Details
Original language | English |
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Title of host publication | Superalloys 2024 |
Subtitle of host publication | Proceedings of the 15th International Symposium on Superalloys |
Editors | Jonathan Cormier, Ian Edmonds, Stephane Forsik, Paraskevas Kontis, Corey O’Connell, Timothy Smith, Akane Suzuki, Sammy Tin, Jian Zhang |
Publisher | Springer Science and Business Media Deutschland GmbH |
Pages | 971-983 |
Number of pages | 13 |
ISBN (electronic) | 978-3-031-63937-1 |
ISBN (print) | 9783031639364 |
Publication status | Published - 21 Aug 2024 |
Event | 15th International Symposium on Superalloys, ISS 2024 - Pennsylvania, United States Duration: 8 Sept 2024 → 12 Sept 2024 |
Publication series
Name | Minerals, Metals and Materials Series |
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ISSN (Print) | 2367-1181 |
ISSN (electronic) | 2367-1696 |
Abstract
Superior repairRepair technology is a principal driver for resource-effective operation in the aviation industry. Routine operation of aircraft engines exposes the turbine components to high stresses and high temperaturesHigh temperature. To withstand extreme operational conditions Ni-based superalloysNi- based superalloys are used to manufacture turbine components. A crucial factor in targeting the assurance of repairRepair reliability is improving the repairRepair braze gap strength. This study seeks to improve the braze repairRepair strength by optimising a novel superalloySuperalloys filler material. The superalloySuperalloys filler material acts as a complementary additiveAdditive that is blended with the braze alloy in powder form and improves the joint properties after brazing. The novel superalloySuperalloys filler was developed by materials simulationMaterials simulationusing the CALPHADCALculation of PHAse Diagrams (CALPHAD) (CALculation of PHAse Diagram) approach. Phase fieldPhase fieldmodellingModelling using MICRESS® was applied to study the brazing kinetics and microstructureMicrostructure evolution. The developed superalloySuperalloys filler was validated experimentally in respect to microstructureMicrostructure improvement and mechanical potential by tensile testing at service-equivalent temperature (871 °C). The application of the novel superalloySuperalloys filler shows an increase in ultimate tensile strength in comparison with a conventional braze blend.
Keywords
- Alloy development, Diffusion brazing, Materials simulation, Repair, Superalloys
ASJC Scopus subject areas
- Materials Science(all)
- Electronic, Optical and Magnetic Materials
- Energy(all)
- Energy Engineering and Power Technology
- Engineering(all)
- Mechanics of Materials
- Materials Science(all)
- Metals and Alloys
- Materials Science(all)
- Materials Chemistry
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Superalloys 2024: Proceedings of the 15th International Symposium on Superalloys. ed. / Jonathan Cormier; Ian Edmonds; Stephane Forsik; Paraskevas Kontis; Corey O’Connell; Timothy Smith; Akane Suzuki; Sammy Tin; Jian Zhang. Springer Science and Business Media Deutschland GmbH, 2024. p. 971-983 (Minerals, Metals and Materials Series).
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler
AU - Reker, Dirk Wilhelm
AU - Sowa, Roman
AU - Schwalbe, Caspar
AU - Boettger, Bernd
AU - Seidel, Frank
AU - Panella, Marco
AU - Moehwald, Kai
AU - Nicolaus, Martin
AU - Tillmann, Wolfgang
N1 - Publisher Copyright: © The Minerals, Metals & Materials Society 2024.
PY - 2024/8/21
Y1 - 2024/8/21
N2 - Superior repairRepair technology is a principal driver for resource-effective operation in the aviation industry. Routine operation of aircraft engines exposes the turbine components to high stresses and high temperaturesHigh temperature. To withstand extreme operational conditions Ni-based superalloysNi- based superalloys are used to manufacture turbine components. A crucial factor in targeting the assurance of repairRepair reliability is improving the repairRepair braze gap strength. This study seeks to improve the braze repairRepair strength by optimising a novel superalloySuperalloys filler material. The superalloySuperalloys filler material acts as a complementary additiveAdditive that is blended with the braze alloy in powder form and improves the joint properties after brazing. The novel superalloySuperalloys filler was developed by materials simulationMaterials simulationusing the CALPHADCALculation of PHAse Diagrams (CALPHAD) (CALculation of PHAse Diagram) approach. Phase fieldPhase fieldmodellingModelling using MICRESS® was applied to study the brazing kinetics and microstructureMicrostructure evolution. The developed superalloySuperalloys filler was validated experimentally in respect to microstructureMicrostructure improvement and mechanical potential by tensile testing at service-equivalent temperature (871 °C). The application of the novel superalloySuperalloys filler shows an increase in ultimate tensile strength in comparison with a conventional braze blend.
AB - Superior repairRepair technology is a principal driver for resource-effective operation in the aviation industry. Routine operation of aircraft engines exposes the turbine components to high stresses and high temperaturesHigh temperature. To withstand extreme operational conditions Ni-based superalloysNi- based superalloys are used to manufacture turbine components. A crucial factor in targeting the assurance of repairRepair reliability is improving the repairRepair braze gap strength. This study seeks to improve the braze repairRepair strength by optimising a novel superalloySuperalloys filler material. The superalloySuperalloys filler material acts as a complementary additiveAdditive that is blended with the braze alloy in powder form and improves the joint properties after brazing. The novel superalloySuperalloys filler was developed by materials simulationMaterials simulationusing the CALPHADCALculation of PHAse Diagrams (CALPHAD) (CALculation of PHAse Diagram) approach. Phase fieldPhase fieldmodellingModelling using MICRESS® was applied to study the brazing kinetics and microstructureMicrostructure evolution. The developed superalloySuperalloys filler was validated experimentally in respect to microstructureMicrostructure improvement and mechanical potential by tensile testing at service-equivalent temperature (871 °C). The application of the novel superalloySuperalloys filler shows an increase in ultimate tensile strength in comparison with a conventional braze blend.
KW - Alloy development
KW - Diffusion brazing
KW - Materials simulation
KW - Repair
KW - Superalloys
UR - http://www.scopus.com/inward/record.url?scp=85202767547&partnerID=8YFLogxK
U2 - 10.1007/978-3-031-63937-1_90
DO - 10.1007/978-3-031-63937-1_90
M3 - Conference contribution
AN - SCOPUS:85202767547
SN - 9783031639364
T3 - Minerals, Metals and Materials Series
SP - 971
EP - 983
BT - Superalloys 2024
A2 - Cormier, Jonathan
A2 - Edmonds, Ian
A2 - Forsik, Stephane
A2 - Kontis, Paraskevas
A2 - O’Connell, Corey
A2 - Smith, Timothy
A2 - Suzuki, Akane
A2 - Tin, Sammy
A2 - Zhang, Jian
PB - Springer Science and Business Media Deutschland GmbH
T2 - 15th International Symposium on Superalloys, ISS 2024
Y2 - 8 September 2024 through 12 September 2024
ER -