Pane having improved properties

• US 5,585,188 A
• Filed: 05/30/1995
• Issued: 12/17/1996
• Est. Priority Date: 06/22/1993
• Status: Expired due to Term

• Current Assignee: Saint-Gobain Vitrage International
• Original Assignee: Saint-Gobain Vitrage International
• Inventors: Chaussade, Pierre, Cheron, Jean
• Primary Examiner(s): Ryan, Patrick
• Assistant Examiner(s): Bahta, Abraham
• Application Number:
  US08/374,525
• Time in Patent Office: 567 Days
• Field of Search: 428/76, 428/426, 428/437, 428/911, 428/192, 428/194, 428/343, 428/417, 428/423.1, 428/68, 428/424.2, 428/34, 428/425.6, 428/428, 428/913, 52/308, 52/399
• US Class Current: 428/426
• CPC Class Codes: B32B 17/10155 Edge treatment or chamfering
• CPC Class Codes: B32B 17/10302 Edge sealing
• CPC Class Codes: C03C 17/32 with synthetic or natural resins C03C17/30 takes precedence
• CPC Class Codes: Y10S 428/911 Penetration resistant layer
• CPC Class Codes: Y10S 428/913 Material designed to be responsive to temperature, light, moisture
• CPC Class Codes: Y10T 428/23 Sheet including cover or casing
• CPC Class Codes: Y10T 428/239 Complete cover or casing
• CPC Class Codes: Y10T 428/24777 Edge feature
• CPC Class Codes: Y10T 428/31525 Next to glass or quartz
• CPC Class Codes: Y10T 428/31551 Of polyamidoester [polyurethane, polyisocyanate, polycarbamate, etc.]
• CPC Class Codes: Y10T 428/31601 Quartz or glass
• CPC Class Codes: Y10T 428/3163 Next to acetal of polymerized unsaturated alcohol [e.g., formal butyral, etc.]

Abstract

The invention concerns a monolithic or laminated pane of glass or of plastic materials which contains at least one glass sheet (8, 9). The edge face of the glass sheet is at least partly covered with a protective strip (11, 12) of elastomeric material which has a hardness less than 90 shore A. The protected strip is adhered to the edge face. The strip serves to protect the sheet from any shock or impact it receives during processing prior to assembly into a pane for use in aircraft or transportation vehicles.

Claims

1. A monolithic or laminated pane of glass or plastic material for use in aircraft or transportation vehicles comprising at least one sheet of glass or plastic having an edge face, and a protective strip of elastomeric material adhered to said edge face and at least partly covering said edge face, said strip having a hardness less than 90 Shore A.

2. A pane as set forth in claim 1, wherein said elastomeric material of said protective strip is selected from the group consisting of silicone or polyurethane.

3. A pane as set forth in claim 2, wherein said elastomeric material is a polyurethane.

4. A pane as set forth in claim 3, wherein said polyurethane has a Shore A hardness in the range between 60 and 90 Shore A.

5. A pane as set forth in claim 1, wherein said strip has a tear resistance higher than 2 kg, measured according to ASTM 1938.

6. A pane as set forth in claim 1, wherein said elastomeric strip has a thickness between 0.1 and 2 mm.

7. A pane as set forth in claim 1, wherein said elastomeric strip includes an adhesive film component for bonding said protective strip to said edge and said adhesive film component of said strip has a thickness in the range 0.01 to 0.2 mm.

8. Pane according to claim 7, characterized in that the adhesive film is of the acrylic type.

9. A pane as set forth in claim 7, wherein said strip is capable of being unrolled from an unreeling device.

10. A pane as set forth in claim 1, which further comprises a seal mounted as the periphery of the pane, said strip being located between the edge of said glass or plastic and the inner surface of said seal.

11. A pane according to claim 1, wherein said pane comprises glass and said glass is chemically toughened.

12. A pane according to claim 1, wherein said pane is laminated.

13. A pane according to claim 4, wherein said pane is laminated.

14. A pane according to claim 10, wherein said pane is laminated.

20. Pane according to claim 1, characterized in that the edge face of the pane is rounded.

15. In the process of preparing a glass laminate for aircraft, said glass laminate comprising a plurality of glass sheets having edge faces, the improvement comprising adhesively boding a protective strip of elastomeric material to at least part of the edge face of at least one of said glass sheets prior to assembly and lamination of said sheets to form a laminated assembly.

16. The process of claim 15, wherein at least those sheets exposed to the pressure and temperature obtained inside the aircraft are protected by said elastomeric strip.

17. The process of claim 15, wherein said laminate is composed of three glass sheets and the edge faces of all of said glass sheets are protected by said strip.

18. The process of claim 15, wherein after lamination, said glass sheets are intimately bonded together and a silicone seal is subsequently molded onto the periphery of the laminated pane, said strips being intermediate the silicone seal and said edge faces of said glass sheets.

19. The process of claim 15, wherein said strip is unrolled from an unreeling device and immediately afterwards is applied against the edge face of at least one of said sheets.