Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment

Laser powder bed fusion (L-PBF) has the potential to be applied in the production of titanium aircraft components with good mechanical properties, provided the technology has been qualified and accepted in the aviation industry. To achieve acceptance of the L-PBF technology in the aircraft industry,...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autores principales: Lehlohonolo Francis Monaheng, Willie Bouwer du Preez, Claudia Polese
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
Materias:
Acceso en línea:https://doaj.org/article/674334bdf5f7459f96c657197e550eae
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
id oai:doaj.org-article:674334bdf5f7459f96c657197e550eae
record_format dspace
spelling oai:doaj.org-article:674334bdf5f7459f96c657197e550eae2021-11-25T18:21:35ZTowards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment10.3390/met111117362075-4701https://doaj.org/article/674334bdf5f7459f96c657197e550eae2021-10-01T00:00:00Zhttps://www.mdpi.com/2075-4701/11/11/1736https://doaj.org/toc/2075-4701Laser powder bed fusion (L-PBF) has the potential to be applied in the production of titanium aircraft components with good mechanical properties, provided the technology has been qualified and accepted in the aviation industry. To achieve acceptance of the L-PBF technology in the aircraft industry, mechanical property data needed for the qualification process must be generated according to accepted testing standards. The impact toughness of Ti6Al4V extra low interstitial (ELI) specimens, produced through L-PBF followed by annealing, was investigated in this study. Charpy impact testing complying with American Standard Test Method (ASTM) E23 was performed with specimens annealed and conditioned at low temperature. On average, the toughness recorded for the specimens with 3D-printed and machined V-notches was 28 J and 31 J, respectively. These results are higher than the 24 J required in the aerospace industry. Finally, fractographic analyses of the fracture surfaces of the specimens were performed to determine the fracture mechanism of the Ti6Al4V(ELI) impact specimens.Lehlohonolo Francis MonahengWillie Bouwer du PreezClaudia PoleseMDPI AGarticleimpact toughnessaviation industryadditive manufacturingTi6Al4V(ELI)two-stage heat treatmentMining engineering. MetallurgyTN1-997ENMetals, Vol 11, Iss 1736, p 1736 (2021)
institution DOAJ
collection DOAJ
language EN
topic impact toughness
aviation industry
additive manufacturing
Ti6Al4V(ELI)
two-stage heat treatment
Mining engineering. Metallurgy
TN1-997
spellingShingle impact toughness
aviation industry
additive manufacturing
Ti6Al4V(ELI)
two-stage heat treatment
Mining engineering. Metallurgy
TN1-997
Lehlohonolo Francis Monaheng
Willie Bouwer du Preez
Claudia Polese
Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment
description Laser powder bed fusion (L-PBF) has the potential to be applied in the production of titanium aircraft components with good mechanical properties, provided the technology has been qualified and accepted in the aviation industry. To achieve acceptance of the L-PBF technology in the aircraft industry, mechanical property data needed for the qualification process must be generated according to accepted testing standards. The impact toughness of Ti6Al4V extra low interstitial (ELI) specimens, produced through L-PBF followed by annealing, was investigated in this study. Charpy impact testing complying with American Standard Test Method (ASTM) E23 was performed with specimens annealed and conditioned at low temperature. On average, the toughness recorded for the specimens with 3D-printed and machined V-notches was 28 J and 31 J, respectively. These results are higher than the 24 J required in the aerospace industry. Finally, fractographic analyses of the fracture surfaces of the specimens were performed to determine the fracture mechanism of the Ti6Al4V(ELI) impact specimens.
format article
author Lehlohonolo Francis Monaheng
Willie Bouwer du Preez
Claudia Polese
author_facet Lehlohonolo Francis Monaheng
Willie Bouwer du Preez
Claudia Polese
author_sort Lehlohonolo Francis Monaheng
title Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment
title_short Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment
title_full Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment
title_fullStr Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment
title_full_unstemmed Towards Qualification in the Aviation Industry: Impact Toughness of Ti6Al4V(ELI) Specimens Produced through Laser Powder Bed Fusion Followed by Two-Stage Heat Treatment
title_sort towards qualification in the aviation industry: impact toughness of ti6al4v(eli) specimens produced through laser powder bed fusion followed by two-stage heat treatment
publisher MDPI AG
publishDate 2021
url https://doaj.org/article/674334bdf5f7459f96c657197e550eae
work_keys_str_mv AT lehlohonolofrancismonaheng towardsqualificationintheaviationindustryimpacttoughnessofti6al4velispecimensproducedthroughlaserpowderbedfusionfollowedbytwostageheattreatment
AT williebouwerdupreez towardsqualificationintheaviationindustryimpacttoughnessofti6al4velispecimensproducedthroughlaserpowderbedfusionfollowedbytwostageheattreatment
AT claudiapolese towardsqualificationintheaviationindustryimpacttoughnessofti6al4velispecimensproducedthroughlaserpowderbedfusionfollowedbytwostageheattreatment
_version_ 1718411261895507968