Glazed assembly for an aircraft, method for manufacturing such a glazed assembly and aircraft comprising such a glazed assembly
AssigneeSaint-Gobain Sully
InventorThomas Tondu
Life of this patent
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Abstract
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.
Claims25
A glazed assembly for an aircraft, said glazed assembly comprising a laminated glazing comprising a set of structural plies including a first structural ply and a second structural ply fixed to the first structural ply by an interlayer, said glazed assembly further comprising:
- a retaining element, a first portion of which is fixedly inserted in at least said interlayer at an edge of the laminated glazing and over at least a portion of its periphery, and a second portion of which extends the first portion outside of the laminated glazing, and
- a plurality of cleats arranged in respective cavities formed in the laminated glazing so that said cleats extend substantially perpendicularly across the first portion of the retaining element and into each of said structural plies.
Dependencies are inferred from the claim text.