A power system for an aircraft is disclosed. The power system comprises a power panel, at least one power rail coupled to the power panel, wherein the power rail is integrated with a mounting rail for the passenger service unit, and at least one universal serial bus (USB) port coupled to the power panel and mounted in the passenger service unit.


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    Titel :

    Plug-n-play power system for an accessory in an aircraft


    Beteiligte:
    LEE DONALD B (Autor:in)

    Erscheinungsdatum :

    2016-11-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR



    Plug & Play Power

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    AIRCRAFT ACCESSORY SYSTEM

    HOLLIDAY, T. B. | SAE Technical Papers | 1943


    Aircraft accessory system

    Holliday, T.B. | Engineering Index Backfile | 1943


    Aircraft accessory system

    Holliday, T.B. | Engineering Index Backfile | 1943


    VEHICLE ACCESSORY PORT AND PLUG

    ELDER CHRISTIAN / GRIFFITH ERIC | Europäisches Patentamt | 2020

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