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Effect of oxygen shielding on the tensile and fatigue performance of 300M repaired through laser-directed energy deposition

Published online by Cambridge University Press:  03 November 2023

C. Barr*
Affiliation:
RMIT Centre for Additive Manufacturing, Carlton, VIC, Australia DMTC Ltd, Hawthorn, VIC, Australia
R.A.R. Rashid
Affiliation:
School of Engineering, Faculty of Science, Engineering and Technology, Swinburne University of Technology, Melbourne, VIC, Australia DMTC Ltd, Hawthorn, VIC, Australia
S. Palanisamy
Affiliation:
School of Engineering, Faculty of Science, Engineering and Technology, Swinburne University of Technology, Melbourne, VIC, Australia DMTC Ltd, Hawthorn, VIC, Australia
N. Matthews
Affiliation:
Rosebank Engineering, Bayswater, VIC, Australia DMTC Ltd, Hawthorn, VIC, Australia
M. Brandt
Affiliation:
RMIT Centre for Additive Manufacturing, Carlton, VIC, Australia DMTC Ltd, Hawthorn, VIC, Australia
*
Corresponding author: C. Barr; Email: cameron.barr@rmit.edu.au

Abstract

Laser-directed energy deposition (L-DED) is a key enabling technology for the repair of high-value aerospace components, as damaged regions can be removed and replaced with additively deposited material. While L-DED repair improves strength and fatigue performance compared to conventional subtractive techniques, mechanical performance can be limited by process-related defects. To assess the role of oxygen on defect formation, local and chamber-based shielding methods were applied in the repair of 300M high strength steel. Oxidation between layers for locally shielded specimens is confirmed to cause large gas pores which have deleterious effects on fatigue life. Such pores are eliminated for chamber shielded specimens, resulting in an increased ductility of ∼15%, compared to ∼11% with chamber shielding. Despite this, unmelted powder defects are not affected by oxygen content and are found in both chamber- and locally shielded samples, which still have negative consequences for fatigue.

Type
Research Article
Copyright
© The Author(s), 2023. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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Footnotes

A version of this paper first appeared at The Australian International Aerospace Congress 2021 (AIAC19).

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