Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries

Novel joining methods are crucial for the aerospace industry to repair components damaged in the high stress, high cycle environment of the jet turbine engine. Powder interlayer bonding (PIB) is a novel joining technique that is being explored for use in the aerospace industry. PIB involves the use...

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Main Authors: Olivia Stanners, James Russell, Sean John, Helen M. Davies, Silvia Marchisio
Format: Article
Language:English
Published: MDPI AG 2021-04-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/14/8/2029
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spelling doaj-e007c254c0e048a29df9ab0089a053f22021-04-17T23:03:37ZengMDPI AGMaterials1996-19442021-04-01142029202910.3390/ma14082029Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar ChemistriesOlivia Stanners0James Russell1Sean John2Helen M. Davies3Silvia Marchisio4Institute of Structural Materials, Swansea University, Bay Campus, Swansea SA1 8EN, UKAdvanced Imaging of Materials Facility, College of Engineering, Swansea University, Bay Campus, Swansea SA1 8EN, UKInstitute of Structural Materials, Swansea University, Bay Campus, Swansea SA1 8EN, UKInstitute of Structural Materials, Swansea University, Bay Campus, Swansea SA1 8EN, UKRolls-Royce plc, P.O. Box 31, Derby DE24 8BJ, UKNovel joining methods are crucial for the aerospace industry to repair components damaged in the high stress, high cycle environment of the jet turbine engine. Powder interlayer bonding (PIB) is a novel joining technique that is being explored for use in the aerospace industry. PIB involves the use of a powder interlayer between two faying surfaces alongside a localised temperature gradient and compressive force to produce one joined workpiece. The use of a localised temperature gradient not only reduces the heat affected zone (HAZ) but also reduces the energy requirements for the process as only a small area of the component needs to be elevated in temperature. Nickel-based superalloys are commonly used in the gas turbine engine due to their superior mechanical properties that are maintained even under the most elevated temperatures experienced in the jet turbine engine. It is therefore essential these alloys can be easily repaired. Conventional joining methods such as friction welding have proved difficult for new generation nickel-based superalloys; therefore, there is much interest in PIB as an alternative repair technology. This study shows the potential of PIB to join dissimilar nickel-based superalloys: bonds with very little porosity were observed after only a short processing time.https://www.mdpi.com/1996-1944/14/8/2029powderinterlayerbondingjoiningnickel-based superalloys
collection DOAJ
language English
format Article
sources DOAJ
author Olivia Stanners
James Russell
Sean John
Helen M. Davies
Silvia Marchisio
spellingShingle Olivia Stanners
James Russell
Sean John
Helen M. Davies
Silvia Marchisio
Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries
Materials
powder
interlayer
bonding
joining
nickel-based superalloys
author_facet Olivia Stanners
James Russell
Sean John
Helen M. Davies
Silvia Marchisio
author_sort Olivia Stanners
title Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries
title_short Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries
title_full Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries
title_fullStr Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries
title_full_unstemmed Powder Interlayer Bonding of Nickel-Based Superalloys with Dissimilar Chemistries
title_sort powder interlayer bonding of nickel-based superalloys with dissimilar chemistries
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2021-04-01
description Novel joining methods are crucial for the aerospace industry to repair components damaged in the high stress, high cycle environment of the jet turbine engine. Powder interlayer bonding (PIB) is a novel joining technique that is being explored for use in the aerospace industry. PIB involves the use of a powder interlayer between two faying surfaces alongside a localised temperature gradient and compressive force to produce one joined workpiece. The use of a localised temperature gradient not only reduces the heat affected zone (HAZ) but also reduces the energy requirements for the process as only a small area of the component needs to be elevated in temperature. Nickel-based superalloys are commonly used in the gas turbine engine due to their superior mechanical properties that are maintained even under the most elevated temperatures experienced in the jet turbine engine. It is therefore essential these alloys can be easily repaired. Conventional joining methods such as friction welding have proved difficult for new generation nickel-based superalloys; therefore, there is much interest in PIB as an alternative repair technology. This study shows the potential of PIB to join dissimilar nickel-based superalloys: bonds with very little porosity were observed after only a short processing time.
topic powder
interlayer
bonding
joining
nickel-based superalloys
url https://www.mdpi.com/1996-1944/14/8/2029
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