Since inverter induced instability is system problem, analysis of whole aircraft d-c power system is presented to point out measurable properties which may be used to predict stability. (See also Am Inst Elec Engrs -- Trans v 76 (Applications and Industry) n 32 Sept 1957 p 183-8)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stability of aircraft D-C power systems with inverter loads


    Weitere Titelangaben:

    Elec Eng


    Beteiligte:
    Thomas, R.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Aircraft Electrical Power Systems and Nonlinear Dynamic Loads

    Singer, Charles / Guernsey, Corinne M. / Gousy, Jason et al. | SAE Technical Papers | 2012


    Aircraft Loads

    M. Neubauer / G. Gunther | NTIS | 2001


    Electro-Mechanical-Thermal Performance and Stability of Aircraft Energy Networks With Pulse Power Loads

    Dillon, Joshua A. / Weaver, Wayne W. / Robinett iii, Rush D. et al. | IEEE | 2020


    System for multiple inverter-driven loads

    LOVERCHECK GLENN T / DAIGLE JEFFREY LOUIS / VERMA RAJEEV et al. | Europäisches Patentamt | 2017

    Freier Zugriff