Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autoren

Organisationseinheiten

Externe Organisationen

  • MTU Maintenance
  • Technische Universität Dortmund
  • MTU Aero Engines Polska
  • MTU Maintenance GmbH
  • ACCESS e.V.
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Details

OriginalspracheEnglisch
Titel des SammelwerksSuperalloys 2024
Untertitel Proceedings of the 15th International Symposium on Superalloys
Herausgeber/-innenJonathan Cormier, Ian Edmonds, Stephane Forsik, Paraskevas Kontis, Corey O’Connell, Timothy Smith, Akane Suzuki, Sammy Tin, Jian Zhang
Herausgeber (Verlag)Springer Science and Business Media Deutschland GmbH
Seiten971-983
Seitenumfang13
ISBN (elektronisch)978-3-031-63937-1
ISBN (Print)9783031639364
PublikationsstatusVeröffentlicht - 21 Aug. 2024
Veranstaltung15th International Symposium on Superalloys, ISS 2024 - Pennsylvania, USA / Vereinigte Staaten
Dauer: 8 Sept. 202412 Sept. 2024

Publikationsreihe

NameMinerals, Metals and Materials Series
ISSN (Print)2367-1181
ISSN (elektronisch)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.

ASJC Scopus Sachgebiete

Zitieren

Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler. / Reker, Dirk Wilhelm; Sowa, Roman; Schwalbe, Caspar et al.
Superalloys 2024: Proceedings of the 15th International Symposium on Superalloys. Hrsg. / 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. S. 971-983 (Minerals, Metals and Materials Series).

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Reker, DW, Sowa, R, Schwalbe, C, Boettger, B, Seidel, F, Panella, M, Moehwald, K, Nicolaus, M & Tillmann, W 2024, Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler. in J Cormier, I Edmonds, S Forsik, P Kontis, C O’Connell, T Smith, A Suzuki, S Tin & J Zhang (Hrsg.), Superalloys 2024: Proceedings of the 15th International Symposium on Superalloys. Minerals, Metals and Materials Series, Springer Science and Business Media Deutschland GmbH, S. 971-983, 15th International Symposium on Superalloys, ISS 2024, Pennsylvania, USA / Vereinigte Staaten, 8 Sept. 2024. https://doi.org/10.1007/978-3-031-63937-1_90
Reker, D. W., Sowa, R., Schwalbe, C., Boettger, B., Seidel, F., Panella, M., Moehwald, K., Nicolaus, M., & Tillmann, W. (2024). Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler. In J. Cormier, I. Edmonds, S. Forsik, P. Kontis, C. O’Connell, T. Smith, A. Suzuki, S. Tin, & J. Zhang (Hrsg.), Superalloys 2024: Proceedings of the 15th International Symposium on Superalloys (S. 971-983). (Minerals, Metals and Materials Series). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-3-031-63937-1_90
Reker DW, Sowa R, Schwalbe C, Boettger B, Seidel F, Panella M et al. Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler. in Cormier J, Edmonds I, Forsik S, Kontis P, O’Connell C, Smith T, Suzuki A, Tin S, Zhang J, Hrsg., Superalloys 2024: Proceedings of the 15th International Symposium on Superalloys. Springer Science and Business Media Deutschland GmbH. 2024. S. 971-983. (Minerals, Metals and Materials Series). doi: 10.1007/978-3-031-63937-1_90
Reker, Dirk Wilhelm ; Sowa, Roman ; Schwalbe, Caspar et al. / Improving Repair Braze Gap Strength Through the Development of a Novel Superalloy Filler. Superalloys 2024: Proceedings of the 15th International Symposium on Superalloys. Hrsg. / 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. S. 971-983 (Minerals, Metals and Materials Series).
Download
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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{\textregistered} 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.",
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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

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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 -

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