A fuel transfer system for an aircraft includes an upper tank, a lower tank, a fuel transfer line connecting the upper tank to the lower tank, an upper fuel transfer line outlet in the lower tank, a lower fuel transfer line outlet in the lower tank, an upper float valve associated with the upper fuel transfer line outlet, and a lower float valve associated with the lower fuel transfer line outlet. The upper fuel transfer line outlet, which is in the lower tank, is in fluid communication with the upper tank. The lower fuel transfer line outlet, which is located in the lower tank, is in fluid communication with the upper tank.


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    Title :

    FUEL TRANSFER SYSTEM CONTROLLED BY FLOAT VALVES


    Additional title:

    DURCH SCHWIMMERVENTILE GESTEUERTES BRENNSTOFFTRANSFERSYSTEM
    SYSTÈME DE TRANSFERT DE CARBURANT COMMANDÉ PAR DES VANNES À FLOTTEUR


    Contributors:

    Publication date :

    2019-01-16


    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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