Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition |
| Untertitel | Turbomachinery |
| Herausgeber (Verlag) | American Society of Mechanical Engineers(ASME) |
| Band | 2E |
| ISBN (elektronisch) | 9780791884102 |
| Publikationsstatus | Veröffentlicht - 11 Jan. 2021 |
| Veranstaltung | ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT2020 - online Dauer: 21 Sept. 2020 → 25 Sept. 2020 |
Abstract
This paper presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D inverse design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall and thus contributing to the reduction of both the aircraft noise footprint and the impact of aviation emission on local air quality. As part of a collaborative work between the Institute of Turbomachinery and Fluid Dynamics of the Leibniz University Hannover and Advanced Design Technology Ltd., an existing optimized compressor stage for this application is redesigned using a 3D inverse method. The new compressor design presents an increase in pressure ratio and total-to-total isentropic efficiency of more than 5.5% and 1% respectively at design point. The higher PR at design point allows the compressor to be run at lower rotational speeds, which decreases the load on the electric motor and the power electronic systems, and hence contributing further to the overall weight reduction of the entire system. The advantage of using an inverse design methodology is shown in this paper as a method that allows a very simple parameterization, reducing significantly the design time and hence allowing the exploration of wider design spaces, with the potential of reaching more innovative and efficient designs. The fast and reliable design and analysis of components represents an important advantage for the enhancement of aircraft electrification, where long design times are often a barrier for the exploration of system configurations.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Allgemeiner Maschinenbau
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ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition: Turbomachinery . Band 2E American Society of Mechanical Engineers(ASME), 2021. V02ET39A023.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Design of a mixed-flow transonic compressor for active high-lift system using a 3D inverse design methodology
AU - Wang, Peng
AU - Vera-Morales, Maria
AU - La, Patrick
AU - Zangeneh, Mehrdad
AU - Maroldt, Niklas
AU - Willers, Ole
AU - Kauth, Felix
AU - Seume, Jörg
N1 - Funding Information: The authors gratefully acknowledge the support of the German Science Foundation (DFG) provided for Collaborative Research Centre (CRC) 880 “Efficient High-Lift for Future Civil Aircraft”.
PY - 2021/1/11
Y1 - 2021/1/11
N2 - This paper presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D inverse design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall and thus contributing to the reduction of both the aircraft noise footprint and the impact of aviation emission on local air quality. As part of a collaborative work between the Institute of Turbomachinery and Fluid Dynamics of the Leibniz University Hannover and Advanced Design Technology Ltd., an existing optimized compressor stage for this application is redesigned using a 3D inverse method. The new compressor design presents an increase in pressure ratio and total-to-total isentropic efficiency of more than 5.5% and 1% respectively at design point. The higher PR at design point allows the compressor to be run at lower rotational speeds, which decreases the load on the electric motor and the power electronic systems, and hence contributing further to the overall weight reduction of the entire system. The advantage of using an inverse design methodology is shown in this paper as a method that allows a very simple parameterization, reducing significantly the design time and hence allowing the exploration of wider design spaces, with the potential of reaching more innovative and efficient designs. The fast and reliable design and analysis of components represents an important advantage for the enhancement of aircraft electrification, where long design times are often a barrier for the exploration of system configurations.
AB - This paper presents the redesign of an electrically driven mixed flow transonic compressor by using a 3D inverse design methodology. The compressor will be used for an active high-lift system application that aims to delay the onset of stall and thus contributing to the reduction of both the aircraft noise footprint and the impact of aviation emission on local air quality. As part of a collaborative work between the Institute of Turbomachinery and Fluid Dynamics of the Leibniz University Hannover and Advanced Design Technology Ltd., an existing optimized compressor stage for this application is redesigned using a 3D inverse method. The new compressor design presents an increase in pressure ratio and total-to-total isentropic efficiency of more than 5.5% and 1% respectively at design point. The higher PR at design point allows the compressor to be run at lower rotational speeds, which decreases the load on the electric motor and the power electronic systems, and hence contributing further to the overall weight reduction of the entire system. The advantage of using an inverse design methodology is shown in this paper as a method that allows a very simple parameterization, reducing significantly the design time and hence allowing the exploration of wider design spaces, with the potential of reaching more innovative and efficient designs. The fast and reliable design and analysis of components represents an important advantage for the enhancement of aircraft electrification, where long design times are often a barrier for the exploration of system configurations.
KW - 3D inverse design
KW - Active high-lift system
KW - Electrically powered transonic mixed-flow compressor
UR - http://www.scopus.com/inward/record.url?scp=85099779369&partnerID=8YFLogxK
U2 - 10.1115/GT2020-15645
DO - 10.1115/GT2020-15645
M3 - Conference contribution
AN - SCOPUS:85099779369
VL - 2E
BT - ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition
PB - American Society of Mechanical Engineers(ASME)
T2 - ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT2020
Y2 - 21 September 2020 through 25 September 2020
ER -