| About this Abstract |
| Meeting |
Materials Science & Technology 2020
|
| Symposium
|
Solid State Processing of Metals and Composites
|
| Presentation Title |
Development of Spare Parts and Components for Aerospace Engineering out of Heavily Deformed Steels |
| Author(s) |
Valeriy Mishchenko, Anna Ben, Anton Matiukhin, Vitalii Shyrokobokov, Sergey Sheyko, Elena Kulabneva |
| On-Site Speaker (Planned) |
Anton Matiukhin |
| Abstract Scope |
A method of obtaining turbine disks of gas turbine engines (GTE) by isothermal stamping in the shell, which is a complete substitute for cost analogues, is proposed. Further studies of deformation conditions in QForm have been carried out. The application of technology allows obtaining a homogeneous fine-grained structure by volume of the workpiece. Keywords:Hot stamping, heavily deformed alloys, isothermal stamping, sheath, turbine disc, gas turbine engine. |