A refueling boom is provided for use in an aerial refueling system. The refueling boom may include a boom section configured to extend from a tanker aircraft. A pressure limiting valve may be provided downstream of the boom section. A boom nozzle may be provided downstream of, or integral with, the pressure limiting valve.


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    Title :

    AERIAL REFUELING BOOM WITH PRESSURE LIMITING VALVE


    Contributors:

    Publication date :

    2015-10-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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