Görke, Daniel und Pahs, Andreas und Reiber, Christoph und Berthold, Christian (2026) Using PERMAS for Modal Analyses of High-Pressure Turbine Blades Made of a Single-Crystal Nickel-Based Superalloy. PERMAS Users' Conference 2026, 2026-04-23 - 2026-04-24, Tübingen, Deutschland.
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Kurzfassung
High-pressure turbines are located downstream of the combustion chamber and are subject to a high thermal load. The CFD solver TRACE is used to calculate the flow which is in contact with the turbine components. By the multidisciplinary software platform Flow Simulator, TRACE and PERMAS are coupled so that the loads of the CFD mesh can be transferred to the PERMAS mesh in order to calculate the behavior of the structure. Especially the stiffness of the turbine materials, the single-crystal nickel-based superalloys CMSX-4 and CMSX-10, depend strongly on the temperature. The PERMAS load steps consist of a thermal analysis as well as a subsequent nonlinear static and modal analysis. In addition to the temperature dependency, the orthotropic material properties are taken into account. The effect of the thermal and mechanical loads on the eigenfrequencies of the high-pressure turbine blades is shown.
| elib-URL des Eintrags: | https://elib.dlr.de/226097/ | ||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
| Titel: | Using PERMAS for Modal Analyses of High-Pressure Turbine Blades Made of a Single-Crystal Nickel-Based Superalloy | ||||||||||||||||||||
| Autoren: |
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| Datum: | 23 April 2026 | ||||||||||||||||||||
| Referierte Publikation: | Nein | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | high-pressure turbine, CFD-FEM coupling, TRACE, Flow Simulator, PERMAS, CMSX-4, CMSX-10, orthotropic material properties, thermal analysis, modal analysis | ||||||||||||||||||||
| Veranstaltungstitel: | PERMAS Users' Conference 2026 | ||||||||||||||||||||
| Veranstaltungsort: | Tübingen, Deutschland | ||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
| Veranstaltungsbeginn: | 23 April 2026 | ||||||||||||||||||||
| Veranstaltungsende: | 24 April 2026 | ||||||||||||||||||||
| Veranstalter : | INTES GmbH | ||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||
| HGF - Programmthema: | Umweltschonender Antrieb | ||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | L CP - Umweltschonender Antrieb | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtuelles Triebwerk | ||||||||||||||||||||
| Standort: | Göttingen , Köln-Porz , Stuttgart | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Bauweisen und Strukturtechnologie > Bauteilgestaltung und Fertigungstechnologien Institut für Antriebstechnik > Turbine Institut für Aeroelastik > Aeroelastische Experimente Institut für Antriebstechnik > Numerische Methoden | ||||||||||||||||||||
| Hinterlegt von: | Görke, Daniel | ||||||||||||||||||||
| Hinterlegt am: | 14 Sep 2026 13:56 | ||||||||||||||||||||
| Letzte Änderung: | 14 Sep 2026 13:56 |
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