An aircraft fuel scavenge system incorporates a scavenge pump (30) receiving fuel from a center tank (10) and depositing the fuel in a wing tank (14). A water separator (40) receives fuel through an inlet tube (38) providing a plurality of momentum changes to incoming fuel, the water separator having a fuel outlet (32) connected to the scavenge pump and a water outlet. A water manifold (80) is connected from the water outlet to an input to a fuel supply line to an engine.


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    Title :

    Fuel scavenge water removal system


    Additional title:

    Kraftstoff-Wasserentfernungssystem
    Système d'élimination de l'eau dans les réservoir de carburant


    Contributors:

    Publication date :

    2017-03-22


    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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