Process for preparing advanced composite structures

• US 5,198,173 A
• Filed: 12/13/1990
• Issued: 03/30/1993
• Est. Priority Date: 12/13/1990
• Status: Expired due to Term

• Current Assignee: DePuy Orthopaedics Incorporated (Johnson & Johnson)
• Original Assignee: E. I. du Pont de Nemours and Company (Corteva, Inc.)
• Inventors: Terzian, ALbert, Trentacosta, Joseph D.
• Primary Examiner(s): HEITBRINK, TIMOTHY W
• Application Number:
  US07/626,886
• Time in Patent Office: 838 Days
• Field of Search: 264/255, 264/261, 264/257, 264/258, 264/510
• US Class Current: 264/257
• CPC Class Codes: A61F 2/3094 Designing or manufacturing processes
• CPC Class Codes: A61F 2/30965 Reinforcing the prosthesis by embedding particles or fibres during moulding or dipping
• CPC Class Codes: A61F 2/32 for the hip
• CPC Class Codes: A61F 2/34 Acetabular cups
• CPC Class Codes: A61F 2/3609 Femoral heads or necks; Connections of endoprosthetic heads or necks to endoprosthetic femoral shafts A61F2/3601 takes precedence
• CPC Class Codes: A61F 2/3672 Intermediate parts of shafts
• CPC Class Codes: A61L 27/44 having a macromolecular matrix
• CPC Class Codes: B29C 43/12 using bags surrounding the moulding material or using membranes contacting the moulding material
• CPC Class Codes: B29C 45/14 incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles B29C45/1671 takes precedence
• CPC Class Codes: B29C 55/24 radial
• CPC Class Codes: B29C 70/446 Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
• CPC Class Codes: B29C 70/745 Filling cavities in the preformed part for joining B29C70/84
• CPC Class Codes: B29L 2031/7532 Artificial members, protheses

Abstract

A novel procedure for molding composite structures is disclosed wherein the finished part exhibits a net shape geometry requiring minimal further machining and displaying enhanced consolidation and surface characteristics. A composite preform having a hollow core portion containing a polymer insert is introduced into a mold cavity. One end of the preform core is sealed and the preform together with the polymer insert is heated to melt the composite matrix and core polymer. Pressure is applied to the core at the other end of the part, causing radial expansion of the part against the molded cavity and consolidation of the composite into a finished part. A product finished part is also disclosed and is useful as a component of an orthopedic implant.

Claims

1. A method of making a composite structure comprising:

providing a preform for disposition within a mold cavity, said preform having a hollow core portion and further having an external configuration which is undersized relative to the cavity of the mold;

introducing said preform into said cavity having an internal configuration appropriate to the configuration of a finished part;

plugging one or more openings to the core of said preform with one or more plugs to prevent polymer flow from these openings;

introducing polymer into the core of the preform;

heating the preform together with the polymer in the core so as to melt the polymer in the preform in the core;

applying pressure to the polymer in the core of the preform via one or more remaining unplugged openings to the core of the preform to cause expansion of the preform against the internal configuration of the mold cavity and to consolidate the preform to form a finished part;

cooling the finished part while maintaining pressure on the core; and

removing the finished part from the mold.

2. The method of claim 1 further comprising heating the part and applying pressure to the core for a period sufficient to substantially eliminate the presence of voids in the finished part.

3. The method of claim 1 wherein the mold includes a polymer reservoir sized to contain polymer in excess of that within the core of the preform prior to pressurization and further shaped to urge polymer into the core while applying pressure to the core.

4. The method of claim 1 wherein the mold is attached to a screw injection molding machine which fills the core of the preform with polymer and also applies pressure to the core.

5. The method of claim 1 wherein the plugs are fixed to prevent polymer flow from the plugged openings.

6. The method of claim 1 wherein the plugs are moveable and have a load applied to them by of a spring or other actuator to impede polymer leakage through the plugged openings.

7. The method of claim 1 wherein one or more openings to the core are sealed to the mold by incorporation of threaded shapes into the plugs and the plugged openings.

8. The method of claim 1 wherein the plugged openings include bleed ports.

9. The method of claim 1 wherein the one or more plugs has a removable mandrel attached thereto spanning the length of the mold cavity such that the finished part has a hollow core.

10. A method of making a composite structure comprising:

providing a thermoplastic matrix, fiber reinforced preform for disposition within a mold cavity, said preform having a hollow core portion and further having an external configuration which is undersized relative to the cavity of the mold;

introducing said preform into said cavity having an internal configuration appropriate to the configuration of a finished part;

plugging one or more openings to the core of said preform with one or more plugs to prevent polymer flow from these openings;

introducing polymer into the preform;

heating the preform together with the polymer in the core so as to melt the polymer the preform in the core;

applying pressure to the polymer in the core of the preform via one or more remaining, unplugged openings to the core of the preform to cause expansion of the preform against the internal configuration of the mold cavity and to consolidate the preform to form a finished part;

cooling the finished part while maintaining pressure on the core; and

removing the finished part from the mold.

11. The method of claim 10 wherein the fibers are selected from the group consisting of carbon, glass and aramid fiber.

12. The method of claim 10 wherein the thermoplastic matrix is selected from the group consisting of polyamide, polyester, polysulfone, polyether-ether-ketone, polyether-ketone-ketone, polyimide, copolymers of tetrafluoroethylene and perfluorovinylether and copolymers of polytetrafluoroethylene and ethylene.

13. The method of claim 10 wherein the polymer introduced into the core is selected from the group consisting of polyamide, polyester, polysulfone, polyether-ether-ketone, polyether-ketone-ketone, polyimide, copolymers of tetrafluoroethylene and perfluorovinylether and copolymers of polytetrafluoroethylene and ethylene.

14. The method of claim 10 wherein the preform is made by filament winding.

15. The method of claim 10 wherein the preform is made by braiding.

16. The method of claim 10 wherein the preform is made by fiber placement machines incorporating a robot,