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The joining of gamma titanium aluminides via the powder interlayer bonding method
The International Journal of Advanced Manufacturing Technology, Volume: 109, Issue: 7-8, Pages: 2049 - 2054
Swansea University Authors: Peter Davies, Helen Davies , Daniel Britton
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DOI (Published version): 10.1007/s00170-020-05725-9
Abstract
Powder interlayer bonding (PIB) is a joining technique originally developed to enable high-integrity repairs of aerospace components. The technique has previously been employed for the joining of titanium and nickel alloys utilised in the aerospace industry. This study expands on the application of...
Published in: | The International Journal of Advanced Manufacturing Technology |
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ISSN: | 0268-3768 1433-3015 |
Published: |
Springer Science and Business Media LLC
2020
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URI: | https://cronfa.swan.ac.uk/Record/cronfa54683 |
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2021-12-01T13:59:28.4038446 v2 54683 2020-07-10 The joining of gamma titanium aluminides via the powder interlayer bonding method 6001f4a98b5ed1259d64498333697ca5 Peter Davies Peter Davies true false a5277aa17f0f10a481da9e9751ccaeef 0000-0003-4838-9572 Helen Davies Helen Davies true false 09da4807d902e139e89b80e6cd3e8fd5 Daniel Britton Daniel Britton true false 2020-07-10 EAAS Powder interlayer bonding (PIB) is a joining technique originally developed to enable high-integrity repairs of aerospace components. The technique has previously been employed for the joining of titanium and nickel alloys utilised in the aerospace industry. This study expands on the application of the novel joining technique known as powder interlayer bonding (PIB), to the bonding of γ titanium aluminide (TiAl) material. PIB has been used to facilitate high-integrity joints in gamma titanium aluminides (TiAl), where full densification of the joint was achieved. The PIB technique described here used a metallic powder interlayer between the two faying surfaces of γ TiAl specimens. Bonds were formed in an inert atmosphere under induction heating. The PIB technique proved capable of producing high-integrity bonds in terms of microstructural evaluation, with very limited porosity retained after the bonding cycle. A brittle Ti2Al phase can be produced with heavily oxidised powder which is susceptible to cracking and will negatively affect mechanical properties. Journal Article The International Journal of Advanced Manufacturing Technology 109 7-8 2049 2054 Springer Science and Business Media LLC 0268-3768 1433-3015 Powder interlayer bonding (PIB); Gamma titanium aluminides 1 8 2020 2020-08-01 10.1007/s00170-020-05725-9 COLLEGE NANME Engineering and Applied Sciences School COLLEGE CODE EAAS Swansea University SU Library paid the OA fee (TA Institutional Deal) EPSRC EP/R511614/1 2021-12-01T13:59:28.4038446 2020-07-10T09:09:03.3070824 Faculty of Science and Engineering School of Engineering and Applied Sciences - Materials Science and Engineering Peter Davies 1 Helen Davies 0000-0003-4838-9572 2 I. Watkins 3 Daniel Britton 4 54683__17842__295fe2681a9b447cb9eaf3105d32c3f5.pdf 54683.pdf 2020-08-03T17:27:06.6422336 Output 1189005 application/pdf Version of Record true Released under the terms of a Creative Commons Attribution 4.0 International License (CC-BY). true English http://creativecommons.org/licenses/by/4.0/ |
title |
The joining of gamma titanium aluminides via the powder interlayer bonding method |
spellingShingle |
The joining of gamma titanium aluminides via the powder interlayer bonding method Peter Davies Helen Davies Daniel Britton |
title_short |
The joining of gamma titanium aluminides via the powder interlayer bonding method |
title_full |
The joining of gamma titanium aluminides via the powder interlayer bonding method |
title_fullStr |
The joining of gamma titanium aluminides via the powder interlayer bonding method |
title_full_unstemmed |
The joining of gamma titanium aluminides via the powder interlayer bonding method |
title_sort |
The joining of gamma titanium aluminides via the powder interlayer bonding method |
author_id_str_mv |
6001f4a98b5ed1259d64498333697ca5 a5277aa17f0f10a481da9e9751ccaeef 09da4807d902e139e89b80e6cd3e8fd5 |
author_id_fullname_str_mv |
6001f4a98b5ed1259d64498333697ca5_***_Peter Davies a5277aa17f0f10a481da9e9751ccaeef_***_Helen Davies 09da4807d902e139e89b80e6cd3e8fd5_***_Daniel Britton |
author |
Peter Davies Helen Davies Daniel Britton |
author2 |
Peter Davies Helen Davies I. Watkins Daniel Britton |
format |
Journal article |
container_title |
The International Journal of Advanced Manufacturing Technology |
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109 |
container_issue |
7-8 |
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2049 |
publishDate |
2020 |
institution |
Swansea University |
issn |
0268-3768 1433-3015 |
doi_str_mv |
10.1007/s00170-020-05725-9 |
publisher |
Springer Science and Business Media LLC |
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Faculty of Science and Engineering |
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School of Engineering and Applied Sciences - Materials Science and Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Materials Science and Engineering |
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description |
Powder interlayer bonding (PIB) is a joining technique originally developed to enable high-integrity repairs of aerospace components. The technique has previously been employed for the joining of titanium and nickel alloys utilised in the aerospace industry. This study expands on the application of the novel joining technique known as powder interlayer bonding (PIB), to the bonding of γ titanium aluminide (TiAl) material. PIB has been used to facilitate high-integrity joints in gamma titanium aluminides (TiAl), where full densification of the joint was achieved. The PIB technique described here used a metallic powder interlayer between the two faying surfaces of γ TiAl specimens. Bonds were formed in an inert atmosphere under induction heating. The PIB technique proved capable of producing high-integrity bonds in terms of microstructural evaluation, with very limited porosity retained after the bonding cycle. A brittle Ti2Al phase can be produced with heavily oxidised powder which is susceptible to cracking and will negatively affect mechanical properties. |
published_date |
2020-08-01T07:55:24Z |
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1821391322392559616 |
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11.047523 |