A glazed assembly for an aircraft, includes a laminated glazing having a first structural ply and a second structural ply bonded to the first structural ply by an adhesive interlayer. The glazed assembly also includes a retaining element, a first portion of which is fixedly inserted into at least the adhesive interlayer and a second portion of which extends the first portion outside of the glazing, a plurality of cleats arranged in respective cavities formed in the glazing in such a way that the cleats extend through the first portion and into each of the structural plies.
GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY
2025-05-22
Patent
Electronic Resource
English
IPC: | B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
GLAZED UNIT WITH ANTENNA PLATE AND METHOD FOR MANUFACTURING THIS GLAZED UNIT
European Patent Office | 2024
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