The invention relates to a solid state power controller for an aircraft. The solid state power controller comprises a solid state switching device for activating an electrical power output bus, a control unit for controlling the solid state switching device, and a current sensing circuit for monitoring current flowing in the electrical power output bus. The current sensing circuit includes a sensing fuse that provides a simplified and more reliable solid state power controller.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SOLID STATE POWER CONTROLLER FOR AN AIRCRAFT


    Weitere Titelangaben:

    DISPOSITIF DE COMMANDE DE PUISSANCE A SEMI-CONDUCTEURS POUR UN AERONEF


    Beteiligte:

    Erscheinungsdatum :

    2017-05-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01H Elektrische Schalter , ELECTRIC SWITCHES




    SOLID STATE POWER CONTROLLER FOR AIRCRAFT

    JULIAN PETER MAYES | Europäisches Patentamt | 2015

    Freier Zugriff



    PRINTED CIRCUIT BOARD ASSEMBLY FOR AN AIRCRAFT SOLID STATE POWER CONTROLLER

    MAIER JOSEF / GIETZOLD THOMAS | Europäisches Patentamt | 2024

    Freier Zugriff