Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy
The age hardening response of a high-purity Al–4Cu–1Li–0.25Mn alloy (wt. %) during isothermal aging without and with an applied external load was investigated. Plate shaped nanometer size T1 (Al2CuLi) and θ′ (Al2Cu) hardening phases were formed. The...
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doaj-475a54d419dc4a32a8c01833da3fbe412020-11-25T00:17:16ZengMDPI AGMaterials1996-19442018-12-011213010.3390/ma12010030ma12010030Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn AlloyInes Häusler0Reza Darvishi Kamachali1Walid Hetaba2Birgit Skrotzki3Federal Institute for Materials Research and Testing (BAM), Department 5: Materials Engineering, 12205 Berlin, GermanyMax-Planck-Institut für Eisenforschung GmbH, Max-Planck-Straße 1, 40237 Düsseldorf, GermanyDepartment of Inorganic Chemistry, Fritz-Haber-Institute of the Max-Planck-Gesellschaft, 14195 Berlin, GermanyFederal Institute for Materials Research and Testing (BAM), Department 5: Materials Engineering, 12205 Berlin, GermanyThe age hardening response of a high-purity Al–4Cu–1Li–0.25Mn alloy (wt. %) during isothermal aging without and with an applied external load was investigated. Plate shaped nanometer size T1 (Al2CuLi) and θ′ (Al2Cu) hardening phases were formed. The precipitates were analyzed with respect to the development of their structure, size, number density, volume fraction and associated transformation strains by conducting transmission electron microscopy (TEM) and scanning transmission electron microscopy (STEM) studies in combination with geometrical phase analysis (GPA). Special attention was paid to the thickening of T1 phase. Two elementary types of single-layer T1 precipitate, one with a Li-rich (Type 1) and another with an Al-rich (Defect Type 1) central layer, were identified. The results show that the Defect Type 1 structure can act as a precursor for the Type 1 structure. The thickening of T1 precipitates occurs by alternative stacking of these two elementary structures. The thickening mechanism was analyzed based on the magnitude of strain associated with the precipitation transformation normal to its habit plane. Long-term aging and aging under load resulted in thicker and structurally defected T1 precipitates. Several types of defected precipitates were characterized and discussed. For θ′ precipitates, a ledge mechanism of thickening was observed. Compared to the normal aging, an external load applied to the peak aged state leads to small variations in the average sizes and volume fractions of the precipitates.http://www.mdpi.com/1996-1944/12/1/30Al-Cu-Li-alloyprecipitationT1 precipitatemicrostructure evolutionthickeningcreepvolume fractionnumber densitystrain difference |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Ines Häusler Reza Darvishi Kamachali Walid Hetaba Birgit Skrotzki |
spellingShingle |
Ines Häusler Reza Darvishi Kamachali Walid Hetaba Birgit Skrotzki Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy Materials Al-Cu-Li-alloy precipitation T1 precipitate microstructure evolution thickening creep volume fraction number density strain difference |
author_facet |
Ines Häusler Reza Darvishi Kamachali Walid Hetaba Birgit Skrotzki |
author_sort |
Ines Häusler |
title |
Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy |
title_short |
Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy |
title_full |
Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy |
title_fullStr |
Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy |
title_full_unstemmed |
Thickening of T1 Precipitates during Aging of a High Purity Al–4Cu–1Li–0.25Mn Alloy |
title_sort |
thickening of t1 precipitates during aging of a high purity al–4cu–1li–0.25mn alloy |
publisher |
MDPI AG |
series |
Materials |
issn |
1996-1944 |
publishDate |
2018-12-01 |
description |
The age hardening response of a high-purity Al–4Cu–1Li–0.25Mn alloy (wt. %) during isothermal aging without and with an applied external load was investigated. Plate shaped nanometer size T1 (Al2CuLi) and θ′ (Al2Cu) hardening phases were formed. The precipitates were analyzed with respect to the development of their structure, size, number density, volume fraction and associated transformation strains by conducting transmission electron microscopy (TEM) and scanning transmission electron microscopy (STEM) studies in combination with geometrical phase analysis (GPA). Special attention was paid to the thickening of T1 phase. Two elementary types of single-layer T1 precipitate, one with a Li-rich (Type 1) and another with an Al-rich (Defect Type 1) central layer, were identified. The results show that the Defect Type 1 structure can act as a precursor for the Type 1 structure. The thickening of T1 precipitates occurs by alternative stacking of these two elementary structures. The thickening mechanism was analyzed based on the magnitude of strain associated with the precipitation transformation normal to its habit plane. Long-term aging and aging under load resulted in thicker and structurally defected T1 precipitates. Several types of defected precipitates were characterized and discussed. For θ′ precipitates, a ledge mechanism of thickening was observed. Compared to the normal aging, an external load applied to the peak aged state leads to small variations in the average sizes and volume fractions of the precipitates. |
topic |
Al-Cu-Li-alloy precipitation T1 precipitate microstructure evolution thickening creep volume fraction number density strain difference |
url |
http://www.mdpi.com/1996-1944/12/1/30 |
work_keys_str_mv |
AT ineshausler thickeningoft1precipitatesduringagingofahighpurityal4cu1li025mnalloy AT rezadarvishikamachali thickeningoft1precipitatesduringagingofahighpurityal4cu1li025mnalloy AT walidhetaba thickeningoft1precipitatesduringagingofahighpurityal4cu1li025mnalloy AT birgitskrotzki thickeningoft1precipitatesduringagingofahighpurityal4cu1li025mnalloy |
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1725380000293584896 |