Preformed flexible laminate

• US 5,851,609 A
• Filed: 02/27/1996
• Issued: 12/22/1998
• Est. Priority Date: 02/27/1996
• Status: Expired due to Fees

• Current Assignee: TruSeal Technologies Incorporated (Quanex Building Products Corporation)
• Original Assignee: TruSeal Technologies Incorporated (Quanex Building Products Corporation)
• Inventors: Ferri, Louis Anthony, Buchanan, Ronald Ellsworth, Baratuci, James Lynn, Ritz, Lanny Dean
• Primary Examiner(s): LONEY, DONALD J
• Application Number:
  US08/607,896
• Time in Patent Office: 1,029 Days
• Field of Search: 428/34, 428/68, 428/76, 428/182, 52/172, 52/786.13, 52/786.1, 156/107, 156/109, 49/479, 49/486, 49/488, 49/495, 264/129, 264/135, 264/176.1, 264/177.17, 264/210.1, 264/252, 264/261
• US Class Current: 428/34
• CPC Class Codes: B29C 48/07 Flat, e.g. panels
• CPC Class Codes: B29C 48/08 flexible, e.g. films
• CPC Class Codes: B29C 48/13 Articles with a cross-section varying in the longitudinal direction, e.g. corrugated pipes
• CPC Class Codes: B29C 48/15 incorporating preformed parts or layers, e.g. extrusion moulding around inserts
• CPC Class Codes: B29C 48/34 Cross-head annular extrusion nozzles, i.e. for simultaneously receiving moulding material and the preform to be coated
• CPC Class Codes: E06B 2003/6638 with coatings
• CPC Class Codes: E06B 2003/6639 sinuous
• CPC Class Codes: E06B 3/66328 of rubber, plastics or similar materials E06B3/66314, E06B3/66323 and E06B3/66342 take precedence; transparent materials E06B3/66333
• 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 428/2804 Next to metal

Abstract

A composite structure comprising a preformed flexible laminate in adhering contact with at least a first and second transparent or translucent panel members such as would be useful as an insulated glass unit. The flexible laminate contains an undulating spacer element either partially or totally embedded within a core material and has a polymeric coating on at least one surface thereof. The flexible laminate effectively seals the interior of the panel structure from air and/or moisture and maintains a desired distance between the panels. A multi-cavity extrusion die for forming the preformed flexible laminate has a core cavity for receiving the core material as well as the undulating continuous spacer element. Converging walls within the core cavity serve to embed at least one side of the spacer element in the core material and a land area forms a desired shape or configuration wherein the spacer element undulation is maintained. At least one polymeric feed cavity located downstream from said core cavity and said land area applies a polymeric film or coating to at least a surface of the embedded spacer element. A plurality of optional feed cavities can apply the same or different polymers to additional surfaces of the embedded spacer element and can totally cover or encapsulate the same.

Claims

1. A composite structure comprising;

at least a first and second transparent or translucent panel members having facing, generally parallel surfaces spaced a generally finite distance apart from each other and a unitary seal located generally along the peripheries of said first and second members, in physical contact with the facing surfaces of said members, said unitary seal comprising

a) at least one longitudinal core material

b) at least one longitudinal adhesive film in physical contact with said core material and adhering said core material to said first and second members; and

c) at least one longitudinal spacer element substantially perpendicular to the planes formed by said first and second members and having a width, measured perpendicular to said panel members, of less than or equal to said finite distance, said at least one spacing element being bendable perpendicular to its width to an angle from 2°

to 150°

without changing said width of said spacer element more than one tenth of one percent, said at least one spacing element extending substantially along the length of said unitary seal, and said at least one spacer element adhered to, partially embedded in, or embedded in said at least one longitudinal core material,

said adhesive film of said unitary seal being compositionally different than the composition of said at least one core material and at least a portion of said longitudinal core material being located between said spacer element and a gas space defined by said first and second members and said unitary seal.

2. A composite structure according to claim 1, wherein said adhesive film has greater weight percentage of tackifier resin than said at least one core material and wherein said tackifier resin has a number average molecular weight of less than 10,000.

3. A composite structure according to claim 2, wherein said adhesive film has from about 2 to about 50 weight percent of said tackifier, and said at least one core material has less than 20 weight percent of said tackifier, and said weight percent tackifier of said at least one adhesive material is at least 2 weight percent greater than in said at least one core material.

