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

Amaia Arroyo Llanos; Garbiñe Atxaga Genbeltzu; Begoña Canflanca Garmendia

doi:10.4028/p-jRUp7r

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

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-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 language	English
Title of host publication	Manufacturing Route for Hot Stamping of Aluminium Alloy Applied to a Wing Rib
Publisher	Trans Tech Publications Ltd
Pages	3-15
Number of pages	13
Volume	1034
DOIs	https://doi.org/10.4028/p-jRUp7r
Publication status	Published - 2025

Publication series

Name	Key Engineering Materials
Volume	1034
ISSN (Print)	1013-9826
ISSN (Electronic)	1662-9795

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 9 Industry, Innovation, and Infrastructure

Keywords

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

Access to Document

10.4028/p-jRUp7r

Cite this

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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.",

keywords = "Aeronautics, Aluminium alloys, FE process modelling, Hot forming, Hot stamping, manufacturing route",

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year = "2025",

doi = "10.4028/p-jRUp7r",

language = "English",

volume = "1034",

series = "Key Engineering Materials",

publisher = "Trans Tech Publications Ltd",

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Manufacturing Route for Hot Stamping of Aluminium Alloy Applied to a Wing Rib. / Arroyo Llanos, Amaia ; Atxaga Genbeltzu, Garbiñe ; Canflanca Garmendia, Begoña.
Manufacturing Route for Hot Stamping of Aluminium Alloy Applied to a Wing Rib. Vol. 1034 Trans Tech Publications Ltd, 2025. p. 3-15 (Key Engineering Materials; Vol. 1034).

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

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AU - Arroyo Llanos, Amaia

AU - Atxaga Genbeltzu, Garbiñe

AU - Canflanca Garmendia, Begoña

PY - 2025

Y1 - 2025

N2 - 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.

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KW - Aeronautics

KW - Aluminium alloys

KW - FE process modelling

KW - Hot forming

KW - Hot stamping

KW - manufacturing route

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

PB - Trans Tech Publications Ltd

ER -

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

Abstract

Publication series

UN SDGs

Keywords

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