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Performance Prediction and Early Design Code for Axial Turbines and its Application in Research and Predesign

Krumme, Alexander (2016) Performance Prediction and Early Design Code for Axial Turbines and its Application in Research and Predesign. In: Proceedings of the ASME Turbo Expo: Turbine Technical Conference and Exhibition 2016. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, 2016-06-13 - 2016-06-17, Seoul, Südkorea. doi: 10.1115/GT2016-56082. ISBN 978-0-7918-4971-2.

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Offizielle URL: https://proceedings.asmedigitalcollection.asme.org/proceeding.aspx?articleid=2554763

Kurzfassung

This paper presents DLR’s in-house Performance prediction and Early Design Code for axial Turbines PrEDiCT. It is capable of designing multi-stage, multi-spool air-breathing turbines with consideration of coolant flows and different loading levels, relevant for energy, aircraft and general turbomachinery. After pointing out the integration of PrEDiCT into the DLR predesign process and the role of each method involved, its iterative main calculation routine will be presented as well as its thermodynamic and geometrical methods to output a complete turbine annulus with preliminary blades, fulfilling power requirements and coming from a minimal input parameter set. An important aspect is the developed concept for user-driven design work with PrEDiCT involving an interactive GUI and a built-in execution mode called ‘ReDesign’ that retains the design code nature of the program with geometry output, but still allows for effective evolution and tailoring of the global design down to each stage and blade row. The paper closes with the validation and results section, which highlights three examples where the code is applied to axial turbine predesign and research. The intention of this paper is to encourage the use of early predesign methods even by non-OEM organizations, since the presented work has shown for DLR multiple benefits in terms of research work, cooperation with other departments and OEM industry as well as training of personnel. Furthermore the implementation of PrEDiCT facilitated the transition from pre- to detailed design (i.e. 3D CFD) to such an extent, that the still important role of 2D throughflow methods could be questioned, i.e. being less relevant in the future for some design tasks.

elib-URL des Eintrags:https://elib.dlr.de/107646/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Performance Prediction and Early Design Code for Axial Turbines and its Application in Research and Predesign
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Krumme, AlexanderAlexander.Krumme (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:13 Juni 2016
Erschienen in:Proceedings of the ASME Turbo Expo: Turbine Technical Conference and Exhibition 2016
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
DOI:10.1115/GT2016-56082
ISBN:978-0-7918-4971-2
Status:veröffentlicht
Stichwörter:Turbine Vorentwurf predesign Auslegung
Veranstaltungstitel:ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
Veranstaltungsort:Seoul, Südkorea
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:13 Juni 2016
Veranstaltungsende:17 Juni 2016
Veranstalter :The American Society of Mechanical Engineers ASME
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Antriebssysteme
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L ER - Engine Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Turbinentechnologien (alt), L - Virtuelles Triebwerk und Validierungsmethoden (alt)
Standort: Göttingen
Institute & Einrichtungen:Institut für Antriebstechnik > Turbine
Hinterlegt von: Krumme, Dr.-Ing. Alexander
Hinterlegt am:11 Nov 2016 07:39
Letzte Änderung:24 Apr 2024 20:12

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