Design of gating systems in production of gas turbine engine blades
- Authors: Smykov A.F.1, Moiseev V.S.1, Chumadin A.S.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 60, No 2 (2017)
- Pages: 317-320
- Section: Aircraft Production Technology
- URL: https://journal-vniispk.ru/1068-7998/article/view/230153
- DOI: https://doi.org/10.3103/S1068799817020258
- ID: 230153
Cite item
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.
About the authors
A. F. Smykov
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: tip_dsaf@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
V. S. Moiseev
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
A. S. Chumadin
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
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