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Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging
Materials Science and Engineering: A, Volume: 621, Pages: 265 - 271
Swansea University Author: Karen Perkins
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Copyright 2014 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/3.0/)
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DOI (Published version): 10.1016/j.msea.2014.10.071
Abstract
The next generation of aerospace gas turbine engines need to operate at higher temperatures and stresses to improve their efficiency and reduce emissions. These operating conditions are beyond the capability of existing nickel-base superalloys, requiring the development of new high temperature mater...
Published in: | Materials Science and Engineering: A |
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ISSN: | 0921-5093 |
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2015
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<?xml version="1.0"?><rfc1807><datestamp>2020-09-22T10:28:06.1197938</datestamp><bib-version>v2</bib-version><id>19496</id><entry>2014-11-24</entry><title>Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging</title><swanseaauthors><author><sid>f866eaa2d8f163d2b4e99259966427c8</sid><ORCID>0000-0001-5826-9705</ORCID><firstname>Karen</firstname><surname>Perkins</surname><name>Karen Perkins</name><active>true</active><ethesisStudent>false</ethesisStudent></author></swanseaauthors><date>2014-11-24</date><deptcode>EEN</deptcode><abstract>The next generation of aerospace gas turbine engines need to operate at higher temperatures and stresses to improve their efficiency and reduce emissions. These operating conditions are beyond the capability of existing nickel-base superalloys, requiring the development of new high temperature materials. Controlling the microstructures of these new materials is key to obtaining the required properties and, therefore, it is critical to understand how these alloys respond to processing and heat treatment. Here, the microstructural evolution of V207M, a new δ containing, nickel-base superalloy, has been investigated following heat treatment and forging. The solvus temperatures of the γ′ and δ phases, determined by differential scanning calorimetry and microscopy, were found to be ~985 and ~1060 °C respectively. Isothermal forging of the alloy was conducted at 1000, 1050 and 1100 °C, corresponding to different volume fractions of retained δ. Considerable softening was observed prior to steady state flow when forging at 1000 °C, whilst only steady state flow occurred at 1050 and 1100 °C. The steady state flow process was believed to be dominated by dynamic recovery in the γ phase, with an activation energy of 407 kJmol−1. Samples that exhibited flow softening also showed a significant change in the orientation of the δ precipitates, preferentially aligning normal to the forging axis, and this reorientation was thought to be the cause of the observed flow softening.</abstract><type>Journal Article</type><journal>Materials Science and Engineering: A</journal><volume>621</volume><paginationStart>265</paginationStart><paginationEnd>271</paginationEnd><publisher/><issnPrint>0921-5093</issnPrint><keywords/><publishedDay>5</publishedDay><publishedMonth>1</publishedMonth><publishedYear>2015</publishedYear><publishedDate>2015-01-05</publishedDate><doi>10.1016/j.msea.2014.10.071</doi><url/><notes>& 2014 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY license(http://creativecommons.org/licenses/by/3.0/).</notes><college>COLLEGE NANME</college><department>Engineering</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>EEN</DepartmentCode><institution>Swansea University</institution><degreesponsorsfunders>EPSRC</degreesponsorsfunders><apcterm/><lastEdited>2020-09-22T10:28:06.1197938</lastEdited><Created>2014-11-24T14:22:53.8472143</Created><path><level id="1">Faculty of Science and Engineering</level><level id="2">School of Engineering and Applied Sciences - Uncategorised</level></path><authors><author><firstname>P.M.</firstname><surname>Mignanelli</surname><order>1</order></author><author><firstname>N.G.</firstname><surname>Jones</surname><order>2</order></author><author><firstname>K.M.</firstname><surname>Perkins</surname><order>3</order></author><author><firstname>M.C.</firstname><surname>Hardy</surname><order>4</order></author><author><firstname>H.J.</firstname><surname>Stone</surname><order>5</order></author><author><firstname>Karen</firstname><surname>Perkins</surname><orcid>0000-0001-5826-9705</orcid><order>6</order></author></authors><documents><document><filename>0019496-20072016163001.pdf</filename><originalFilename>1-s2.0-S0921509314013252-main.pdf</originalFilename><uploaded>2016-07-20T16:30:01.8930000</uploaded><type>Output</type><contentLength>3184292</contentLength><contentType>application/pdf</contentType><version>Version of Record</version><cronfaStatus>true</cronfaStatus><embargoDate>2016-07-20T00:00:00.0000000</embargoDate><documentNotes>Copyright 2014 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/3.0/)</documentNotes><copyrightCorrect>true</copyrightCorrect></document></documents><OutputDurs/></rfc1807> |
