Method and apparatus for inserting a spacer between annular reinforcement bands

• US 9,975,300 B2
• Filed: 02/03/2017
• Issued: 05/22/2018
• Est. Priority Date: 09/20/2011
• Status: Active Grant

• Current Assignee: Milliken & Company
• Original Assignee: Milliken & Company
• Inventors: Petri, Patrick A., Vogt, Kirkland W., Dotson, Michael Edward, Marler, Rush W.
• Primary Examiner(s): Sultana, Nahida
• Application Number:
  US15/423,666
• Publication Number:
  US 20170144390A1
• Time in Patent Office: 473 Days
• Field of Search: 264262, 264257, 264313, 425403, 425389, 425393, 4254051, 428 365, 428 341
• CPC Class Codes: B29C 70/086 and with one or more layers of pure plastics material, e.g. foam layers applying a non-preformed coating, e.g. a gel-coat, B29C37/0025; with foam blocks B29C70/86
• CPC Class Codes: B29C 70/86 Incorporated in coherent impregnated reinforcing layers, e.g. by winding
• CPC Class Codes: B29D 2030/0038 Handling tyre parts or semi-finished parts, excluding beads, e.g., storing, transporting, transferring B29D2030/0044 takes precedence
• CPC Class Codes: B29D 30/2607 Devices for transferring annular tyre components during the building-up stage, e.g. from the first stage to the second stage building drum
• CPC Class Codes: B29D 99/0082 Producing articles in the form of closed loops, e.g. rings B29D29/00 takes precedence
• CPC Class Codes: B29K 2075/00 Use of PU, i.e. polyureas or polyurethanes or derivatives thereof, as moulding material
• CPC Class Codes: B29K 2105/045 with open cells
• CPC Class Codes: B29L 2023/00 Tubular articles B29L2024/00 takes precedence ; catheters B29L2031/7542
• CPC Class Codes: B32B 2266/06 Open cell foam
• CPC Class Codes: B32B 2597/00 Tubular articles, e.g. hoses, pipes
• CPC Class Codes: B32B 27/12 next to a fibrous or filamentary layer
• CPC Class Codes: B32B 27/40 comprising polyurethanes
• CPC Class Codes: B32B 5/245 another layer next to it being a foam layer

Abstract

A method is provided for making an annular reinforcement structure having inner and outer reinforcement bands maintained in concentric alignment by a resilient spacing element positioned between the bands. The method includes the steps of placing the spacing element against the inside face of the outer reinforcement band and compressing the spacing element with a jig, adjacent the top edge of the outer reinforcement band. The spacing element is sufficiently compressed to allow the inner reinforcement band to slide into concentric alignment with the outer reinforcement band, with a minimum of deflection and/or distortion of the inner reinforcement band.

Claims

1. A method of making an annular reinforcement structure having a first reinforcement band and a second reinforcement band, and a resilient spacing element positioned between the first and second reinforcement bands, maintaining the first and second reinforcement bands in a spaced apart, concentric relationship, comprising the steps of:

(a) placing the resilient spacing element against a face of the first reinforcement band;

(b) compressing the resilient spacing element against the face of the first reinforcement band, adjacent a top edge of the first reinforcement band, with a jig;

(c) sliding the second reinforcement band in an axial direction relative to the first reinforcement band, from the top edge of the first reinforcement band towards a bottom edge of the first reinforcement band, while the resilient spacing element is compressed by the jig, whereby the first and second reinforcement bands are concentric, and the jig is positioned between the resilient spacing element and the second reinforcement band; and

(d) removing the jig from between the first reinforcement band and the second reinforcement band, whereby the resilient spacing element is retained in place between the first and second reinforcement bands; and

wherein the first and second reinforcement bands are each comprised of a cord selected from the group consisting of monofilament or multi-filament yarns, and the cord is wound into a helix making at least three revolutions.

2. The method of claim 1, wherein the resilient spacing element has a thickness in the radial direction that is greater than the radial distance between the first and second reinforcement bands, when the bands are in a concentric relationship.

3. The method of claim 2, wherein the resilient spacing element is an open-cell, polymer foam having a fraction of voids to net volume of 75% or greater.

4. The method of claim 2, wherein the resilient spacing element is a reticulated, polyurethane foam having a fraction of voids to net volume of 90% or greater.

5. The method of claim 1, wherein the jig is an annular band having a circumference that is intermediate in value relative to a circumference of the first reinforcement band and a circumference of the second reinforcement band.

6. The method of claim 1, wherein the jig has a width in the axial direction that is less than a width of the first reinforcement band in the axial direction and less than a width of the spacing element in the axial direction.

7. The method of claim 6, wherein the resilient spacing element extends in the axial direction from the top of the first reinforcement band to a distance below the jig, when the resilient spacing element is compressed against the face of the first reinforcement band, and the second reinforcement band frictionally engages the resilient spacing element below the jig, prior to removal of the jig from between the second reinforcement band and the resilient spacing element.

8. The method of claim 1, wherein the resilient spacing element is an annular band comprising an open-cell, polymer foam.

9. The method of claim 1, wherein the resilient spacing element is comprised of a plurality of discrete shims comprising an open-cell, polymer foam.

10. The method of claim 1, wherein the jig is comprised of a plurality of plates, which are spaced around a circumference of the first reinforcement band, each of the plurality of plates has a curved surface corresponding to a curvature of the first reinforcement band, and the curved surfaces engage the spacing element when the plurality of plates is moved from a retracted position to an extended position.

