Disclosed is a sump cover for a sump basin of a generator of an aircraft, the sump cover having: a sump cover shell shaped as an inverted bowl, a front portion of the sump cover shell including a first plurality of fastener features, each configured to fasten to one of a second plurality of fastener features in the sump basin; and a sump cover support extending outwardly from the sump cover shell, past a perimeter edge of the sump cover shell, configured to fit through a sump port and against a sump tube of the sump basin, wherein the sump cover support and the first plurality of fastener features define a multi-point mounting configuration between the sump cover and the sump basin.


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    Title :

    Sump cover assembly for generator


    Contributors:

    Publication date :

    2021-11-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16N LUBRICATING , Schmierung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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