Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society |
| Untertitel | Proceedings |
| Herausgeber (Verlag) | Institute of Electrical and Electronics Engineers Inc. |
| Seiten | 4397-4402 |
| Seitenumfang | 6 |
| ISBN (elektronisch) | 9781538611272 |
| Publikationsstatus | Veröffentlicht - 15 Dez. 2017 |
| Veranstaltung | Annual Conference of the IEEE Industrial Electronics Society - Beijing, China Dauer: 29 Okt. 2017 → 1 Nov. 2017 Konferenznummer: 43 |
Abstract
This paper presents the 100 kW air-cooled inverter design of a power train used for advanced high-lift systems in future aircrafts. To achieve additional high-lift during take-off and landing of a plane, air is blown out at the back flap of the wings using a turbo compressor directly driven by an electrical machine. Silicon Carbide (SiC) devices promise large savings in volume, weight and losses of the inverter, which results in a highly-integrated system. Furthermore, the intake air is used as coolant for the power electronics. Such a system with a high power density of 10.8 kW/l has been designed and implemented, and first tests were performed on a laboratory prototype.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Wirtschaftsingenieurwesen und Fertigungstechnik
- Mathematik (insg.)
- Steuerung und Optimierung
- Energie (insg.)
- Energieanlagenbau und Kraftwerkstechnik
- Ingenieurwesen (insg.)
- Elektrotechnik und Elektronik
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IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society: Proceedings. Institute of Electrical and Electronics Engineers Inc., 2017. S. 4397-4402.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Power Electronics Design for a direct-driven Turbo Compressor Used as Advanced High-Lift System in Future Aircraft
AU - Muller, Jan Kaspar
AU - Mertens, Axel
N1 - Conference code: 43
PY - 2017/12/15
Y1 - 2017/12/15
N2 - This paper presents the 100 kW air-cooled inverter design of a power train used for advanced high-lift systems in future aircrafts. To achieve additional high-lift during take-off and landing of a plane, air is blown out at the back flap of the wings using a turbo compressor directly driven by an electrical machine. Silicon Carbide (SiC) devices promise large savings in volume, weight and losses of the inverter, which results in a highly-integrated system. Furthermore, the intake air is used as coolant for the power electronics. Such a system with a high power density of 10.8 kW/l has been designed and implemented, and first tests were performed on a laboratory prototype.
AB - This paper presents the 100 kW air-cooled inverter design of a power train used for advanced high-lift systems in future aircrafts. To achieve additional high-lift during take-off and landing of a plane, air is blown out at the back flap of the wings using a turbo compressor directly driven by an electrical machine. Silicon Carbide (SiC) devices promise large savings in volume, weight and losses of the inverter, which results in a highly-integrated system. Furthermore, the intake air is used as coolant for the power electronics. Such a system with a high power density of 10.8 kW/l has been designed and implemented, and first tests were performed on a laboratory prototype.
KW - More Electric Aircraft (MEA)
KW - Power converters for aviation
KW - Silicon Carbide (SiC)
KW - Thermal design
UR - http://www.scopus.com/inward/record.url?scp=85046664593&partnerID=8YFLogxK
U2 - 10.1109/IECON.2017.8216756
DO - 10.1109/IECON.2017.8216756
M3 - Conference contribution
AN - SCOPUS:85046664593
SP - 4397
EP - 4402
BT - IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 43rd Annual Conference of the IEEE Industrial Electronics Society, IECON 2017
Y2 - 29 October 2017 through 1 November 2017
ER -