Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | 2023 IEEE International Electric Machines and Drives Conference |
| Untertitel | IEMDC |
| Herausgeber (Verlag) | Institute of Electrical and Electronics Engineers Inc. |
| ISBN (elektronisch) | 9798350398991 |
| ISBN (Print) | 979-8-3503-9900-4 |
| Publikationsstatus | Veröffentlicht - 2023 |
| Veranstaltung | 2023 IEEE International Electric Machines and Drives Conference, IEMDC 2023 - San Francisco, USA / Vereinigte Staaten Dauer: 15 Mai 2023 → 18 Mai 2023 |
Abstract
The number of propulsors used by an aircraft can affect the requirements for its internal systems, even if the rest of the aircraft and the chosen flight mission remain unchanged. One consequence is that each propulsor must generate a different thrust. For an electric propulsor, this means different operating points for the electrical machine. Concerning this aspect, this paper describes electromagnetic scaling methods for geometric design changes based on variable operating points for electric propulsion of a hybrid-electric aircraft. This presents the possibility of creating a universal model of the electrical machine for interdisciplinary investigations.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Elektrotechnik und Elektronik
- Ingenieurwesen (insg.)
- Maschinenbau
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2023 IEEE International Electric Machines and Drives Conference: IEMDC. Institute of Electrical and Electronics Engineers Inc., 2023.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Rapid Electromagnetic Scaling Methodology for the Electric Propulsion of a Hybrid-Electric Aircraft
AU - Blanken, Norman
AU - Boe, Vivien
AU - Ponick, Bernd
N1 - Funding Information: This work is conducted as part of the joint research programme LuFo VI-1. The work is supported by the German Federal Ministry of Economic Affairs and Climate Action.
PY - 2023
Y1 - 2023
N2 - The number of propulsors used by an aircraft can affect the requirements for its internal systems, even if the rest of the aircraft and the chosen flight mission remain unchanged. One consequence is that each propulsor must generate a different thrust. For an electric propulsor, this means different operating points for the electrical machine. Concerning this aspect, this paper describes electromagnetic scaling methods for geometric design changes based on variable operating points for electric propulsion of a hybrid-electric aircraft. This presents the possibility of creating a universal model of the electrical machine for interdisciplinary investigations.
AB - The number of propulsors used by an aircraft can affect the requirements for its internal systems, even if the rest of the aircraft and the chosen flight mission remain unchanged. One consequence is that each propulsor must generate a different thrust. For an electric propulsor, this means different operating points for the electrical machine. Concerning this aspect, this paper describes electromagnetic scaling methods for geometric design changes based on variable operating points for electric propulsion of a hybrid-electric aircraft. This presents the possibility of creating a universal model of the electrical machine for interdisciplinary investigations.
KW - current density
KW - electric aircraft
KW - hybrid-electric
KW - PMSM
KW - scaling methodology
UR - http://www.scopus.com/inward/record.url?scp=85172734080&partnerID=8YFLogxK
U2 - 10.1109/IEMDC55163.2023.10238901
DO - 10.1109/IEMDC55163.2023.10238901
M3 - Conference contribution
AN - SCOPUS:85172734080
SN - 979-8-3503-9900-4
BT - 2023 IEEE International Electric Machines and Drives Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2023 IEEE International Electric Machines and Drives Conference, IEMDC 2023
Y2 - 15 May 2023 through 18 May 2023
ER -