MULTI-LAYERED TRANSPARENCY AND METHOD OF PRODUCING SUCH A MULTI-LAYERED TRANSPARENCY

• US 20140170417A1
• Filed: 12/10/2013
• Published: 06/19/2014
• Est. Priority Date: 12/13/2012
• Status: Abandoned Application

• Current Assignee: Airbus Helicopters Deutschland Gmbh (Airbus SE)
• Original Assignee: Eurocopter Deutschland Gesellschaft Mit Beschrã¤Nkter Haftung (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Kreitmair-Steck, Wolfgang, Barnerssoi, Johann
• Application Number:
  US14/101,432
• Publication Number:
  US 20140170417A1
• Time in Patent Office: Days
• US Class Current: 428/412
• CPC Class Codes: B32B 2250/40 Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
• CPC Class Codes: B32B 2307/412 Transparent
• CPC Class Codes: B32B 2307/554 Wear resistance
• CPC Class Codes: B32B 2307/584 Scratch resistance
• CPC Class Codes: B32B 2307/71 Resistive to light or to UV
• CPC Class Codes: B32B 2605/006 Transparent parts other than made from inorganic glass, e.g. polycarbonate glazings
• CPC Class Codes: B32B 2605/18 Aircraft
• CPC Class Codes: B32B 27/08 of synthetic resin
• CPC Class Codes: B32B 27/34 comprising polyamides
• CPC Class Codes: B32B 27/365 comprising polycarbonates
• CPC Class Codes: B32B 27/40 comprising polyurethanes
• CPC Class Codes: B64C 1/1484 Windows B64C1/1492 takes precedence
• CPC Class Codes: B64C 1/1492 Structure and mounting of the transparent elements in the window or windscreen
• CPC Class Codes: Y10T 428/31507 Of polycarbonate
• CPC Class Codes: Y10T 428/31562 Next to polyamide [nylon, etc.]
• CPC Class Codes: Y10T 428/31728 Next to second layer of polyamide

Abstract

A multi-layered transparency (2.1, 2.2) for an aircraft cockpit, particularly a multi-layered window for a helicopter cockpit (1), comprising: one core layer (6) made of a polymer of either PC or mcPA and at least one foil extruded, adhesive interlayer film (3.1, 3.2, 3.3) unilaterally bonded to said at least one core layer (6). At least one outer top layer (5.1, 5.2) made of mcPA, preferably containing additives, is unilaterally attached to said at least one foil extruded adhesive interlayer film (3.1, 3.2, 3.3) distal to said at least one core layer (6) and a scratch resistant outer top coating (4.1, 4.2) is provided unilaterally to said at least one outer top layer (5.1, 5.2) distal to said at least one foil extruded adhesive interlayer film (3.1, 3.2, 3.3). The invention is as well related to a method of producing such a multi-layered transparency.

Claims

1. A multi-layered transparency for an aircraft cockpit, particularly a multi-layered window for a helicopter cockpit, comprising:

one core layer made of a polymer of either polycarbonate (PC) or microcrystalline polyamide (mcPA);

at least one foil extruded, adhesive interlayer film unilaterally bonded to said at least one core layer;

at least one outer top layer made of microcrystalline polyamide (mcPA), preferably containing additives, said at least one outer top layer being unilaterally attached to said at least one foil extruded adhesive interlayer film distal to said at least one core layer; and

a scratch resistant outer top coating, provided unilaterally to said at least one outer top layer distal to said at least one foil extruded adhesive interlayer film;

wherein at least one foil extruded adhesive interlayer film comprises two foil extruded films with a functional layer in between.

2. The multi-layered transparency according to claim 1, wherein respectively one foil extruded adhesive interlayer film is bonded to either side of said one core layer:

one outer top layer made of microcrystalline polyamide (mcPA) attached to said foil extruded adhesive interlayer film distal to said at least one core layer, and

scratch resistant outer top coatings provided to either side of said outer top layers distal to said two foil extruded adhesive interlayer films.

3. The multi-layered transparency according to claim 1, wherein the functional layer is an active electro chromatic polymer, a conductive coating and/or a wire grid.

4. The multi-layered transparency according to claim 1, wherein an adhesive primer is provided for adhesion of the two foil extruded films to the functional layer.

5. The multi-layered transparency according to claim 1, wherein the outer top layer made of microcrystalline polyamide (mcPA) contains optical brighteners for UV-protection.

6. The multi-layered transparency according to claim 3, wherein the two foil extruded films are made of ionoplast compositions (IOPL), transparent thermoplastic polyurethane (TPU) or polyvinyl butyral (PVB) or a combination of ionoplast compositions (IOPL), transparent thermoplastic polyurethane (TPU) or polyvinyl butyral (PVB), one of inner contact sides in between the two foil extruded films being provided with the conductive coating as a functional layer and in that the conductive coating is provided with electrical contacts.

7. The multi-layered transparency according to claim 6, wherein the conductive coating is preferably metallic, made by physical vapour deposition (PVD) with transparent conductive oxides (TCO) e.g. indium tin oxide, or in that the functional layer is provided by a conductive wire grid.

8. The multi-layered transparency according to claim 6, wherein the conductive coating is laminated as a polymer layer with locally an active electro-chromatic component in between the foil extruded films.

9. The multi-layered transparency according to claim 7, wherein the active electro chromatic polymer, a metallic conductive coating and/or the wire grid as means for dimming/darkening being automatically switched off, if power of the aircraft is switched off or if said power is lost by an incident.

10. The multi-layered transparency according to claim 1, wherein the scratch resistant outer top coating is combined with an anti-reflective coating, said anti-reflective coating being a single layer or a multi-layer interference coating.

11. The multi-layered transparency according to claim 1, wherein 0.01 percent by weight up to about 0.1 percent by weight of an IR absorbing material is mixed into an outer top layer composition based on microcrystalline polyamide (mcPA).

12. A method of producing the multi-layered transparency according to claim 1 in four steps, preferably in clean room environment, by:

manufacturing at least one foil extruded adhesive interlayer film in a first step by treating with an adhesive primer the first foil extruded adhesive interlayer film and the second foil extruded film and by applying both films on both sides of the functional layer,

manufacturing in a second step at least one outer top layer made of microcrystalline polyamide (mcPA) and one core layer made of a polymer of microcrystalline polyamide (mcPA) or polycarbonate (PC) by either injection compression molding with temperatures of 300°

C. for the polycarbonate (PC) layers and 280°

-300°

C. for the microcrystalline polyamide (mcPA) layers, with mold temperatures in both cases of 80°

C.,

or by temperature forming/shaping of polycarbonate (PC) and microcrystalline polyamide (mcPA) sheets at temperatures between 140°

C. and 145°

C. for each individual sheet or for all sheets in one step,

assembling in a third step by laying the core layer, forming and heating between 60°

C. and 110°

C. the at least one foil extruded adhesive interlayer film around the core layer, adding the at least one outer top layer and curing the assembly in an autoclave,

coating the assembly in a fourth step by plasma treatment on at least one outer top layer.

13. The method according to claim 12, wherein sheet forming with only one mold or—

if the radii of the sheets are too small—

with several geometrically adapted molds.