Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging

The Ti 17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) alloy is used in the first stages of engine compressors, at temperatures up to 450°C. However, its use in structural parts such as engine pylons is more prospective and raises the question of damage tolerance. As the engine pylon environment involves prolonged expo...

Full description

Bibliographic Details
Main Authors: SASAKI Layla, HENAFF Gilbert, ARZAGHI Mandana, VILLECHAISE Patrick, HEMERY Samuel, DELFOSSE Jérôme
Format: Article
Language:English
Published: EDP Sciences 2020-01-01
Series:MATEC Web of Conferences
Online Access:https://www.matec-conferences.org/articles/matecconf/pdf/2020/17/matecconf_ti2019_06008.pdf
id doaj-0e57f20cfa494d8a8c9629ab8964551b
record_format Article
spelling doaj-0e57f20cfa494d8a8c9629ab8964551b2021-08-11T12:58:01ZengEDP SciencesMATEC Web of Conferences2261-236X2020-01-013210600810.1051/matecconf/202032106008matecconf_ti2019_06008Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term agingSASAKI Layla0HENAFF Gilbert1ARZAGHI Mandana2VILLECHAISE Patrick3HEMERY Samuel4DELFOSSE Jérôme5Pprime Institute UPR 3346 CNRS, ENSMA - Université de Poitiers, Department of Mechanics and Physics of MaterialsPprime Institute UPR 3346 CNRS, ENSMA - Université de Poitiers, Department of Mechanics and Physics of MaterialsPprime Institute UPR 3346 CNRS, ENSMA - Université de Poitiers, Department of Mechanics and Physics of MaterialsPprime Institute UPR 3346 CNRS, ENSMA - Université de Poitiers, Department of Mechanics and Physics of MaterialsPprime Institute UPR 3346 CNRS, ENSMA - Université de Poitiers, Department of Mechanics and Physics of MaterialsAirbus Group InnovationsThe Ti 17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) alloy is used in the first stages of engine compressors, at temperatures up to 450°C. However, its use in structural parts such as engine pylons is more prospective and raises the question of damage tolerance. As the engine pylon environment involves prolonged exposures to high temperatures, the impact of aging on mechanical properties has also to be taken in account. In this work, the consequences of a long-term aging (up to 10 000 h at 450°C) on the mechanical resistance of a Ti 17 alloy are examined at different scales, from macroscopic fatigue crack growth tests to in-situ tensile tests performed on micro samples in a SEM. The detrimental effect of aging on the mechanical properties of the Ti 17 alloy was then discussed in the light of damage mechanisms analysis and embrittlement kinetics.https://www.matec-conferences.org/articles/matecconf/pdf/2020/17/matecconf_ti2019_06008.pdf
collection DOAJ
language English
format Article
sources DOAJ
author SASAKI Layla
HENAFF Gilbert
ARZAGHI Mandana
VILLECHAISE Patrick
HEMERY Samuel
DELFOSSE Jérôme
spellingShingle SASAKI Layla
HENAFF Gilbert
ARZAGHI Mandana
VILLECHAISE Patrick
HEMERY Samuel
DELFOSSE Jérôme
Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging
MATEC Web of Conferences
author_facet SASAKI Layla
HENAFF Gilbert
ARZAGHI Mandana
VILLECHAISE Patrick
HEMERY Samuel
DELFOSSE Jérôme
author_sort SASAKI Layla
title Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging
title_short Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging
title_full Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging
title_fullStr Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging
title_full_unstemmed Damage mechanisms and embrittlement kinetics in a β-rich Ti 17 alloy after long term aging
title_sort damage mechanisms and embrittlement kinetics in a β-rich ti 17 alloy after long term aging
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2020-01-01
description The Ti 17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) alloy is used in the first stages of engine compressors, at temperatures up to 450°C. However, its use in structural parts such as engine pylons is more prospective and raises the question of damage tolerance. As the engine pylon environment involves prolonged exposures to high temperatures, the impact of aging on mechanical properties has also to be taken in account. In this work, the consequences of a long-term aging (up to 10 000 h at 450°C) on the mechanical resistance of a Ti 17 alloy are examined at different scales, from macroscopic fatigue crack growth tests to in-situ tensile tests performed on micro samples in a SEM. The detrimental effect of aging on the mechanical properties of the Ti 17 alloy was then discussed in the light of damage mechanisms analysis and embrittlement kinetics.
url https://www.matec-conferences.org/articles/matecconf/pdf/2020/17/matecconf_ti2019_06008.pdf
work_keys_str_mv AT sasakilayla damagemechanismsandembrittlementkineticsinabrichti17alloyafterlongtermaging
AT henaffgilbert damagemechanismsandembrittlementkineticsinabrichti17alloyafterlongtermaging
AT arzaghimandana damagemechanismsandembrittlementkineticsinabrichti17alloyafterlongtermaging
AT villechaisepatrick damagemechanismsandembrittlementkineticsinabrichti17alloyafterlongtermaging
AT hemerysamuel damagemechanismsandembrittlementkineticsinabrichti17alloyafterlongtermaging
AT delfossejerome damagemechanismsandembrittlementkineticsinabrichti17alloyafterlongtermaging
_version_ 1721211138551578624