SEMI-RIGID FLEXIBLE DUCT

• US 20100154914A1
• Filed: 12/23/2009
• Published: 06/24/2010
• Est. Priority Date: 03/24/2006
• Status: Active Grant

• Current Assignee: G.L.V. International Ltd.
• Original Assignee: Graeme Liebson, Robert Cohen, Steven Liebson
• Inventors: LIEBSON, Graeme, LIEBSON, Steven, COHEN, Robert
• Granted Patent: US 8,439,085 B2
• Time in Patent Office: Days
• US Class Current: 138/122
• CPC Class Codes: B29D 23/001 Pipes; Pipe joints pleated hoses B29D23/18
• CPC Class Codes: D06F 58/20 General details of domestic laundry dryers D06F59/00 takes precedence
• CPC Class Codes: F16L 11/081 comprising one or more layers of a helically wound cord or wire in combination with braided layers F16L11/088
• CPC Class Codes: F16L 11/112 having reinforcements embedded in the wall
• CPC Class Codes: F16L 11/24 wound from strips or bands F16L11/16 takes precedence
• CPC Class Codes: F16L 59/153 for flexible pipes
• CPC Class Codes: F24F 13/0218 Flexible soft ducts, e.g. ducts made of permeable textiles
• CPC Class Codes: Y10T 29/5185 Tube making
• CPC Class Codes: Y10T 29/5191 Assembly
• CPC Class Codes: Y10T 428/1393 Multilayer [continuous layer]

Abstract

A semi-rigid, flexible duct including a pair of coaxial sleeves, namely an inner sleeve and an outer sleeve disposed parallel to and about the inner sleeve and a resilient wound element disposed between the sleeves. Each of the inner sleeve and the outer sleeve constitutes an aluminum foil ribbon. The wound element imparts corrugations to the two sleeves, such that the duct is extendible between a compacted configuration suitable for storage and for shipping and an extended configuration suitable for installation in a gas transport arrangement. Both the inner sleeve and the outer sleeve are of a predetermined thickness rendering the duct substantially rigid when in an extended configuration and enabling the duct to maintain its substantial rigidity upon extension from a compacted configuration. Optionally, at least one of the sleeves further includes a second, plastic layer bonded to the aluminum foil ribbon layer.

Claims

1. A semi-rigid, flexible duct having an axis running the length of said duct and having an inner and outer surface, comprising:

a pair of coaxial sleeves, including an inner sleeve and an outer sleeve disposed parallel to and about said inner sleeve; and

a resilient wound element disposed between said inner sleeve and said outer sleeve,

wherein each of said inner sleeve and said outer sleeve constitutes an aluminum foil ribbon layer,

wherein each of said sleeves has metallic properties,

wherein said wound element imparts corrugations to said inner sleeve and said outer sleeve, such that said duct is axially extendible between a compacted configuration suitable for storage and for shipping and an extended configuration suitable for installation in an air transport arrangement;

and wherein said layers of both said inner sleeve and said outer sleeve are of a predetermined thickness rendering said duct substantially rigid when in said extended configuration and enabling said duct to maintain its substantial rigidity upon extension from said compacted configuration.

2. The duct of claim 1, wherein said duct is in said extended configuration after having been compressed to said compacted configuration, said inner sleeve having an inward-facing surface being substantially smooth and featureless except for said wound corrugations.

3. The duct of claim 1, wherein both said aluminum foil ribbon layer of said inner sleeve and said aluminum foil ribbon layer of said outer sleeve are of a thickness in a range of 24 to 35 microns.

4. The duct of claim 1, wherein said duct has a cross-sectional configuration selected from the group which consists of:

a circular configuration, a polygonal configuration and a compound configuration wherein said duct is partially circular and partially polygonal.

5. The duct of claim 1, wherein, when a predetermined length L of said duct, of diameter d, is in the extended configuration and is disposed horizontally and supported at a first end thereof, said duct is operative to bend under the influence of gravitational force such that a second unsupported end thereof is lower than said first supported end by no more than y, such that (y/L)×

100≦

p, wherein p is a predetermined percentage of L.

