Design of gating systems in production of gas turbine engine blades


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

Abstract

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.

About the authors

A. F. Smykov

Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: tip_dsaf@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993

V. S. Moiseev

Moscow Aviation Institute (National Research University)

Email: tip_dsaf@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993

A. S. Chumadin

Moscow Aviation Institute (National Research University)

Email: tip_dsaf@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2017 Allerton Press, Inc.