A seal of a glazed element of an aircraft, the seal being configured to receive an edge of a first glazed unit, the first glazed unit having a first face, the seal including a first surface adapted to be mounted on the first face so as to receive the first glazed unit, wherein the seal includes a first damping part, the first damping part including the first surface, and wherein a first material forming the first damping part has a first loss factor η1 strictly greater than 0.10.


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    Title :

    SEAL FOR A GLAZED ELEMENT OF AN AIRCRAFT


    Contributors:

    Publication date :

    2024-06-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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