A fuel system for an aircraft includes a fuel collector downstream of a boost pump and upstream of an engine fuel pump. Said fuel collector (is mounted in a fuel tank and of an open bowl shape so as to collect fuel therein permitting fuel to continuously overflow therefrom. The system further comprises an inverted fuel collector extending over said fuel collector.


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    Title :

    FUEL FEED SYSTEM


    Additional title:

    KRAFTSTOFFZUFÜHRSYSTEM
    SYSTÈME D'ALIMENTATION EN CARBURANT


    Contributors:

    Publication date :

    2018-09-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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