HEATING GLAZING MADE OF A STRUCTURAL PLASTIC MATERIAL

Abstract

A heated glazing includes at least one plastic structural substrate and a heating device and includes at least one transparent and electrically-conductive thin layer. The heated glazing includes, as laminate, at least one first plastic structural substrate, at least one glass sheet equipped with the heating layer, and at least one second plastic structural substrate.

Claims

1. A heated glazing comprising, as laminate, at least one first plastic structural substrate, at least one glass sheet equipped with a heating device, and at least one second plastic structural substrate.

2. The glazing as claimed in claim 1, wherein the at least one glass sheet has surface dimensions smaller than those of the first and second plastic structural substrates.

3. The glazing as claimed in claim 1, wherein the first and second plastic structural substrates are spaced apart from one another and are joined by a transparent plastic intermediate layer made of PVB or PU between 1.2 and 5 mm.

4. The glazing as claimed in claim 1, wherein the glass sheet is joined to each of the plastic structural substrates via a single-layer or multilayer plastic film made of PVB or PU.

5. The glazing as claimed in claim 1, wherein the first and second plastic structural substrates each have a thickness of between 5 and 25 mm.

6. The glazing as claimed in claim 1, wherein the plastic structural substrates are made of PMMA, or PU or PC.

7. The glazing as claimed in claim 1, wherein the glass sheet has a thickness of between 0.5 and 1.6 mm.

8. The glazing as claimed in claim 1, wherein the heating device comprises at least one transparent and electrically-conductive thin layer.

9. The glazing as claimed in claim 1, comprising two sheets consisting of the first and second plastic structural substrates and between which the glass sheet is laminated, and at least one third sheet, which is the outermost of the sheets of the glazing and facing the outside environment in the usage position of the glazing in its final destination, said third sheet being either made of plastic or forms a glass substrate.

10. The glazing as claimed in claim 1, further comprising at least one temperature probe arranged between the first and second plastic structural substrates, by being either joined to the glass sheet on the opposite face to the one equipped with the electrically-conductive layer, or arranged in the thickness of interlayer material separating the two plastic structural substrates.

11. The glazing as claimed in claim 1, wherein the whole of the periphery of the glazing forms, depending on the thickness of said glazing, an extended frame consisting solely of plastic.

12. The glazing as claimed in claim 1, comprising an outermost sheet that is configured to make a peripheral shoulder intended to house a portion of the structure that receives the glazing.

13. The glazing as claimed in claim 1, wherein the glazing is arranged in an aircraft.

14. The glazing as claimed in claim 3, wherein a thickness of said plastic intermediate layer is between 2.5 and 4 mm.

15. The glazing as claimed in claim 7, wherein the thickness of the glass sheet is between 0.5 and 0.7 mm.

16. The glazing as claimed in claim 8, wherein the electrically-conductive layer is based on tin oxide, or on tin oxide doped with indium or with fluorine, or based on metal.

17. The glazing as claimed in claim 9, wherein the thickness of the third sheet is between 1 and 3 mm.

18. The glazing as claimed in claim 9, wherein the glass substrate is a reinforced glass having a thickness of between 0.5 and 5 mm.

19. The glazing as claimed in claim 9, wherein the third sheet is joined to one of the structural substrates via a joining interlayer layer made of PU-plastic.

20. The glazing as claimed in claim 9, wherein surface dimensions of said third sheet are smaller than those of the structural substrate with which it is combined.

21. The glazing as claimed in claim 13, wherein the glazing forms an airplane cockpit side window.

Description

[0028] The present invention is now described with the aid of examples that are purely illustrative and in no way limit the scope of the invention, and using the appended drawings, in which:

[0029] FIG. 1 represents a schematic cross-sectional view of a heated glazing according to the invention;

[0030] FIGS. 2 and 3 are schematic cross-sectional views of two respective embodiment variants of the glazing from FIG. 1;

[0031] FIG. 4 is a schematic cross-sectional view of the glazing from FIG. 2 fastened in a cockpit, such as an airplane structure.

[0032] The heated glazing 1 of the invention illustrated in FIGS. 1 to 3 is intended to be fastened to the structure 2 of an airplane cockpit, as represented in FIG. 4 to form in particular a side window.

[0033] According to the invention, the heated glazing 1 comprises at least two transparent plastic structural substrates 30 and 31, an interlayer layer 32 of transparent thermoplastic connecting the two structural substrates, heating means 4 advantageously comprising a transparent electrically-conductive layer, and a support 5 for said heating means, said support 5 being embedded in the interlayer layer 32 and formed according to the invention by a thin glass sheet.

[0034] The structure 2 of the airplane has a face referred to as the outer face 20 oriented toward the environment outside of the airplane.

