Two systems of a first pump unit and a third pump unit that supply fuel of a fuselage fuel tank, and a second pump unit and a fourth pump unit that supply fuel of fuel tanks in both right and left wings are provided corresponding to a left-wing engine and a right-wing engine, respectively. A supply source of the fuel to be supplied to the left-wing engine or the right-wing engine is switched by switching of the pump unit to be turned on.


    Access

    Download


    Export, share and cite



    Title :

    Fuel supply apparatus for aircraft engine


    Contributors:

    Publication date :

    2019-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



    FUEL SUPPLY APPARATUS FOR AIRCRAFT ENGINE

    MORIOKA NORIKO / OYORI HITOSHI | European Patent Office | 2017

    Free access

    FUEL SUPPLY APPARATUS FOR AIRCRAFT ENGINE

    MORIOKA NORIKO / OYORI HITOSHI | European Patent Office | 2020

    Free access


    METHOD OF FUEL SUPPLY FROM MULTI-COMPACTMENT FUEL TANK INTO AIRCRAFT ENGINE

    KLIKODUEV NIKOLAJ GRIGOR EVICH / MISHCHENKO ANATOLIJ PETROVICH | European Patent Office | 2015

    Free access

    FUEL SUPPLY APPARATUS FOR TESTING ENGINE

    KIM EUN JONG / JEONG SANG SEOP / KIM DONG SIK et al. | European Patent Office | 2016

    Free access