4. A composite structure according to claim 1, wherein the weight percent of desiccant in said at least one core material is greater than in said adhesive film.

5. A composite structure according to claim 4, wherein said at least one core material has from about 5 to about 50 weight percent desiccant and said at least one adhesive film has less than 12 weight percent desiccant and the weight percent of said desiccant in said at least one core material is at least 2 weight percent higher than in said adhesive film.

6. A composite structure according to claim 1, wherein the adhesive film has a greater modulus than said core material.

7. A composite structure according to claim 1, wherein the core material has a greater modulus than said adhesive film.

8. A composite structure according to claim 1, wherein said unitary seal further comprises a barrier film in direct physical contact with a space between said first and second panel members and said unitary seal and in continuous contact around inner peripheries formed from the unitary seal and said first and second panel members.

9. A composite structure according to claim 8, wherein said barrier film acts as a barrier to volatiles in said at least one or more core material from entering said sealed space.

10. A composite structure according to claim 8, wherein said barrier film has less total volatile organic materials upon exposure to U.V. in CAN/0CGSB-12.8-M90 §

4.3.3 than said unitary seal without said barrier film.

11. A composite structure according to claim 1, wherein said at least one adhesive film is comprised of a polymeric material having a primary Tg at least 5°

C. lower than the primary Tg of said at least one core material.

12. A composite structure according to claim 1, wherein the combined thermal conductivity of said at least one core material is at least 10 percent less than the thermal conductivity of said adhesive film.

13. A composite structure according to claim 1, wherein said adhesive film is curable under conditions where the at least one core material does not cure.

14. A composite structure according to claim 11, wherein said at least one spacer element comprises metal spacer element undulating along its length.

15. A composite structure according to claim 1, wherein said at least one spacer element comprises a plastic or cellulosic or crosslinked rubber or combinations thereof.

16. A composite structure according to claim 1, wherein said at least one spacer element comprises an undulating laminate of metal with cellulosic, plastic, or a crosslinked rubber.

17. A composite structure according to claim 1, wherein said core material includes a foamed polymeric material.

18. A composite structure according to claim 1, wherein said adhesive film comprises an isobutylene based polymer.

19. A composite structure according to claim 1, wherein said at least one core material comprises an isobutylene based polymer.

20. A composite structure according to claim 18, wherein said at least one core material comprises an isobutylene based polymer.

21. A composite structure according to claim 18, wherein said spacer element comprises an undulating metal strip.

22. A composite structure according to claim 21, wherein said isobutylene based polymer is at least 20 weight percent of the polymers of said adhesive film.

23. A composite structure comprising at least a first and second transparent or translucent panel members having facing, generally parallel surfaces spaced a finite distance apart from each other and a unitary seal located generally along the peripheries of said first and second members, in physical contact with the facing surfaces of said members, said unitary seal comprising

a) at least one longitudinal core material

b) at least one longitudinal adhesive film in physical contact with said core material and adhering said material to said first and second members;

and

c) at least one spacer element continuous along the length of said unitary seal having its maximum rigidity substantially perpendicular to the planes formed by said first and second members said spacer element being bendable transverse to its width at an angle from 2°

to 150°

without changing said width of said spacer element more than one tenth of one percent and said at least one spacer element adhered to, partially embedded in, or embedded in said at least one core material, p2 said at least one adhesive film being compositionally different than the core material and increasing the cycles to failure of said unitary seal by a factor of at least 1.25 with failure as defined in CAN/CGSB-12.8 M90 §

3.6.5 over a comparable unitary seal having the same spacer element and core material and wherein the adhesive film in said comparable unitary seal is identical in composition to the core material.

24. A composite structure according to claim 23, wherein said adhesive film contains a larger amount of tackifier and glass adhesion promoter on a weight percent basis than said core material.

25. A composite structure according to claim 24, wherein the factor for increasing cycles to failure over a comparable seal is at least 2.0 and wherein said adhesive film has at least 2 weight percent more tackifier and at least 0.25 weight percent more glass adhesion promoter than said core material.

26. A composite according to claim 25, wherein said adhesive film has at least 5 weight percent more tackifier and at least 0.50 weight percent more glass adhesion promoter than said core material and wherein said glass adhesion promoter is a silane compound.