Manufacturing Route for Hot Stamping of Aluminium Alloy Applied to a Wing Rib

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

Abstract

In this study, a hot stamping process, which delivers ready-to-use parts for the production of aircraft components is applied as an alternative manufacturing method to, for instance, machined parts. The research has been focused on examining the formability of an aluminium alloy at high temperatures. An extensive experimental campaign has been conducted to establish the optimal hot stamping process parameters. As a final stage of the development, a demonstrator corresponding to a wing rib with AA2198 aluminium-lithium alloy has been successfully produced. After the corresponding heat treatment, material properties have been restored.

Original languageEnglish
Title of host publicationManufacturing Route for Hot Stamping of Aluminium Alloy Applied to a Wing Rib
PublisherTrans Tech Publications Ltd
Pages3-15
Number of pages13
Volume1034
DOIs
Publication statusPublished - 2025

Publication series

NameKey Engineering Materials
Volume1034
ISSN (Print)1013-9826
ISSN (Electronic)1662-9795

Keywords

  • Aeronautics
  • Aluminium alloys
  • FE process modelling
  • Hot forming
  • Hot stamping
  • manufacturing route

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