Design of gating systems in production of gas turbine engine blades

被引：0
|
作者：
Smykov A.F. [1 ]
Moiseev V.S. [1 ]
Chumadin A.S. [1 ]
机构：
[1] Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, Moscow
来源：
Smykov, A.F. (tip_dsaf@mail.ru) | 1600年 / Allerton Press Incorporation卷 / 60期
关键词：
computer-aided design for technology; gas turbine engine blade; gating system; lost-wax casting;
D O I：
10.3103/S1068799817020258
中图分类号：
学科分类号：
摘要：
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. © 2017, Allerton Press, Inc.
引用
收藏
页码：317 / 320
页数：3
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