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2020-09-22T10:28:06.1197938 v2 19496 2014-11-24 Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging f866eaa2d8f163d2b4e99259966427c8 0000-0001-5826-9705 Karen Perkins Karen Perkins true false 2014-11-24 EEN The next generation of aerospace gas turbine engines need to operate at higher temperatures and stresses to improve their efficiency and reduce emissions. These operating conditions are beyond the capability of existing nickel-base superalloys, requiring the development of new high temperature materials. Controlling the microstructures of these new materials is key to obtaining the required properties and, therefore, it is critical to understand how these alloys respond to processing and heat treatment. Here, the microstructural evolution of V207M, a new δ containing, nickel-base superalloy, has been investigated following heat treatment and forging. The solvus temperatures of the γ′ and δ phases, determined by differential scanning calorimetry and microscopy, were found to be ~985 and ~1060 °C respectively. Isothermal forging of the alloy was conducted at 1000, 1050 and 1100 °C, corresponding to different volume fractions of retained δ. Considerable softening was observed prior to steady state flow when forging at 1000 °C, whilst only steady state flow occurred at 1050 and 1100 °C. The steady state flow process was believed to be dominated by dynamic recovery in the γ phase, with an activation energy of 407 kJmol−1. Samples that exhibited flow softening also showed a significant change in the orientation of the δ precipitates, preferentially aligning normal to the forging axis, and this reorientation was thought to be the cause of the observed flow softening. Journal Article Materials Science and Engineering: A 621 265 271 0921-5093 5 1 2015 2015-01-05 10.1016/j.msea.2014.10.071 & 2014 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY license(http://creativecommons.org/licenses/by/3.0/). COLLEGE NANME Engineering COLLEGE CODE EEN Swansea University EPSRC 2020-09-22T10:28:06.1197938 2014-11-24T14:22:53.8472143 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised P.M. Mignanelli 1 N.G. Jones 2 K.M. Perkins 3 M.C. Hardy 4 H.J. Stone 5 Karen Perkins 0000-0001-5826-9705 6 0019496-20072016163001.pdf 1-s2.0-S0921509314013252-main.pdf 2016-07-20T16:30:01.8930000 Output 3184292 application/pdf Version of Record true 2016-07-20T00:00:00.0000000 Copyright 2014 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/3.0/) true |
title |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging |
spellingShingle |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging Karen Perkins |
title_short |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging |
title_full |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging |
title_fullStr |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging |
title_full_unstemmed |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging |
title_sort |
Microstructural evolution of a delta containing nickel-base superalloy during heat treatment and isothermal forging |
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f866eaa2d8f163d2b4e99259966427c8 |
author_id_fullname_str_mv |
f866eaa2d8f163d2b4e99259966427c8_***_Karen Perkins |
author |
Karen Perkins |
author2 |
P.M. Mignanelli N.G. Jones K.M. Perkins M.C. Hardy H.J. Stone Karen Perkins |
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Materials Science and Engineering: A |
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621 |
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2015 |
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Swansea University |
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0921-5093 |
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10.1016/j.msea.2014.10.071 |
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Faculty of Science and Engineering |
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description |
The next generation of aerospace gas turbine engines need to operate at higher temperatures and stresses to improve their efficiency and reduce emissions. These operating conditions are beyond the capability of existing nickel-base superalloys, requiring the development of new high temperature materials. Controlling the microstructures of these new materials is key to obtaining the required properties and, therefore, it is critical to understand how these alloys respond to processing and heat treatment. Here, the microstructural evolution of V207M, a new δ containing, nickel-base superalloy, has been investigated following heat treatment and forging. The solvus temperatures of the γ′ and δ phases, determined by differential scanning calorimetry and microscopy, were found to be ~985 and ~1060 °C respectively. Isothermal forging of the alloy was conducted at 1000, 1050 and 1100 °C, corresponding to different volume fractions of retained δ. Considerable softening was observed prior to steady state flow when forging at 1000 °C, whilst only steady state flow occurred at 1050 and 1100 °C. The steady state flow process was believed to be dominated by dynamic recovery in the γ phase, with an activation energy of 407 kJmol−1. Samples that exhibited flow softening also showed a significant change in the orientation of the δ precipitates, preferentially aligning normal to the forging axis, and this reorientation was thought to be the cause of the observed flow softening. |
published_date |
2015-01-05T03:22:53Z |
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1763750732050202624 |
score |
11.037581 |