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Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys
MATEC Web of Conferences, Volume: 165, Start page: 02003
Swansea University Authors: Robert Lancaster , Spencer Jeffs
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DOI (Published version): 10.1051/matecconf/201816502003
Abstract
Additive layer manufacturing (ALM) processes are becoming increasingly prevalent in the aerospace industry as design engineers look to profit from the numerous advantages that these advanced techniques can offer. However, given the safety critical nature and arduous operating conditions to which the...
Published in: | MATEC Web of Conferences |
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ISSN: | 2261-236X |
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2018
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URI: | https://cronfa.swan.ac.uk/Record/cronfa40700 |
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2018-09-04T10:42:58.0328959 v2 40700 2018-06-13 Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys e1a1b126acd3e4ff734691ec34967f29 0000-0002-1365-6944 Robert Lancaster Robert Lancaster true false 6ff76d567df079d8bf299990849c3d8f 0000-0002-2819-9651 Spencer Jeffs Spencer Jeffs true false 2018-06-13 MTLS Additive layer manufacturing (ALM) processes are becoming increasingly prevalent in the aerospace industry as design engineers look to profit from the numerous advantages that these advanced techniques can offer. However, given the safety critical nature and arduous operating conditions to which these components will be exposed to whilst in service, it is essential that the mechanical properties of such structures are fully understood. Transient microstructures are a typical characteristic of ALM components and resulting from the thermal cycles that occur during the build operation. Those microstructures make any mechanical assessment an involved procedure when assessing the process variables for any given parameter set. A useful mechanical test technique is small-scale testing, in particular, the small punch (SP) test. SP testing is capable of localised sampling of a larger scale component and presents an attractive option to mechanically assess complex parts with representative geometries, that would not be possible using more conventional uniaxial test approaches. This paper will present the recent development of a small-scale testing methodology capable of inducing fatigue damage and a series of novel tests performed on different variants of Ti-6Al-4V. Journal Article MATEC Web of Conferences 165 02003 2261-236X 31 12 2018 2018-12-31 10.1051/matecconf/201816502003 COLLEGE NANME Materials Science and Engineering COLLEGE CODE MTLS Swansea University 2018-09-04T10:42:58.0328959 2018-06-13T12:32:14.6619564 Faculty of Science and Engineering School of Engineering and Applied Sciences - Materials Science and Engineering Robert Lancaster 0000-0002-1365-6944 1 Henry Illsley 2 Spencer Jeffs 0000-0002-2819-9651 3 Roger Hurst 4 Gavin Baxter 5 0040700-13062018123505.pdf lancaster2018(2).pdf 2018-06-13T12:35:05.5000000 Output 802364 application/pdf Version of Record true 2018-06-13T00:00:00.0000000 true eng |
title |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys |
spellingShingle |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys Robert Lancaster Spencer Jeffs |
title_short |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys |
title_full |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys |
title_fullStr |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys |
title_full_unstemmed |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys |
title_sort |
Application of the small punch test to determine the fatigue properties of additive manufactured aerospace alloys |
author_id_str_mv |
e1a1b126acd3e4ff734691ec34967f29 6ff76d567df079d8bf299990849c3d8f |
author_id_fullname_str_mv |
e1a1b126acd3e4ff734691ec34967f29_***_Robert Lancaster 6ff76d567df079d8bf299990849c3d8f_***_Spencer Jeffs |
author |
Robert Lancaster Spencer Jeffs |
author2 |
Robert Lancaster Henry Illsley Spencer Jeffs Roger Hurst Gavin Baxter |
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Journal article |
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MATEC Web of Conferences |
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165 |
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02003 |
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2018 |
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Swansea University |
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2261-236X |
doi_str_mv |
10.1051/matecconf/201816502003 |
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Faculty of Science and Engineering |
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Faculty of Science and Engineering |
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Faculty of Science and Engineering |
department_str |
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 |
Additive layer manufacturing (ALM) processes are becoming increasingly prevalent in the aerospace industry as design engineers look to profit from the numerous advantages that these advanced techniques can offer. However, given the safety critical nature and arduous operating conditions to which these components will be exposed to whilst in service, it is essential that the mechanical properties of such structures are fully understood. Transient microstructures are a typical characteristic of ALM components and resulting from the thermal cycles that occur during the build operation. Those microstructures make any mechanical assessment an involved procedure when assessing the process variables for any given parameter set. A useful mechanical test technique is small-scale testing, in particular, the small punch (SP) test. SP testing is capable of localised sampling of a larger scale component and presents an attractive option to mechanically assess complex parts with representative geometries, that would not be possible using more conventional uniaxial test approaches. This paper will present the recent development of a small-scale testing methodology capable of inducing fatigue damage and a series of novel tests performed on different variants of Ti-6Al-4V. |
published_date |
2018-12-31T03:51:48Z |
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1763752551263502336 |
score |
11.037603 |