Tensile Behavior of Long-term Aged Nickel-base Superalloy
The microstructural change of directionally solidified nickel-base superalloy which was aged at 900 °C for 1500 hours and tensile behavior at different temperatures were investigated by scanning electron microscope (SEM) and transmission electron microscope (TEM). γ′ phase of the alloy coarsens and...
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Online Access: | https://doi.org/10.1515/htmp-2014-0070 |
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doaj-890367ac637f487b9d086aee9a9b1e9b2021-09-06T19:19:53ZengDe GruyterHigh Temperature Materials and Processes0334-64552191-03242015-07-0134439539810.1515/htmp-2014-0070Tensile Behavior of Long-term Aged Nickel-base SuperalloyXia P. C.0Chen F. W.1Xie K.2Yu J. J.3School of Materials Science and Engineering, Shandong University of Science and Technology, Qingdao 266590, ChinaSchool of Materials Science and Engineering, Shandong University of Science and Technology, Qingdao 266590, ChinaSchool of Materials Science and Engineering, Shandong University of Science and Technology, Qingdao 266590, ChinaInstitute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, ChinaThe microstructural change of directionally solidified nickel-base superalloy which was aged at 900 °C for 1500 hours and tensile behavior at different temperatures were investigated by scanning electron microscope (SEM) and transmission electron microscope (TEM). γ′ phase of the alloy coarsens and rafts in the course of aged treatment. The driving force of rafting is the decrease of interface energy and elastic strain energy. The stress of aged alloy increases slightly with the testing temperature. This arises from a few dislocations shearing the γ′ precipitates. There is a peak stress value at 760 °C, which is attributed to the high strength of the γ′ phase, the homogeneous deformation structure, and dislocation-γ′ precipitate and dislocation–dislocation interactions. The stress then decreases rapidly with increased temperature. The low stress of the γ′ phase and γ′ rafting at high temperature contribute to the drop of alloy strength. The change of elongation is inverse to that of the stress.https://doi.org/10.1515/htmp-2014-0070superalloyagingγ′ phasetensile behaviordislocationcoarsening and rafting81.70.bt |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Xia P. C. Chen F. W. Xie K. Yu J. J. |
spellingShingle |
Xia P. C. Chen F. W. Xie K. Yu J. J. Tensile Behavior of Long-term Aged Nickel-base Superalloy High Temperature Materials and Processes superalloy aging γ′ phase tensile behavior dislocation coarsening and rafting 81.70.bt |
author_facet |
Xia P. C. Chen F. W. Xie K. Yu J. J. |
author_sort |
Xia P. C. |
title |
Tensile Behavior of Long-term Aged Nickel-base Superalloy |
title_short |
Tensile Behavior of Long-term Aged Nickel-base Superalloy |
title_full |
Tensile Behavior of Long-term Aged Nickel-base Superalloy |
title_fullStr |
Tensile Behavior of Long-term Aged Nickel-base Superalloy |
title_full_unstemmed |
Tensile Behavior of Long-term Aged Nickel-base Superalloy |
title_sort |
tensile behavior of long-term aged nickel-base superalloy |
publisher |
De Gruyter |
series |
High Temperature Materials and Processes |
issn |
0334-6455 2191-0324 |
publishDate |
2015-07-01 |
description |
The microstructural change of directionally solidified nickel-base superalloy which was aged at 900 °C for 1500 hours and tensile behavior at different temperatures were investigated by scanning electron microscope (SEM) and transmission electron microscope (TEM). γ′ phase of the alloy coarsens and rafts in the course of aged treatment. The driving force of rafting is the decrease of interface energy and elastic strain energy. The stress of aged alloy increases slightly with the testing temperature. This arises from a few dislocations shearing the γ′ precipitates. There is a peak stress value at 760 °C, which is attributed to the high strength of the γ′ phase, the homogeneous deformation structure, and dislocation-γ′ precipitate and dislocation–dislocation interactions. The stress then decreases rapidly with increased temperature. The low stress of the γ′ phase and γ′ rafting at high temperature contribute to the drop of alloy strength. The change of elongation is inverse to that of the stress. |
topic |
superalloy aging γ′ phase tensile behavior dislocation coarsening and rafting 81.70.bt |
url |
https://doi.org/10.1515/htmp-2014-0070 |
work_keys_str_mv |
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