Design of gating systems in production of gas turbine engine blades
- Autores: Smykov A.F.1, Moiseev V.S.1, Chumadin A.S.1
-
Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 60, Nº 2 (2017)
- Páginas: 317-320
- Seção: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/230153
- DOI: https://doi.org/10.3103/S1068799817020258
- ID: 230153
Citar
Resumo
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.
Sobre autores
A. Smykov
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: tip_dsaf@mail.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
V. Moiseev
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
A. Chumadin
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
Arquivos suplementares
