An aircraft refueling system (10) includes a master controller (12), a fleet controller (14) in communication with the master controller, a platform controller (18) in communication with the fleet controller, and a fuel control system (16) in communication with the platform controller. Embodiments of an aircraft refueling system may include a primary pressure controller (20), a secondary pressure controller (22), a programmable logic controller (24), and a data logger controller (26). The master controller may be configured to receive and analyze data from at least one of the fleet controller, the platform controller, and the fuel control system; and to modify operational parameters or upgrade the fuel control system based at least in part on the analysis of received data.


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    Titel :

    AIRCRAFT REFUELING SYSTEM


    Beteiligte:
    BODKHE ABHIJIT A (Autor:in) / VISHWAKARMA ASHOK K (Autor:in) / RAWAT JASPAL (Autor:in) / HUM STEVEN (Autor:in) / MORE PARAG (Autor:in) / NEHETE CHANDRASHEKHAR S (Autor:in) / SBONEK ROBERT L (Autor:in) / LAING JEFFREY M (Autor:in) / KHANDELWAL TARUNA (Autor:in) / AGARWAL VIVEK (Autor:in)

    Erscheinungsdatum :

    2022-02-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



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