Patent Application
20220250731
The present invention relates to a low-drag lightweight aircraft window, that is to say which, under the effect of the pressurization of the interior volume of the aircraft in flight, does not deform by forming with respect to the surrounding body of the plane, a bulge that is detrimental from an aerodynamic point of view and from the point of view of the energy consumption for propelling the aircraft.
Particularly targeted here are the windows of the type having two panes separated by an air-filled space. Such aircraft windows with two poly(methyl methacrylate) (PMMA) panes are known. In the event of rupture of the exterior pane, the interior pane makes it possible to keep the interior volume of the aircraft under a desired pressure. Even though the interior pane (or the peripheral seal with which it is in contact) is commonly provided with a small through-hole that makes it possible to keep the air-filled space under the pressure of the interior volume of the aircraft in flight under normal conditions, this interior pane is capable of keeping this interior volume of the aircraft under a desired pressure in flight in the event of rupture of the exterior pane, since this hole is sufficiently small; in this case, whistling may occur.
Document US 2015/047275 A1 describes an aircraft window composed of a monolithic interior pane made of polymer material and a laminated exterior pane made of glass which are separated by an air-filled space, but does not describe the structural features of the laminated exterior pane.
The inventors have become aware that the heavy and thick exterior pane made of monolithic polymer material could be replaced by a lighter laminate made of glass, of which it was possible to select the constituents so that, under the flight conditions, the exterior surface of the laminate matches the curvature of the surrounding fuselage of the aircraft.
For this purpose, one subject of the invention is an aircraft window composed of a monolithic interior pane made of polymer material and a laminated exterior pane made of glass which are separated by an air-filled space, characterized in that the laminated exterior pane consists of two sheets of glass bonded by means of an adhesive interlayer, in that 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. The constituents of the laminated exterior pane made of glass, in particular the glass sheets, are selected and sized in order to obtain in particular a flexural stiffness of the exterior pane such that, under the effect of the pressurization of the interior volume of the aircraft in flight, the curvature of the exterior surface of this pane is substantially the same as that of its fitting environment (fuselage of the aircraft), guaranteeing the best aerodynamics of the assembly. The terms “interior” and “exterior” refer here to the interior and exterior of the aircraft.
It should be emphasized that the exterior surface of the window in contact with the air is made of glass, which is advantageous compared to a material such as poly(methyl methacrylate) (PMMA) or the like which, directly abraded by the air friction, loses good optical qualities of transparency, unlike glass, making it necessary, after a certain number of hours of flight, to repolish the PMMA. The invention therefore makes it possible to dispense with this maintenance operation.
The use, in accordance with the invention, of a laminated exterior pane made of glass, makes it possible to integrate an adhesive interlayer with an acoustic damping property, as will be seen in greater detail in the exemplary embodiments below.
The use of the laminated glass also enables the integration of functional layers within the laminated structure, such as solar control or low-emissivity layers protected both from exterior and interior atmosphere, layers for modifying light transmission (SPD (Suspended Particle Device) or electrochromic layers). Some of these layers, in particular metal layers, may be formed in motifs or patterns with holes with no layer, capable of enabling the passage of GSM, 3G, 4G, 5G waves and the like.
It is also advantageous to provide the face of the window in contact with the outside air with a layer for modifying the surface tension such as a hydrophobic, hydrophilic or even active layer such as a photocatalytic layer of the type having TiO2 nanoparticles with a self-cleaning effect, without departing from the scope of the invention.
The structure of the window of the invention also facilitates the integration of antennas such as Wi-Fi antennas.
According to particular embodiments:
The appended drawing illustrates the invention:
With reference to this drawing, the window comprises a monolithic interior pane 1 made of poly(methyl methacrylate) (PMMA) or polycarbonate (PC) having a thickness of between 2.5 and 12 mm, for example made of 4 mm thick PMMA, and a laminated outer pane 2 made of glass that are separated by an air-filled space 3.
Several compositions of laminated exterior pane 2 in accordance with the invention are given below, in the order: exterior glass sheet 4/adhesive interlayer 6/interior glass sheet 5:
The glass used is chemically toughened, of soda-lime, aluminosilicate or borosilicate type.
The monolithic interior pane 1 and the laminated exterior pane 2 are fitted to the structure of the aircraft (aluminum fitting 7) by means of a silicon seal 8.
These window structures, in particular those of the laminated exterior pane 2 made of glass cited above, make it possible to lighten the window while avoiding a deformation as an excessively large bulge in flight, which is unfavorable from an aerodynamic point of view.
| Number | Date | Country | Kind |
|---|---|---|---|
| 1908521 | Jul 2019 | FR | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2020/068542 | 7/1/2020 | WO |
