elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Advancing high-pressure turbine vane cooling through additive manufacturing: Insights from the 3DCeraTURB project

Haubrich, Jan and Kasperovich, Galina and Gussone, Joachim and Petersen, Anna and Schöffler, Robin and Lakemann, Moritz and Ebel, Paul-Benjamin and Winkelmann, Peter (2025) Advancing high-pressure turbine vane cooling through additive manufacturing: Insights from the 3DCeraTURB project. ASME Turbo Expo 2025 Conference, 2025-06-16 - 2025-06-20, Memphis, USA.

Full text not available from this repository.

Abstract

The efficiency of modern gas turbines and jet engines is closely tied to the permissible operating temperatures of the materials used. As the inlet temperature of high-pressure turbines rises, the need for advanced cooling techniques becomes critical, demanding the development of robust materials and innovative fabrication methods. Key challenges in designing these cooling systems include achieving uniform airflow distribution, reducing temperature gradients, and optimizing cooling according to load zones, all while adhering to manufacturing and strength constraints. Research at the German Aerospace center aims at furthering and exploiting additive manufacturing (AM) technologies to addresses these challenges by developing turbine vanes with intricate cooling structures suited particularly for fabrication with Laser Powder Bed Fusion (LPBF). In the highly interdisciplinary 3DCeraTurb project, new designs are being developed, LPBF materials studied and turbine vane demonstrators realized and tested. These demonstrators feature double-wall pins and an array of holes and film cooling holes. The aim is to achieve a more efficient cooling to enhance engine performance and enable fuel savings and emission reductions. This talk summarizes the progress of 3DCeraTurb with a focus on the additive manufacturing process developments and materials studies. Beyond the production of advanced turbine vanes, the project has enabled enhancements across the production chain, including heat treatment, mechanical property optimization, and post-processing of surfaces. Different materials suited well for laser welding-related processed including Inconel 718 and VDM780 are being investigated. Inconel 718 is readily available at low cost, well understood and can be processed robust and reproducibly, but to pave the way for better high-temperature performance materials, new alloys such as VDM780 that can potentially withstand temperatures up to 750 °C under fatigue and creep conditions need to be considered. 3DCeraTurb marks a significant step toward in exploiting additive manufacturing for enhancing turbine efficiency and reliability in extreme operating environments

Item URL in elib:https://elib.dlr.de/215457/
Document Type:Conference or Workshop Item (Speech)
Title:Advancing high-pressure turbine vane cooling through additive manufacturing: Insights from the 3DCeraTURB project
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Haubrich, JanJan.Haubrich (at) dlr.dehttps://orcid.org/0000-0002-5748-2755UNSPECIFIED
Kasperovich, GalinaGalina.Kasperovich (at) dlr.dehttps://orcid.org/0000-0002-0096-0533UNSPECIFIED
Gussone, JoachimJoachim.Gussone (at) dlr.deUNSPECIFIEDUNSPECIFIED
Petersen, AnnaAnna.Petersen (at) dlr.dehttps://orcid.org/0000-0003-4819-4994UNSPECIFIED
Schöffler, RobinRobin.Schoeffler (at) dlr.dehttps://orcid.org/0000-0002-0931-9021UNSPECIFIED
Lakemann, MoritzMoritz.Lakemann (at) dlr.deUNSPECIFIEDUNSPECIFIED
Ebel, Paul-Benjaminpaul.ebel (at) dlr.dehttps://orcid.org/0000-0002-7112-7653UNSPECIFIED
Winkelmann, PeterPeter.Winkelmann (at) dlr.deUNSPECIFIEDUNSPECIFIED
Date:18 June 2025
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Additive manufacturing, Inconel 718, VDM780, laser powder bed fusion, heat treatment, turbine vane
Event Title:ASME Turbo Expo 2025 Conference
Event Location:Memphis, USA
Event Type:international Conference
Event Start Date:16 June 2025
Event End Date:20 June 2025
Organizer:American Society of Mechanical Engineers (ASME)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Advanced Materials and New Manufacturing Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Materials Research > Metallic and Hybrid Materials
Deposited By: Kasperovich, Dr.-Ing. Galina
Deposited On:12 Aug 2025 10:14
Last Modified:03 Dec 2025 09:37

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.