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MULTI-DISCIPLINARY TOOL COUPLING FOR THE DETERMINATION OF TURBOFAN TRANSIENTS DURING PRELIMINARY DESIGN

Vieweg, Maximilian and Wolters, Florian and Reitenbach, Stanislaus and Hollmann, Carsten and Becker, Richard-Gregor (2019) MULTI-DISCIPLINARY TOOL COUPLING FOR THE DETERMINATION OF TURBOFAN TRANSIENTS DURING PRELIMINARY DESIGN. In: Proceedings of the ASME Turbo Expo. Proceedings of the ASME Turbo Expo. ASME Turbo Expo 2019, 17.-21. Jun 2019, Phoenix, USA.

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Abstract

Over the past decades of preliminary aero-engine design a great effort has been invested in increasing steady-state efficiency to reduce missions fuel burn and thus CO2 emissions. Whilst pushing the performance cycle further to its limits previously minor deemed processes such as the transient behavior become more important because engines stability must still be granted for. It is therefore beneficial to integrate transient performance early into the overall aero-engine design tool chain to be able to predict the dynamic behavior from the beginning. This paper presents a methodology to couple predesign and transient performance simulation in order to get a more holistic picture of aero-engines early in the design process. This procedure entails extensive amount of data transfer throughout multi-disciplinary tools with different fidelity levels. This task is tackled using DLRs virtual engine platform GTlab (Gas Turbine Laboratory), which provides a geometric data model with abstract description of predesign components and standardized interfaces for data exchange. In order to demonstrate the proposed methodology a performance model of a turbofan similar to the V2500 aero-engine is used. For that purpose, a performance cycle is established providing boundary conditions for the preliminary aerodynamic engine design. The designed components provide necessary input data for the subsequent transient certification maneuver. Eventually, parametric studies are conducted to show the impact of design variations on transient data such as the minimum surge margin and minimum tip clearance as well as on preliminary engine design.

Item URL in elib:https://elib.dlr.de/130871/
Document Type:Conference or Workshop Item (Speech)
Title:MULTI-DISCIPLINARY TOOL COUPLING FOR THE DETERMINATION OF TURBOFAN TRANSIENTS DURING PRELIMINARY DESIGN
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Vieweg, MaximilianMaximilian.Vieweg (at) dlr.deUNSPECIFIED
Wolters, FlorianFlorian.Wolters (at) dlr.deUNSPECIFIED
Reitenbach, StanislausStanislaus.Reitenbach (at) dlr.deUNSPECIFIED
Hollmann, Carstencarsten.hollmann (at) dlr.deUNSPECIFIED
Becker, Richard-GregorRichard-Gregor.Becker (at) dlr.deUNSPECIFIED
Date:June 2019
Journal or Publication Title:Proceedings of the ASME Turbo Expo
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Publisher:Proceedings of the ASME Turbo Expo
Status:Published
Keywords:Transient Performance Instationär Heat Soakage Wärmeübertragung V2500
Event Title:ASME Turbo Expo 2019
Event Location:Phoenix, USA
Event Type:international Conference
Event Dates:17.-21. Jun 2019
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 - Virtual Engine and Validation methods
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine
Deposited By: Vieweg, Maximilian
Deposited On:19 Dec 2019 14:26
Last Modified:19 Dec 2019 14:26

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