Un ensamble de la transparencia de la aeronave (46), que comprende: una transparencia de la aeronave (48) que comprende al menos una capa (52) que tiene una superficie exterior (54) y una porción extendida (60) que define un reborde (62) y un sello de presión (10) que se acopla a la porción extendida (60) de al menos una capa (52), en donde el sello de presión (10) incluye un cuerpo del sello de presión (12), al menos un tope de compresión integrado (36) y al menos una lengüeta conductora (30).

    An aircraft transparency assembly includes an aircraft transparency (48) having at least one ply having an outer surface and an extended portion (60) . The assembly also includes a pressure seal (10) configured to engage the extended portion of the ply, wherein the pressure seal includes a pressure seal body, at least one integrated compression stop (36) and at least one conductive tab (30). The transparency can include an optional anti-static drain assembly (66) including at least one flexible conductive element having a first end in electrical contact with the outer surface of the ply, for example with an optional conductive coating (58) on the outer surface of the ply, and a second end configured to contact the pressure seal.


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    Title :

    Transparencia de las aeronaves con sello de presión y/o drenaje antiestático


    Contributors:

    Publication date :

    2021-11-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Spanish


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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