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For an aircraft turbine, all necessary compressor stages for a test bench installation were made by rapid prototyping. Due to the fact that the guide vanes inside the compressor stages could not be machined afterwards, it was necessary to achieve the high accuracy demanded before this in the unfinished casting blank. The molds used for this are made by direct molding material milling in combination with Direct Croning® - batch parts and cores. Before the mold assembly, the individual mold segments were surveyed and the mold assembly itself supervised by a 3D measuring lever. The surface quality of Rz 6.3 necessary for aerodynamics was achieved by grinding after CNC machining.
