RR GOM: Automatic Generation of Digital Geometry Models from GOM-STL Scans of Turbine Components. Phase IV

Beschreibung:

Building on the findings of three previous phases, the functionalities of the software „Blade2Parameter“ and “BladeCLeaner”, which were developed at the chair of Turbomachinery and Flight Propulsion, are extended to rebuild the geometry of several turbine and compressor components based on optical measurement data. Within this scope, the focus is on an enhanced methodology for closing the cooling holes for turbine components, capturing the tip geometry of compressor blades and others. Furthermore, the treatment of FAN blades will be enabled.