This paper describes the design, construction and testing of a matrix converter permanent magnet motor drive for an electro-hydrostatic aircraft actuator (ERA). The converter has been built using a 35Amp Eupec matrix converter module with closed loop vector control. The commutation time has been minimized to avoid any unnecessary waveform distortion. Practical results from the testing of this converter are presented.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A matrix converter based permanent magnet motor drive for an aircraft actuation system


    Beteiligte:
    Wheeler, P. (Autor:in) / Clare, J. (Autor:in) / Empringham, L. (Autor:in) / Apap, M. (Autor:in) / Bradley, K. (Autor:in) / Whitley, C. (Autor:in) / Towers, G. (Autor:in)


    Erscheinungsdatum :

    01.01.2003


    Format / Umfang :

    562896 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    An electro-hydrostatic aircraft actuator using a matrix converter permanent magnet motor drive

    Wheeler, P.W. / Clare, J.C. / Apap, M. et al. | IET Digital Library Archive | 2004


    Fault-tolerant, matrix converter, permanent magnet synchronous motor drive for open-circuit failures

    Khwan-on, S. / Lillo, L. / Empringham, L. et al. | Tema Archiv | 2011


    Permanent magnet brushless drives for aircraft flight control surface actuation

    Atallah, K. / Caparrelli, F. / Bingham, C.M. et al. | IET Digital Library Archive | 1999


    ROTOR, PERMANENT-MAGNET MOTOR, MOTOR DRIVE SYSTEM, AND VEHICLE

    HUANG XIN / LI MENGDE / YANG HUI et al. | Europäisches Patentamt | 2023

    Freier Zugriff