Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016 |
| Herausgeber (Verlag) | Institute of Electrical and Electronics Engineers Inc. |
| ISBN (elektronisch) | 9781509008148 |
| Publikationsstatus | Veröffentlicht - 2016 |
| Veranstaltung | 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016 - Toulouse, Frankreich Dauer: 2 Nov. 2016 → 4 Nov. 2016 |
Abstract
This paper presents the design approach of a power train used in an advanced high-lift system for future aircraft. Aircraft applications require an ultra-light and integrated design leading to an electrical machine with a high power to weight ratio of 2.82 kW/kg. To achieve additional high lift during take-off and landing, air is blown out at the back flaps of the aircraft wings using a turbo compressor which is directly driven by an inverter-fed electrical machine. The design of the power train and the electrical machine in particular is discussed under different aspects, e.g. the electromagnetic design and the mechanical demands including the selection of a feasible rotor armour. This paper identifies the interfaces between the different factors and describes their dependencies.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
- Ingenieurwesen (insg.)
- Fahrzeugbau
- Energie (insg.)
- Energieanlagenbau und Kraftwerkstechnik
- Ingenieurwesen (insg.)
- Elektrotechnik und Elektronik
- Sozialwissenschaften (insg.)
- Verkehr
Zitieren
- Standard
- Harvard
- Apa
- Vancouver
- BibTex
- RIS
2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016. Institute of Electrical and Electronics Engineers Inc., 2016. 7841338.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - Design Considerations for an Electrical Machine Propelling a Direct Driven Turbo Compressor for Use in Active High-Lift Systems
AU - Narjes, Gerrit
AU - Müller, Jan
AU - Mertens, Axel
AU - Ponick, Bernd
AU - Kauth, Felix
AU - Seume, Jörg
PY - 2016
Y1 - 2016
N2 - This paper presents the design approach of a power train used in an advanced high-lift system for future aircraft. Aircraft applications require an ultra-light and integrated design leading to an electrical machine with a high power to weight ratio of 2.82 kW/kg. To achieve additional high lift during take-off and landing, air is blown out at the back flaps of the aircraft wings using a turbo compressor which is directly driven by an inverter-fed electrical machine. The design of the power train and the electrical machine in particular is discussed under different aspects, e.g. the electromagnetic design and the mechanical demands including the selection of a feasible rotor armour. This paper identifies the interfaces between the different factors and describes their dependencies.
AB - This paper presents the design approach of a power train used in an advanced high-lift system for future aircraft. Aircraft applications require an ultra-light and integrated design leading to an electrical machine with a high power to weight ratio of 2.82 kW/kg. To achieve additional high lift during take-off and landing, air is blown out at the back flaps of the aircraft wings using a turbo compressor which is directly driven by an inverter-fed electrical machine. The design of the power train and the electrical machine in particular is discussed under different aspects, e.g. the electromagnetic design and the mechanical demands including the selection of a feasible rotor armour. This paper identifies the interfaces between the different factors and describes their dependencies.
KW - Aircraft propulsion
KW - Compressors
KW - Electric machines
KW - High-speed electric machine
KW - Inverters
KW - Permanent magnet machines
KW - Rotating machines
UR - http://www.scopus.com/inward/record.url?scp=85015381970&partnerID=8YFLogxK
U2 - 10.1109/esars-itec.2016.7841338
DO - 10.1109/esars-itec.2016.7841338
M3 - Conference contribution
AN - SCOPUS:85015381970
BT - 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016
Y2 - 2 November 2016 through 4 November 2016
ER -