Design of gating systems in production of gas turbine engine blades
- Авторлар: Smykov A.F.1, Moiseev V.S.1, Chumadin A.S.1
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- Шығарылым: Том 60, № 2 (2017)
- Беттер: 317-320
- Бөлім: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/230153
- DOI: https://doi.org/10.3103/S1068799817020258
- ID: 230153
Дәйексөз келтіру
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.
Авторлар туралы
A. Smykov
Moscow Aviation Institute (National Research University)
Хат алмасуға жауапты Автор.
Email: tip_dsaf@mail.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
V. Moiseev
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
A. Chumadin
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
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