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The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy
Materials & Design, Volume: 189, Start page: 108529
Swansea University Authors: David Lewis, Mark Whittaker
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DOI (Published version): 10.1016/j.matdes.2020.108529
Abstract
A number of thermal exposures were undertaken to determine the effect oxidation has on the fatigue lives of the nickel-based superalloy RR1000. The thermal exposures initially caused a considerable reduction in the fatigue lives with increasing oxidation. However, the longest exposure time resulted...
Published in: | Materials & Design |
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ISSN: | 0264-1275 |
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Elsevier BV
2020
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URI: | https://cronfa.swan.ac.uk/Record/cronfa53385 |
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2020-10-22T13:07:07.0299811 v2 53385 2020-01-29 The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy f52973928db300e06885ef9aabde1d63 David Lewis David Lewis true false a146c6d442cb2c466d096179f9ac97ca 0000-0002-5854-0726 Mark Whittaker Mark Whittaker true false 2020-01-29 A number of thermal exposures were undertaken to determine the effect oxidation has on the fatigue lives of the nickel-based superalloy RR1000. The thermal exposures initially caused a considerable reduction in the fatigue lives with increasing oxidation. However, the longest exposure time resulted in an S-N curve that lay between the shortest and mid length exposure. A range of analyses were undertaken to determine the presence of any mechanisms that could have caused this unexpected life increase; vacuum thermal exposures, small punch tensile, nanoindentation, microscopy and transmission Kikuchi diffraction. It was found that few of the mechanisms investigated were likely to have an effect on the change in life with the exceptions being; reduction in dislocation movement and crack deflection as a result of a recrystallised zone at the surface, variation in hardness of different regions due to a γ′ depleted plastic zone and a hard ceramic oxide, and reduced initiations due to the presence of a ‘healing’ chromium oxide scale. Notch fatigue tests were performed to determine the importance of the findings to components in service and it was found that the notch acted as the cause of crack initiation, effectively mitigating against the effects of the oxidation damage. Journal Article Materials & Design 189 108529 Elsevier BV 0264-1275 Ni-based superalloys; Fatigue behaviour; Micro-/nanoindentation; Profilometry; Transmission electron microscopy (TEM) 1 4 2020 2020-04-01 10.1016/j.matdes.2020.108529 COLLEGE NANME COLLEGE CODE Swansea University UKRI, EP/H022309/1 2020-10-22T13:07:07.0299811 2020-01-29T12:30:28.4219625 Faculty of Science and Engineering School of Engineering and Applied Sciences - Materials Science and Engineering David Lewis 1 R.G. Ding 2 Mark Whittaker 0000-0002-5854-0726 3 P.M. Mignanelli 4 M.C. Hardy 5 53385__16516__e42eb64d3d1b4987932e308ea4921de5.pdf 53385.pdf 2020-02-03T16:27:50.7955600 Output 3547266 application/pdf Version of Record true 2020-02-05T00:00:00.0000000 Released under the terms of a Creative Commons License (CC-BY). true eng http://creativecommons.org/licenses/by/4.0/ |
title |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy |
spellingShingle |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy David Lewis Mark Whittaker |
title_short |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy |
title_full |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy |
title_fullStr |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy |
title_full_unstemmed |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy |
title_sort |
The effect of oxidising thermal exposures on the fatigue properties of a polycrystalline powder metallurgy nickel-based superalloy |
author_id_str_mv |
f52973928db300e06885ef9aabde1d63 a146c6d442cb2c466d096179f9ac97ca |
author_id_fullname_str_mv |
f52973928db300e06885ef9aabde1d63_***_David Lewis a146c6d442cb2c466d096179f9ac97ca_***_Mark Whittaker |
author |
David Lewis Mark Whittaker |
author2 |
David Lewis R.G. Ding Mark Whittaker P.M. Mignanelli M.C. Hardy |
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Materials & Design |
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189 |
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108529 |
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2020 |
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Swansea University |
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0264-1275 |
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10.1016/j.matdes.2020.108529 |
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Elsevier BV |
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Faculty of Science and Engineering |
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description |
A number of thermal exposures were undertaken to determine the effect oxidation has on the fatigue lives of the nickel-based superalloy RR1000. The thermal exposures initially caused a considerable reduction in the fatigue lives with increasing oxidation. However, the longest exposure time resulted in an S-N curve that lay between the shortest and mid length exposure. A range of analyses were undertaken to determine the presence of any mechanisms that could have caused this unexpected life increase; vacuum thermal exposures, small punch tensile, nanoindentation, microscopy and transmission Kikuchi diffraction. It was found that few of the mechanisms investigated were likely to have an effect on the change in life with the exceptions being; reduction in dislocation movement and crack deflection as a result of a recrystallised zone at the surface, variation in hardness of different regions due to a γ′ depleted plastic zone and a hard ceramic oxide, and reduced initiations due to the presence of a ‘healing’ chromium oxide scale. Notch fatigue tests were performed to determine the importance of the findings to components in service and it was found that the notch acted as the cause of crack initiation, effectively mitigating against the effects of the oxidation damage. |
published_date |
2020-04-01T07:52:04Z |
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1821391112743419904 |
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11.048042 |