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.

Abstract: An assembly of a laminated glazed unit and the peripheral seal thereof, the laminated glazed unit including a transparent structural block, the peripheral seal having a first spacer part between the external surface of the structural block and a windowpane retainer, and a second spacer part between the internal surface of the structural block and the mounting structure, at least one of the contact surface between the first spacer part and the windowpane retainer and/or between the second spacer part and the mounting structure approaching the structural block, from the edge of the latter to the central part thereof; and the application of this assembly to a clamped glazed unit in the field of aeronautics or railways.