In an embodiment, the present invention provides an aircraft fuel pump assembly including: a pump; a canister to enclose the pump and mount the pump within an aircraft fuel tank; and a discrete electronics unit mounted remotely to the pump. In another embodiment, the present invention provides a manhole cover for an aircraft, comprising an integral mounting for an electronics unit.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT FUEL PUMP


    Additional title:

    FLUGZEUGKRAFTSTOFFPUMPE
    POMPE À CARBURANT D'AÉRONEF


    Contributors:
    EGNER JOHN (author) / BRADSHAW NIGEL (author)

    Publication date :

    2021-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    AIRCRAFT FUEL PUMP

    EGNER JOHN / BRADSHAW NIGEL | European Patent Office | 2018

    Free access

    AIRCRAFT FUEL PUMP

    EGNER JOHN / BRADSHAW NIGEL | European Patent Office | 2016

    Free access

    Aircraft fuel pump

    EGNER JOHN / BRADSHAW NIGEL | European Patent Office | 2020

    Free access

    AIRCRAFT FUEL PUMP

    EGNER JOHN / BRADSHAW NIGEL | European Patent Office | 2020

    Free access

    AIRCRAFT FUEL PUMP SYSTEMS

    RIBAROV LUBOMIR A / VEILLEUX JR LEO J | European Patent Office | 2018

    Free access