A system for allocating power includes a plurality of receptacles and a power delivery controller communicatively coupled to the plurality of receptacles. The power delivery controller is to: detect a new connection to a first receptacle of the plurality of receptacles; receive a request from the first receptacle which would exceed an amount of uncommitted available power; request a device attached to a second receptacle of the plurality of receptacles reduce an amount of power being received from the second receptacle; and in response to detecting a reduction of power to the second receptacle, provide power to the first receptacle as indicated in the request.


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    Title :

    POWER CONTROLLER FOR AIRCRAFT RECEPTACLES


    Contributors:

    Publication date :

    2020-02-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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