Non-linear fiber/matrix architecture

• US 20050116400A1
• Filed: 10/29/2004
• Published: 06/02/2005
• Est. Priority Date: 11/14/2003
• Status: Abandoned Application

• Current Assignee: SPARTA, Inc. (New Port Group Holdings, Inc.)
• Original Assignee: SPARTA, Inc. (New Port Group Holdings, Inc.)
• Inventors: White, Moreno J.
• Application Number:
  US10/976,556
• Publication Number:
  US 20050116400A1
• Time in Patent Office: Days
• US Class Current: 267/158
• CPC Class Codes: A61F 2/3094 Designing or manufacturing processes
• CPC Class Codes: A61F 2/442 Intervertebral or spinal discs, e.g. resilient non-disc-shaped intervertebral inflatable pockets A61F2/441; non-disc-shaped intervertebral fusion implants A61F2/4455
• CPC Class Codes: A61F 2/6607 Ankle joints
• CPC Class Codes: A61F 2002/30009 differing in fibre orientations
• CPC Class Codes: A61F 2002/30014 differing in elasticity, stiffness or compressibility
• CPC Class Codes: A61F 2002/30563 having elastic means or damping means, different from springs, e.g. including an elastomeric core or shock absorbers
• CPC Class Codes: A61F 2002/3092 having an open-celled or open-pored structure
• CPC Class Codes: A61F 2002/4495 having a fabric structure, e.g. made from wires or fibres
• CPC Class Codes: A61F 2250/0018 differing in elasticity, stiffness or compressibility
• CPC Class Codes: A61F 2250/0028 differing in fibre orientations
• CPC Class Codes: F16F 1/366 made of fibre-reinforced plastics, i.e. characterised by their special construction from such materials

Abstract

Provided is a composite spring assembly configured to provide non-linear stiffness in response to a load. The spring assembly comprises a body portion and a reinforcing element. The body portion defines a longitudinal axis along which the load may be placed. The reinforcing element is embedded in the body portion and is oriented in general disalignment with the longitudinal axis such that deformation of the body portion under the load causes the reinforcing element to move toward alignment with the load direction. The spring assembly may be provided as a prosthetic spine disc wherein the body portion is cylindrically shaped and has an outer wall and planar opposed body end faces. The reinforcing elements are cylindrically shaped and coaxially disposed relative to one another and to the outer wall. The spring assembly may be configured as an elongate tension band with the reinforcing element being configured as a continuous loop of material arranged in a double bowtie configuration.

Claims

1. A composite spring assembly configured to provide non-linear stiffness in response to a load, the composite spring assembly comprising:

a body portion defining a longitudinal axis;

at least one reinforcing element embedded in the body portion and oriented in general disalignment with the longitudinal axis such that deformation of the body portion under the load causes the reinforcing element to move toward alignment with the load direction.

2. The composite spring assembly of claim 1 wherein the body portion is formed of a polymer resin matrix material.

3. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of a fiber bundle.

4. The composite spring assembly of claim 1 wherein the fiber bundle is comprised of a plurality of synthetic continuous filaments disposed in parallel relationship to one another.

5. The composite spring assembly of claim 4 wherein the fiber bundle includes from about 1000 to about 125000 filaments.

6. The composite spring assembly of claim 4 wherein the filaments are held in position by cross stitches.

7. The composite spring assembly of claim 1 wherein the reinforcing element is provided as fabric.

8. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of glass.

9. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of quartz.

10. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of carbon.

11. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of graphite.

12. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of metallic material.

13. The composite spring assembly of claim 1 wherein the reinforcing element is comprised of organic material.

14. The composite spring assembly of claim 1 wherein:

the body portion is generally cylindrically shaped and having an outer wall defining a diameter, the body portion having substantially planar opposed body end faces;

a pair of the reinforcing elements being embedded within the body portion and being generally cylindrically shaped and coaxially disposed relative to one another and to the outer wall.

15. The composite spring assembly of claim 14 wherein each one of the cylindrically shaped reinforcing elements is formed of a plurality of non-parallel tows arranged such that the tows intersect one another.

16. The composite spring assembly of claim 14 wherein the body portion includes a core element generally concentrically disposed therewithin.

17. The composite spring assembly of claim 14 further comprising:

a disc-shaped interface plate attached to each one of the end faces, each of the interface plates having a diameter approximately equal to that of the cylindrical outer wall.

18. The composite spring assembly of claim 17 wherein the interface plates are fabricated of a biocompatible matrix material.

19. The composite spring assembly of claim 18 wherein the biocompatible matrix material is carbon/polyetheretherketone.

20. The composite spring assembly of claim 1 wherein:

the body portion is configured as an elongate tension band defining a length having a midpoint and having opposing ends with the longitudinal axis extending therebetween;

the reinforcing element being configured as a continuous loop of material disposed along the length and arranged in a double bowtie configuration wherein the reinforcing element extends about each one of the ends and tapering inwardly toward the longitudinal axis along a direction from the ends toward the midpoint, and tapering back outwardly away from the longitudinal axis and joining the reinforcing element extending from the opposing one of the ends at the midpoint such that substantially no portion of the reinforcing element is aligned with the longitudinal axis.

21. The composite spring assembly of claim 17 wherein the reinforcing material is generally symmetrical about the longitudinal axis and about the midpoint.

22. The composite spring assembly of claim 17 wherein each one of the opposing ends has a bore formed therethrough, the continuous loop extending about each one of the bores.