6. The duct of claim 1, wherein, when a predetermined length L of said duct, of diameter d, is in the extended configuration and is disposed horizontally and supported at both ends thereof, said duct is operative to bend under the influence of gravitational force such that the central portion thereof is lower than the level of said supported ends by no more than c, such that (c/L)×

100≦

q, wherein q is a predetermined percentage of L.

7. The duct of claim 3, wherein, when L=2 meters and d=10 centimeters, c≦

0.005 L, and wherein, when said duct is in said extended configuration upon extension from said compacted configuration, c≦

0.025 L.

8. The duct of claim 1, wherein said inner sleeve is bonded to said outer sleeve with a fire-retardant adhesive.

9. The duct of claim 1, wherein each of said inner sleeve and said outer sleeve are fabricated of aluminum ribbon of predetermined thicknesses, and wherein said inner sleeve is an inner wound wrapping with a predetermined overlap of said inner sleeve and said outer sleeve is an outer wound wrapping with a predetermined overlap of said outer sleeve.

10. The duct of claim 1, wherein said resilient wound element is fabricated of a metal having spring-like resilience.

11. The duct of claim 10, wherein said resilient wound element is a wound galvanized wire.

12. The duct of claim 10, wherein said galvanized wire has a diameter in the range of 0.9 to 1.3 millimeters.

13. The duct of claim 1 further comprising:

a second, plastic layer bonded to said first foil layer of at least one of said inner sleeve and said outer sleeve.

14. The duct of claim 13, wherein each of said inner sleeve and said outer sleeve includes a second, plastic layer bonded to said first foil layer, forming thereby, respectively, an inner two-layer laminate and an outer two-layer laminate.

15. The duct of claim 14, wherein both said inner two-layer laminate and said outer two-layer laminate are fabricated of fire-resistant materials and wherein said second, plastic layers of both said inner two-layer laminate and said outer two-layer laminate are fabricated of puncture-resistant materials.

16. The duct of claim 14, wherein said second plastic layer of both said inner two-layer laminate and said outer two-layer laminate is bonded to said first layer thereof with a fire-retardant adhesive.

17. The duct of claim 13, wherein said first layers of said inner two-layer laminate and said outer two-layer laminate are fabricated of aluminum ribbon of predetermined thicknesses and said second, plastic layers of said inner two-layer laminate and said outer two-layer laminate are fabricated of polyester ribbon of predetermined thicknesses, and wherein said aluminum ribbon of said inner two-layer laminate is bonded to said polyester ribbon to form an inner two-layer laminated tape of predetermined thickness, and said aluminum ribbon of said outer two-layer laminate is bonded to said polyester ribbon thereof so as to form an outer two-layer laminated tape of predetermined thickness, and wherein said inner two-layer laminate is an inner wound wrapping with a predetermined overlap of said inner two-layer laminated tape and said outer two-layer laminate is an outer wound wrapping with a predetermined overlap of said outer two-layer laminated tape.

18. The duct of claim 14, wherein said second plastic layer of both said inner two-layer and said outer two-layer laminate is fabricated of polyester ribbon of a thickness in the range of 10 to 14 microns, and wherein said aluminum ribbon layer of said inner sleeve is of a thickness in a range of 6 to 12 microns and said aluminum ribbon layer of said outer sleeve is fabricated of aluminum ribbon of a thickness in the range of 24 to 35 microns.

19. The duct of claim 14, wherein said resilient wound element is aligned with said inner wound wrapping so as to be approximately centered over said overlap of said inner wound wrapping of said inner two-layer laminated tape, and said outer wound wrapping of said outer two-layer laminated tape is aligned with said resilient wound element so that said overlap of said outer wound wrapping of said outer two-layer laminated tape is approximately centered over the spaces between the windings of said resilient wound element.

20. The duct of claim 14, wherein, said second plastic layer of said inner sleeve is disposed parallel to and about said first layer thereof;

and said first layer of said outer sleeve is disposed parallel to and about said second plastic layer thereof.

21. The duct of claim 13, further including an insulating sheath, disposed parallel to and about said outer sleeve, and an enclosing jacket disposed parallel to and about said insulating sheath.

22. The duct of claim 21, wherein said insulating sheath is fabricated of fiberglass of a thickness in the range 25 to 60 millimeters.

