Method and apparatus for inserting a spacer between annular reinforcement bands

Patent metadata

Field	Value
Publication number	US-9975300-B2
Application number	US-201715423666-A
Country	US
Kind code	B2
Filing date	Feb 3, 2017
Priority date	Sep 20, 2011
Publication date	May 22, 2018
Grant date	May 22, 2018

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.

First claim

What we claim is:

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

Assignees

• Petri Patrick A
• Vogt Kirkland W
• Dotson Michael Edward
• Marler Rush W
• Milliken & Co

Inventors

• Petri Patrick A
• Vogt Kirkland W
• Dotson Michael Edward
• Marler Rush W

Classifications

• B29L2023/00

  Tubular articles (B29L2024/00 takes precedence {; catheters B29L2031/7542}) · CPC title

• B29D30/2607

  Devices for transferring annular tyre components during the building-up stage, e.g. from the first stage to the second stage building drum · CPC title

• B29D2030/0038

  Handling tyre parts or semi-finished parts, excluding beads, e.g., storing, transporting, transferring (B29D2030/0044 takes precedence) · CPC title

• B32B5/245

  another layer next to it being a foam layer · CPC title

• B32B2597/00

  Tubular articles, e.g. hoses, pipes · CPC title