A system and method for installing a window panel assembly into an aircraft is disclosed. In one embodiment, the system has a retaining device having an outside edge that is sealed against an inboard surface of the aircraft skin. A biasing member is mounted to an inboard edge of the retaining device, and a plurality of protrusions (which are secured onto the biasing member) press against the window panel. This pushes the window panel outward, maintaining a seal around the edge of the window.


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    Title :

    Window Assembly Installation


    Contributors:

    Publication date :

    2015-08-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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