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 :

    ТОПЛИВНЫЙ НАСОС ЛЕТАТЕЛЬНОГО АППАРАТА


    Erscheinungsdatum :

    2019-05-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT