Abstract
The work describes the results of developing a duplicate model of the gas turbine engine blade casting process. The work was based on the development of the digital “furnace-flask-filler-mould-metal-stopper” process system considering the geometrical, structural and thermophysical specifications of the turbine blade casting process. The industrial approbation of the developed process under the experimental production conditions exemplified by the manufacture of the GTE turbine moving blades demonstrated a 3- to 4-fold decrease in time of the blade blank manufacturing cycle due to the virtual multi-iteration optimization of the process.
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