TU Berlin


Logo Fachgebiet Luftfahrtantriebe

Inhalt des Dokuments

zur Navigation

Publikationen am Fachgebiet Luftfahrtantriebe

Detailed Design of a High Speed Switched Reluctance Starter/Generator for More/All Electric Aircraft
Zitatschlüssel 2010_shoujun_jcja
Autor Shoujun, S. and Weiguo, L. and Peitsch, D. and Schaefer, U.
Seiten 216–226
Jahr 2010
ISSN 1000-9361
DOI 10.1016/S1000-9361(09)60208-9
Ort UK
Journal Chinese Journal of Aeronautics
Jahrgang 23
Nummer 2
Monat 04
Notiz Northwestern Polytechnical University, Xi'an, China:
S. Shoujun, L. Weiguoa
Technische Universität Berlin:
S. Shoujun, D. Peitsch, U. Schaefer
Verlag Elsevier Ltd.
Serie ScienceDirect
Zusammenfassung The basic concepts and advantages of more/all electric aircraft (M/AEA) are briefly addressed. The combined starter/generator (CS/G) system is introduced as a key technology to enable M/AEA. Some important performance requirements for CS/G system are obtained. Based on these requirements, a high speed switched reluctance machine (SRM) is designed to operate as a starter/generator. The entire design process is mainly divided into two stages: electromagnetic design and thermal design. In electromagnetic design stage, the electromagnetic structure and dimensions of the machine and the number of phase winding turns per pole are obtained; the topology and main technical details of the converter are briefly introduced as well. In thermal design stage, a liquid-cooling system is designed based on the thermal analysis of the machine. In the end, the performances of the designed SRM are basically verified by simulation. To get high performances, the exciting angles are optimized in two different operating modes respectively, and the optimized performances in the motoring mode are given as well.
Link zur Publikation Link zur Originalpublikation Download Bibtex Eintrag

Nach oben



Schnellnavigation zur Seite über Nummerneingabe