A system and method for an aircraft refueling receptacle. The aircraft refueling receptacle comprises a pedestal, a flanged structure, a sliding valve, and a bolt. The flanged structure has a first ledge, a second ledge, and a number of flanges extending inwardly. The pedestal contacts the first ledge. The sliding valve has a first face that contacts the second ledge of the flanged structure during refueling. The bolt extends a part of a length of the pedestal and is connected to a receiver within the pedestal.


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    Titel :

    Aircraft receptacle


    Beteiligte:
    LEWIS BRIAN (Autor:in) / KLENKE PAUL WILLIAM (Autor:in) / BYRNE DENNIS P (Autor:in) / NGUYEN KY HUU (Autor:in) / WEBER PAUL GERARD (Autor:in)

    Erscheinungsdatum :

    2019-04-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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



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