11. The method of claim 1, wherein the jig is an annular band.

12. A method of making an annular reinforcement structure, comprising the steps of:

(a) placing a resilient spacing element against an inside face of an outer reinforcement band, wherein the resilient spacing element is selected from the group consisting of (i) an annular band, and (ii) a plurality of discrete shims, arranged around a circumference of the outer reinforcement band;

(b) compressing the resilient spacing element against the inside face of the outer reinforcement band, with a jig;

(c) sliding an inner reinforcement band in an axial direction relative to the outer reinforcement band, from a top edge of the outer reinforcement band towards a bottom edge of the outer reinforcement band, while the resilient spacing element is compressed by the jig, whereby the inner reinforcement band is positioned inside the outer reinforcement band and the resilient spacing element, and the inner and outer reinforcement bands are concentric;

(d) removing the jig from between the inner reinforcement band and the spacing element, whereby the resilient spacing element is retained in place between the inner reinforcement band and the outer reinforcement band; and

wherein the jig is comprised of a plurality of plates, which are spaced inside a circumference of the outer reinforcement band, each of the plates has a convex surface, which compresses the spacing element against the inside face of the outer reinforcement band, when the plurality of plates is moved from a retracted position to an extended position.

13. The method of claim 12, wherein the resilient spacing element has a thickness in the radial direction that is greater than the radial distance between the inner and outer reinforcement bands, when the bands are concentric.

14. The method of claim 12, wherein the resilient spacing element is an open-cell, polymer foam having a fraction of voids to net volume of 75% or greater.

15. The method of claim 12, wherein the resilient spacing element is a reticulated, polyurethane foam having a fraction of voids to net volume of 90% or greater.

16. The method of claim 12, further including the step of retracting the plates, to allow the resilient spacing element to expand inward toward the inner reinforcement band and decrease the friction between the plates and the resilient spacing element, after the inner reinforcement band is positioned inside the outer reinforcement band and the resilient spacing element, and before removing the jig from between the inner reinforcement band and the resilient spacing element.

17. The method of claim 12, wherein each of the plurality of plates moves from a retracted to an extended position by sliding in a track, wherein the tracks are aligned in a radial direction relative to the outer reinforcement band, and the tracks are supported by a base.

18. The method of claim 17, wherein each of the plurality of plates has a pin that engages a spiral groove in an actuation disk, the disk is aligned parallel to the tracks and rotatable relative to the base, whereby rotating the disk in one direction relative to the base radially extends the plates and rotating the disk in an opposite direction relative to the base radially retracts each of the plurality of plates.

19. The method of claim 12, wherein the jig is removed from between the inner reinforcement band and the resilient spacing element by the relative movement between the jig and the annular reinforcement structure in the axial direction, and wherein the annular reinforcement structure is engaged by a plurality of pins spaced axially and circumferentially around the annular reinforcement structure, which transfer force to the annular reinforcement structure in the axial direction.

20. The method of claim 12, wherein the jig is an annular band, and the jig has a width in the axial direction that is less than a width of the outer reinforcement band in the axial direction and less, than a width of the resilient spacing element in the axial direction.

21. The method of claim 20, wherein the resilient spacing element extends in the axial direction from a top of the outer reinforcement band to a distance below the jig, when the resilient spacing element is compressed against the face of the outer reinforcement band, and the inner reinforcement band frictionally engages the resilient spacing element below the jig, prior to removal of the jig from between the inner reinforcement band and the resilient spacing element.

22. The method of claim 12, wherein the resilient spacing element is an annular band comprising an open-cell, polymer foam.

23. The method of claim 12, wherein the resilient spacing element is comprised of a plurality of discrete shims comprising an open-cell, polymer foam.

24. The method of claim 12, wherein the inner and outer reinforcement bands are each comprised of a cord selected from the group consisting of monofilament or multi-filament yarns, and the cord is wound into a helix making at least three revolutions.

25. A method of making a reinforced matrix material, comprising the steps of:

(a) placing a resilient, porous spacing element against a face of a first reinforcement band;

(b) compressing the resilient, porous spacing element against the face of the first reinforcement band, adjacent a top edge of the first reinforcement band, with a jig;

(c) sliding a second reinforcement band in an axial direction relative to the first reinforcement band, from the top edge of the first reinforcement band towards a bottom edge of the first reinforcement band, while the resilient, porous spacing element is compressed by the jig, whereby the first and second reinforcement bands are in a concentric relationship, and the jig is positioned between the resilient, porous spacing element and the second reinforcement band;

wherein the first and second reinforcement bands are each comprised of a cord selected from the group consisting of monofilament or multi-filament yarns, and the cord is wound into a helix making at least three revolutions;

(d) removing the jig from between the first reinforcement band and the second reinforcement band, whereby the resilient, porous spacing element is retained in place between the first and second reinforcement bands; and

(e) introducing a liquid matrix material in the space between the first reinforcement band and second reinforcement band and curing the liquid matrix material;

wherein the first reinforcement band is positioned around the second reinforcement band, when the first and second reinforcement bands are concentric.

26. The method of claim 25, wherein the cords are brass-plated steel, the resilient, porous spacing element is a polyurethane foam, and the matrix material is a natural or synthetic elastomeric polymer.

27. The method of claim 25, wherein the jig is comprised of a plurality of plates, which are spaced around a circumference of the first reinforcement band, each of the plurality of plates has a curved surface corresponding to a curvature of the first reinforcement band, and the curved surfaces engage the resilient, porous spacing element when the plurality of plates is moved from a retracted position to an extended position.

28. The method of claim 25, wherein the jig is an annular band.

29. The method of claim 25, further comprising the step of embedding the first and second reinforcement bands and resilient, porous spacing element in a secondary matrix material, wherein the matrix material and the secondary matrix material have different chemical compositions.

30. The method of claim 25, further comprising the step of embedding the first and second reinforcement bands in a secondary matrix material, wherein the matrix material and the secondary matrix material have different chemical compositions.