Design of gating systems in production of gas turbine engine blades
- Авторы: Smykov A.F.1, Moiseev V.S.1, Chumadin A.S.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Выпуск: Том 60, № 2 (2017)
- Страницы: 317-320
- Раздел: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/230153
- DOI: https://doi.org/10.3103/S1068799817020258
- ID: 230153
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Аннотация
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.
Об авторах
A. Smykov
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: tip_dsaf@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
V. Moiseev
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
A. Chumadin
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
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