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.


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    Title :

    SOLID STATE POWER CONTROLLER FOR AN AIRCRAFT


    Additional title:

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


    Contributors:

    Publication date :

    2017-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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