23. The duct of claim 21, wherein said enclosing jacket is a multi-layer jacket including a tubular, plastic inner wrapping and a two-layer laminate outer wrapping disposed parallel thereto and thereabout and bonded thereto,

wherein said two-layer laminate outer wrapping includes a plastic inner layer and an outer layer having metallic properties, bonded together.

24. The duct of claim 23, wherein said plastic inner wrapping is fabricated of polyester ribbon of predetermined thickness and wherein said plastic inner layer of said two-layer laminate outer wrapping is fabricated of polyester ribbon of predetermined thickness and said outer layer having metallic properties of said two-layer laminate outer wrapping is fabricated of aluminum ribbon of predetermined thickness.

25. The duct of claim 23, wherein said tubular, plastic inner wrapping and said two-layer laminate outer wrapping are bonded together with a fire-retardant adhesive and wherein said polyester ribbon and said aluminum ribbon of said two-layer laminate outer wrapping are bonded together with a fire-retardant adhesive.

26. The duct of claim 23, wherein said plastic inner wrapping is fabricated of polyester ribbon of a thickness in the range of 10 to 14 microns and said plastic inner layer of said two-layer laminate outer wrapping is fabricated of polyester ribbon of a thickness in the range of 10 to 14 microns and said outer layer having metallic properties of said two-layer laminate outer wrapping is fabricated of aluminum ribbon of a thickness in the range of 6 to 9 microns.

27. The duct of claim 1, wherein said duct is selected from the group which consists of:

a gas transport duct; and

a duct for enclosing utility supply lines.

28. The duct of claim 1, wherein said duct has a cross-sectional configuration selected from a group which consists of:

circular, polygonal, square; and

rectangular configuration.

29. A method for manufacturing a semi-rigid, flexible duct, comprising the steps of:

a) providing a mandrel of preselected diameter for fabricating a duct therearound;

b) providing a first continuous aluminum ribbon of predetermined thickness;

c) providing a second continuous aluminum ribbon of predetermined thickness;

d) wrapping said first continuous ribbon with a predetermined overlap around said mandrel to form an inner sleeve;

e) winding a wire around said inner sleeve; and

f) wrapping said second continuous ribbon with a predetermined overlap around said inner sleeve and the wire winding to form an outer sleeve disposed parallel to and about said inner sleeve, thereby to form a duct.

30. The method of claim 29, wherein in said step f) of wrapping said second ribbon, the outer sleeve is bonded to said inner sleeve using a fire-retardant adhesive with the wire wound around said outer sleeve and said inner sleeve.

31. The method of claim 29, wherein said step e) of winding a wire includes the sub-step of aligning said wire with the overlap of said first ribbon so that the wire is approximately centered over the overlap of said first ribbon, and wherein said step f) of wrapping said second ribbon includes the sub-step of aligning said second ribbon so that the overlap thereof is approximately centered over the spaces between the wire windings.

32. The method of claim 29 for manufacturing a semi-rigid flexible duct, wherein said step b) further includes combining said first continuous aluminum ribbon of predetermined thickness with a first continuous polyester ribbon of predetermined thickness to form a first continuous two-layer laminated tape, and

wherein said step c) further includes combining said second continuous aluminum ribbon of predetermined thickness with a second continuous polyester ribbon of predetermined thickness to form a second continuous two-layer laminated tape.

33. The method of claim 32, wherein said step b) of combining said first aluminum ribbon with said first polyester ribbon includes the sub-step of applying a fire-retardant adhesive between said first aluminum ribbon and said first polyester ribbon to bond them together;

and wherein said step c) of combining said second aluminum ribbon with said second polyester ribbon includes the sub-step of applying a fire-retardant adhesive between said second aluminum ribbon and said second polyester ribbon to bond them together.

34. The method of claim 29, further including, after said step f) of wrapping said second aluminum ribbon, the steps of:

g) sheathing the outer sleeve with a fiberglass insulating sheath, disposed parallel thereto and thereabout; and

h) enveloping the insulating sheath with an enclosing jacket.

35. The method of claim 32, wherein said step e) of winding a wire includes the sub-step of aligning the wire with the overlap of the first two-layer laminated continuous tape so that the wire is approximately centered over the overlap of the first two-layer laminated continuous tape, and wherein said step f) of wrapping the second two-layer laminated continuous tape includes the sub-step of aligning the second two-layer laminated continuous tape so that the overlap thereof is approximately centered over the spaces between the wire windings.

