Design of gating systems in production of gas turbine engine blades
- 作者: Smykov A.F.1, Moiseev V.S.1, Chumadin A.S.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 60, 编号 2 (2017)
- 页面: 317-320
- 栏目: 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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详细
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.
作者简介
A. Smykov
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: tip_dsaf@mail.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
V. Moiseev
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
A. Chumadin
Moscow Aviation Institute (National Research University)
Email: tip_dsaf@mail.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
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