Titel: Hybrid pressure control concept for a speed variable AC motor pump in aerospace application
Sprache: English
Autor/Autorin: Engelhardt, Joerg 
Greißner, Carsten 
Schlagwörter: Aerospace fluid power systems;AC motor pump;variable speed drives;brushless DC motor;pressure control loop;load observer
Erscheinungsdatum: 2002
Quellenangabe: 2nd PhD Symposium 2002 , Modena, Italy, 2002
Zusammenfassung (englisch): This paper describes a new pressure control strategy for AC motor driven pumps in aircraft application. Both, swash plate position and pump speed are used for controlling system pressure in a hybrid approach. The requirements for the pressure control loop and the design methods for the hybrid control circuits with a load observer are introduced. The new control concept has been implemented into an experimental set-up. The validation and evaluation of simulation results on the test rig are discussed in detail. Finally, the new hybrid approach is compared to the conventional approach concerning efficiency, noise level and wear for typical aircraft flight missions.
URI: http://tubdok.tub.tuhh.de/handle/11420/227
DOI: 10.15480/882.225
Institut: Flugzeug-Systemtechnik M-7 
Dokumenttyp: InProceedings (Aufsatz / Paper einer Konferenz etc.)
Enthalten in den Sammlungen:Publications (tub.dok)

Dateien zu dieser Ressource:
Datei Beschreibung GrößeFormat
208_19.pdf683,96 kBAdobe PDFMiniaturbild
Öffnen/Anzeigen
Zur Langanzeige

Seitenansichten

548
Letzte Woche
6
Letzten Monat
5
checked on 22.03.2019

Download(s)

122
checked on 22.03.2019

Google ScholarTM

Prüfe

Export

Alle Ressourcen in diesem Repository sind urheberrechtlich geschützt.