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Distributed Multidisciplinary Optimization of a Turbine Blade Regarding Performance, Reliability and Castability

Buske, Clemens and Krumme, Alexander and Schmidt, Thomas and Dresbach, Christian and Zur, Sascha Andre and Tiefers, Rüdiger (2016) Distributed Multidisciplinary Optimization of a Turbine Blade Regarding Performance, Reliability and Castability. ASME Turbo Expo 2016, 13-17 Jun 2016, Seoul, South Korea. DOI: 10.1115/GT2016-56079 ISBN 978-0-7918-4971-2

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Official URL: http://proceedings.asmedigitalcollection.asme.org/proceeding.aspx?articleid=2554815

Abstract

Modern aero-engine blades are optimized for high perfor- mance and long service life, but manufacturing requirements are not considered adequately during the design process. Thus, time- consuming, iterative re-designs become necessary until a pro- ducible component evolves. The multidisciplinary design opti- mization method presented in this paper addresses not only the aerodynamic efficiency and structural reliability of a new turbine blade, but also ensures the castability of the design and thereby accelerates the entire design process and reduces the time-to- production. Because real casting process simulations are very time-intensive, they were substituted by checks of experimentally and numerically validated geometrical constraints. Different engineering tools were assembled in a joint process chain using an integration framework, which manages and distributes the calculations and hence the workload in a shared network. Based on a preliminary design of a new turbine section, the selected initial low pressure turbine blade was neither castable nor reliable. The multidisciplinary optimization achieved a blade design that satisfies the requirements for a successful casting process, has a low failure probability and, although not as high as from a pure aerodynamic optimization, exhibits an efficiency improvement.

Item URL in elib:https://elib.dlr.de/104867/
Document Type:Conference or Workshop Item (Speech)
Title:Distributed Multidisciplinary Optimization of a Turbine Blade Regarding Performance, Reliability and Castability
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Buske, ClemensClemens.Buske (at) dlr.dehttps://orcid.org/0000-0003-4157-7415
Krumme, AlexanderAlexander.Krumme (at) dlr.deUNSPECIFIED
Schmidt, ThomasThomas.Schmidt (at) dlr.deUNSPECIFIED
Dresbach, ChristianChristian.Dresbach (at) dlr.deUNSPECIFIED
Zur, Sascha AndreSascha.Zur (at) dlr.deUNSPECIFIED
Tiefers, RüdigerACCESS e.V., AachenUNSPECIFIED
Date:June 2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:2C
DOI :10.1115/GT2016-56079
Page Range:V02CT45A002
ISBN:978-0-7918-4971-2
Status:Published
Keywords:MDO, CFD, FEA, Turbine, Castability, High Fidelity
Event Title:ASME Turbo Expo 2016
Event Location:Seoul, South Korea
Event Type:international Conference
Event Dates:13-17 Jun 2016
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies, L - Simulation and Validation
Location: Göttingen , Köln-Porz , Stuttgart
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Institute of Structures and Design > Design and Manufacture Technologies
Institute of Materials Research > Metallic Structures and Hybrid Material Systems
Institut of Simulation and Software Technology > Distributed Systems and Component Software
Deposited By: Buske, Clemens
Deposited On:18 Oct 2016 12:44
Last Modified:08 Nov 2016 07:59

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