other registration or coordinate transformation rules like 3-2-1 or RPS registration which uses reference elements like planes, holes, cones, cylinders and much more allow manifold individual solutions.
Fixtures, measured with TRITOP, which are used for the components or turbine blades, guarantee a reproducible positioning of these parts, and coordinate transformation after measuring is no longer necessary. The ATOS system measures directly in the defined coordinate system using the reference point markers of the fixture.
For analysis, components can be measured completely or partially with ATOS in each production step in order to,
- Determine the geometry of blanks. This guarantees that subsequent processing can be carried out properly. It is also possible to consider the blank's geometry when creating processing programs (e.g. milling paths). This reduces the processing time.
- Exactly check the dimensional consistency after cutting processes.
- Check the dimensional consistency or the deformation after heat treatments.
- Measure and assess dents and bumps on airfoils.
- Check the layer thickness when applying protective and insulating layers. The comparison of measurements before and after coating, aligned to the root of the turbine blade, result in the layer thickness.
- Check the mounting of components, e.g. the mounting of individual turbine blades to a blisk.
When repairing turbine blades, ATOS measurements may be used to:
- Document the blades' geometry before and after weld cladding.
- Check the dimensional consistency after processing. |