An electric fuse for an aircraft solid-state power controller comprising at least one electric conductor, which is connected between an electric input terminal and an electric output terminal, and which is configured to blow when an electric current (I) flowing through the at least one electric conductor exceeds a predefined threshold (Imax). The at least one electric conductor is encapsulated in a potting and at least one outer surface of the potting is covered with a polymeric coating.


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    Title :

    ELECTRIC FUSE FOR AN AIRCRAFT SOLID STATE POWER CONTROLLER AND AIRCRAFT SOLID STATE POWER CONTROLLER COMPRISING AN ELECTRIC FUSE


    Contributors:

    Publication date :

    2024-10-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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