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.
SEAL FOR A GLAZED ELEMENT OF AN AIRCRAFT
27.06.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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