GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY

The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by means of an adhesive interlayer (115). The glazed assembly also...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	TONDU, Thomas
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES TRANSPORTING VEHICLES IN GENERAL WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES
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Beschreibung
Zusammenfassung:	The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by means of an adhesive interlayer (115). The glazed assembly also comprises: - a retaining element (120), a first portion (121) of which is fixedly inserted into at least the adhesive interlayer and a second portion (122) of which extends the first portion outside of the glazing; - a plurality of cleats (130) arranged in respective cavities (140) formed in the glazing in such a way that the cleats extend through the first portion and into each of the structural plies.