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.


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    Titel :

    Aircraft fuel pump


    Beteiligte:
    EGNER JOHN (Autor:in) / BRADSHAW NIGEL (Autor:in)

    Erscheinungsdatum :

    18.08.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / H05K PRINTED CIRCUITS , Gedruckte Schaltungen



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