Abstract The methodological background of designing the casting technological processes by controlling cast workpieces solidification process is considered for gas turbine engine blades. The general structure of software packages for computer-aided calculations of casting process parameters for the blade class cast product is presented. The example of designing the gating system for a specific product is given.
Design of gating systems in production of gas turbine engine blades
Russian Aeronautics ; 60 , 2 ; 317-320
2017-04-01
4 pages
Article (Journal)
Electronic Resource
English
Design of gating systems in production of gas turbine engine blades
Online Contents | 2017
|Probabalistic modal analysis for turbine engine blades
AIAA | 2001
|Multiaxial testing of gas turbine engine blades
AIAA | 2000
|Aircraft turbine engine comprising variable-pitch propeller blades
European Patent Office | 2023
|Cooling Modern Aero Engine Turbine Blades and Vanes
SAE Technical Papers | 1966
|