36. The method of claim 29, wherein said step d) of winding said first aluminum ribbon, said step e) of winding the wire, and said step f) of winding said second aluminum ribbon, are performed by rotating said mandrel as said first aluminum ribbon, the wire, and said second aluminum ribbon are respectively taken up by said mandrel, continuously and with predetermined phase differences therebetween, with respect to the rotation of said mandrel.

37. The method of claim 29, wherein said step d) of winding said first aluminum ribbon and said step e) of winding the wire are performed continuously and with a first preselected phase difference therebetween, with respect to the rotation of said mandrel;

and wherein said step e) of winding the wire and said step f) of winding said second aluminum ribbon are performed continuously and with a second preselected phase difference therebetween, with respect to the rotation of said mandrel.

38. The method of claim 34, wherein said step h) of enveloping includes the following sub-steps:

1) providing a mandrel of preselected diameter for fabricating the enclosing jacket therearound;

2) combining a polyester continuous ribbon of predetermined thickness with an aluminum continuous ribbon of predetermined thickness to form a two-layer laminated continuous tape;

3) wrapping a continuous polyester ribbon of predetermined thickness around said mandrel to form an inner plastic sleeve; and

4) wrapping said continuous two-layer laminated tape around said inner plastic sleeve with said polyester ribbon facing inward toward said mandrel and said aluminum ribbon facing outwardly with respect to said mandrel to form an outer two-layer sleeve disposed parallel to and about said inner plastic sleeve.

39. The method of claim 38, wherein said sub-step 2) of combining includes the sub-sub-step of applying a fire-retardant adhesive between said polyester ribbon and said aluminum ribbon of said continuous two-layer laminated tape to bond them together.

40. The method of claim 38, wherein said sub-step 3) of winding a polyester ribbon includes the sub-sub-step of coating the outer face of said inner plastic sleeve with a fire-retardant adhesive to bond it to said two-layer laminated tape.

41. The method of claim 38, wherein said sub-steps 3) and 4) are performed by rotating said mandrel as said polyester ribbon and said two-layer laminated tape are respectively taken up by said mandrel, continuously and with a predetermined phase difference therebetween, with respect to the rotation of said mandrel.

42. The method of claim 38, wherein said sub-steps 3) and 4) of winding a polyester ribbon and winding the two-layer laminated tape are performed continuously and with a phase difference of 360 degrees therebetween, with respect to the rotation of said mandrel.

43. The method of claim 38, wherein in said sub-step 3) of winding a polyester ribbon, said polyester ribbon of said inner plastic sleeve is of a thickness in the range 10 to 14 microns;

and wherein, in said sub-step

     2) of combining, said polyester ribbon of said continuous two-layer laminated tape is of a thickness in the range 10 to 14 microns and said aluminum ribbon of said continuous two-layer laminated tape is of a thickness in the range 6 to 9 microns.

44. The method of claim 38, and further including, after said step f) of wrapping, the additional step of imparting to at least a portion of said duct, a polygonal cross-sectional configuration.

45. The method of claim 44, and wherein said additional step of imparting a polygonal cross-sectional configuration to at least a portion of said duct comprises imparting thereto a square or rectangular cross-sectional configuration.

46. The method of claim 29, wherein said first continuous aluminum ribbon and said second continuous aluminum ribbon maintain a substantially constant and identical tension, while being wrapped around said mandrel, in the range of 65-70 kgf, and wherein said wire is also maintained in the same said tension of both said aluminum ribbons.

47. The method of claim 46, wherein said mandrel comprises a plurality of rollers each mounted so as to be individually rotatable on a fixed plate at a predetermined angle, each comprising a set of precision-shaped grooves for accepting said wire, and wherein said grooves are precision-spaced apart in order to accept a predetermined flow of said wire, established by said predetermined angle of said rollers, onto said mandrel, such that said wire becomes a spiral form within said duct being drawn off said mandrel in an automatic fashion.

48. The method of claim 47 wherein each of said rollers is mounted on said plate so as to provide a flexible spring-like action which absorbs any irregularities in said tension and irregularities associated with said wire and said ribbons.