[0035] The two transparent plastic structural substrates 30 and 31 are for example made of PMMA. The structural substrate 30, referred to as the outer substrate since it is oriented toward the outside of the airplane, preferably has a thickness for example of 14 mm, which is greater than that of the structural substrate 31, referred to as the inner substrate since it is oriented toward the inside, having a thickness of 6 mm for example.

[0036] The intermediate layer 32 which makes it possible to join the two structural substrates is for example made of PVB or TPU. It has, for example, a thickness of 3.1 mm. There are at least two films of PVB film type in order to incorporate the thin glass sheet 5 into the glazing and join it.

[0037] The glass sheet 5 is therefore laminated between the two structural substrates 30 and 31 by means of the intermediate layer 32. The glass sheet 5 is joined by one of its faces 50 to the outer structural substrate 30 via a single-layer or multilayer PVB film 32A, and by its opposite face 51 to the outer structural substrate 31 via a second single-layer or multilayer PVB film 32B.

[0038] According to the invention, the thin glass sheet 5 forms a means of support for the deposition of the heating layer 4.

[0039] The thin glass sheet has for example a thickness of 0.7 mm.

[0040] The transparent electrically-conductive layer 4 is a thin layer deposited in a known manner on the glass, for example by PVD (physical vapor deposition) or CVD (chemical vapor deposition). Preferably, the layer is based on a doped oxide, such as ITO. It has, for example, a thickness of between 50 and 800 nm.

[0041] The heating layer covers all or some of one of the faces 50 of the glass sheet. The glass sheet 5, with its heating layer 4, is positioned in the glazing so that the heating layer 4 is facing the outer structural substrate 30.

[0042] The heating layer 4 is connected to current supply collectors or strips, not illustrated here, intended to be connected to a current source external to the glazing.

[0043] Advantageously, the glazing comprises at least one temperature probe 6 which is preferably arranged on the glass sheet 5, in particular on the face 51 of the glass sheet opposite the face 50 bearing the heating layer 4. The temperature probe comprises for example, in a known manner, thin wires of variable resistance. As a variant, the temperature probe could be placed in the thickness of the interlayer layer 32.

[0044] In the embodiment example represented in FIG. 2, the glazing 1 comprises a third sheet 7 on the outside of the glazing and therefore of the airplane. This sheet is formed of a third rigid substrate, for example with a thickness of between 1 and 3 mm, being either made of rigid plastic, such as PMMA, or made of reinforced glass (which is reinforced by thermal or chemical tempering). This third sheet 7 is joined to the outer face of the outer structural substrate 31 via a transparent plastic interlayer 70, for instance made of PU, for example with a thickness of 5 mm. The glazing of this example thus has more sheets than the embodiment example from FIG. 1, and the thickness thereof is also greater.

[0045] In the embodiment example from FIG. 3, the glazing 1 comprises only two sheets which correspond to the plastic structural substrates 30 and 31, but the thickness of the outer substrate 30, in particular made of 18 mm PMMA, is increased relative to that of the example from FIG. 1.

[0046] For the manufacture of the glazing, each structural substrate 30 and 31, the thin glass 5 (before deposition of the heating layer 4), the additional substrate 7 and the interlayer 70 are produced to the desired dimensions and shapes, then each constituent element of the glazing, structural substrates, thin glass 5 covered with the heating layer, optionally additional substrate and the interlayer thereof, and also the joining elements which are in particular the films 32A and 32B, are deposited on one another as a laminate, and finally the assembly is passed into an autoclave. As a variant, the final dimensioning of the plastic structural substrates 30 and 31 may be carried out after autoclaving, by cutting them to the desired dimensions.

[0047] To ensure the fastening of the glazing 1 of the invention in the structure of the airplane (FIG. 4), the glass sheet 5 inside the thickness of the glazing (FIGS. 1 to 3) and the third sheet 7 and its interlayer 70 for the example from FIG. 2 have surface dimensions which are smaller than the surface dimensions of the plastic structural substrates 30 and 31, in order to provide an extended peripheral frame 8 entirely made of plastic for the entire thickness of the glazing so that fixing means 80 pass solely through the plastic, as depicted in FIG. 4.

[0048] Moreover, in order to incorporate the glazing into the structure of the airplane so that the outer face 10 of the glazing 1 is coplanar with the outer face 20 of the structure of the airplane (FIG. 4), the third sheet 7 and its interlayer 70 of the embodiment example from FIG. 2 have surface dimensions smaller than those of the outer structural substrate 30, and the outer structural substrate 30 from FIG. 3 itself has a suitable shape for providing an outer peripheral shoulder 9, in which the thickness of the cabin 2 of the airplane is housed.

[0049] Of course, seals not illustrated here are provided between the glazing and the structure of the airplane.