Design of gating systems in production of gas turbine engine blades


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

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

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2017