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.
AIRCRAFT TRANSPARENCY WITH PRESSURE SEAL AND/OR ANTI-STATIC DRAIN
FLUGZEUGTRANSPARENZ MIT DRUCKDICHTUNG UND/ODER ANTISTATISCHEM ABLAUF
VITRAGE D'AÉRONEF AYANT UN JOINT D'ÉTANCHÉITÉ ET/OU UN DRAIN ANTISTATIQUE
2019-07-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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