A refueling coupling regulator assembly including a housing forming a fluid path. A first stage pressure regulator may be provided within the housing, and may be operable between an un-modulated position and a modulated position to regulate a flow of fluid through the housing. A second stage pressure regulator may be provided within the housing, and may be operable between an un-modulated position and a modulated position to regulate a flow of fluid through the housing. The first stage pressure regulator and the second stage pressure regulator may be operable independent of one another.


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    Title :

    DUAL REDUNDANT AERIAL REFUELING COUPLING REGULATOR ASSEMBLY


    Contributors:

    Publication date :

    2016-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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