Abstract: A laminated glazing includes a first transparent sheet intended, in the mounting position of the glazing, to constitute the exterior face thereof, a second transparent sheet bonded to the first by an adhesive interlayer, a heating layer supplied with electric current by leads positioned at the periphery of the glazing, and a mask also positioned at the periphery of the glazing between the first transparent sheet and the leads so as to hide the latter from view from the outside in the mounting position of the laminated glazing, wherein the heating layer and the mask are on the same plane of the laminated structure of the glazing.

Abstract: An aircraft window composed of a monolithic interior pane made of polymer material and of a laminated exterior pane made of glass that are separated by an air-filled space, wherein the laminated exterior pane consists of two glass sheets bonded by an adhesive interlayer, and wherein the thickness of the exterior glass sheet is between 0.2 and 2.6 mm, and the thickness of the interior glass sheet is between 0.2 and 2.1 mm.

Abstract: An aeronautical glazing unit includes at least one sheet of modified acrylic, wherein the sheet is combined with at least one other sheet of modified acrylic, and/or at least one sheet of cast poly(methyl methacrylate) (PMMA), and/or at least one sheet of another transparent polymer such as polycarbonate (PC), and/or at least one sheet of glass in particular that is chemically strengthened, as a laminated and/or multiple glazing unit.

Abstract: A laminated glazing unit includes one to ten first glass sheets each of thickness included between 1.5 and 22 mm, if needs be adhesively bonded to one another by one or more first adhesive interlayers, and a second glass sheet forming one of the two faces of the laminated glazing unit, of thickness included between 0.5 and 1.5 mm, and adhesively bonded to the first glass sheet(s) by a second adhesive interlayer, the second glass sheet being made of aluminosilicate or soda-lime glass that is chemically toughened, having a surface stress comprised between 300 and 1000 and between 200 and 500 MPa, respectively, and a depth under compression between 20 and 100 ?m.

Abstract: An aeronautical glazing unit includes at least one sheet of modified acrylic, wherein the sheet is combined with at least one other sheet of modified acrylic, and/or at least one sheet of cast poly(methyl methacrylate) (PMMA), and/or at least one sheet of another transparent polymer such as polycarbonate (PC), and/or at least one sheet of glass in particular that is chemically strengthened, as a laminated and/or multiple glazing unit.

Abstract: A glazing includes a transparent polymer material sheet having a thickness of from 5 to 25 mm and a glass sheet having a thickness of between 0.5 and 1.5 mm, which are bonded to one another by an adhesive interlayer, the hardness of which at a temperature at least equal to ?5° C. is at most equal to 70 Shore A and the thickness of which is a decreasing function of the thickness of the glass sheet, an adhesive interlayer thickness of 2.5 mm being sufficient for a glass sheet thickness of 0.55 mm and an adhesive interlayer thickness of 1.25 mm being sufficient for a glass sheet thickness of 1.25 mm.

Abstract: A laminated glazing unit includes one to ten first glass sheets each of thickness included between 1.5 and 22 mm, if needs be adhesively bonded to one another by one or more first adhesive interlayers, and a second glass sheet forming one of the two faces of the laminated glazing unit, of thickness included between 0.5 and 1.5 mm, and adhesively bonded to the first glass sheet(s) by a second adhesive interlayer, the second glass sheet being made of aluminosilicate or soda-lime glass that is chemically toughened, having a surface stress comprised between 300 and 1000 and between 200 and 500 MPa, respectively, and a depth under compression between 20 and 100 ?m.

Abstract: A glazing includes a transparent polymer material sheet having a thickness of from 5 to 25 mm and a glass sheet having a thickness of between 0.5 and 1.5 mm, which are bonded to one another by an adhesive interlayer, the hardness of which at a temperature at least equal to ?5° C. is at most equal to 70 Shore A and the thickness of which is a decreasing function of the thickness of the glass sheet, an adhesive interlayer thickness of 2.5 mm being sufficient for a glass sheet thickness of 0.55 mm and an adhesive interlayer thickness of 1.25 mm being sufficient for a glass sheet thickness of 1.25 mm.

Abstract: The invention relates to a glazing comprising a glass substrate and a complex sheet made of a plastic comprising a plasticized polyvinyl butyral layer and a polyester film provided with a scratch-resistant and abrasion-resistant coating, an adhesive layer of thermoplastic polyurethane being inserted between the glass substrate and the polyvinyl butyral layer of the complex sheet of plastic, characterized in that the adhesion of the polyester film to the polyvinyl butyral layer, measured by exerting on a 1 cm wide strip of the polyester film a tensile force perpendicular to the surface of the glazing with a pull rate of 5 cm/min, is at least equal to 3 daN/cm. It also relates to the application of such a glazing for an airborne transport vehicle in particular.

Abstract: Iron-base alloys having a high elastic limit after quenching and ageing and resistant to corrosion by seawater, have the following composition, by weight:______________________________________ C less than 0.15% Mn less than 2% Si less than 1.5% S + P less than 0.03% Ni 34-40% Cr 16-21% Co 6-18% Mo 2-3.5% Al less than 0.25% Ti 2.5-3.5% W less than 2% B less than 0.