Method for attaching a porous metal layer to a metal substrate

• US 7,918,382 B2
• Filed: 04/18/2005
• Issued: 04/05/2011
• Est. Priority Date: 06/18/2002
• Status: Active Grant

• Current Assignee: Zimmer Incorporated (Zimmer Biomet Holdings, Inc.)
• Original Assignee: Zimmer Technology Incorporated (Zimmer Biomet Holdings, Inc.)
• Inventors: Charlebois, Steven J., Zawadzki, Steven A., Gilbertson, Leslie N., Medlin, Dana J., Shetty, H. Ravindranath, Hawkins, Michael E.
• Primary Examiner(s): King; Roy
• Assistant Examiner(s): Aboagye; Michael
• Application Number:
  US11/109,166
• Publication Number:
  US 20050184134A1
• Time in Patent Office: 2,178 Days
• Field of Search: 228/248.1, 228/193, 228/253, 228/254, 228/255, 228/262.3, 228/262.71, 228/262.31, 228/262.1, 228/262, 228/245, 623/901, 623/920, 623/923, 623/53.53, 623/16.11, 623/23.36, 427/2.24, 427/2.26, 427/455, 427/456, 427/475, 427/420, 427/427, 427/123, 427/124, 427/528, 427/531
• US Class Current: 228/248.1
• CPC Class Codes: A61F 2/30767 Special external or bone-contacting surface, e.g. coating for improving bone ingrowth
• CPC Class Codes: A61F 2/30907 Nets or sleeves applied to surface of prostheses or in cement
• CPC Class Codes: A61F 2/3094 Designing or manufacturing processes
• CPC Class Codes: A61F 2/3859 Femoral components
• CPC Class Codes: A61F 2002/30787 inclined obliquely with respect to each other
• CPC Class Codes: A61F 2002/30967 Diffusion bonding
• CPC Class Codes: A61F 2002/30968 Sintering
• CPC Class Codes: A61F 2002/30978 using electrical discharge machining [EDM]
• CPC Class Codes: A61F 2002/3401 with radial apertures, e.g. radial bores for receiving fixation screws
• CPC Class Codes: A61F 2310/00023 Titanium or titanium-based alloys, e.g. Ti-Ni alloys
• CPC Class Codes: A61F 2310/00029 Cobalt-based alloys, e.g. Co-Cr alloys or Vitallium
• CPC Class Codes: A61F 2310/00407 Coating made of titanium or of Ti-based alloys
• CPC Class Codes: A61F 2310/00544 Coating made of tantalum or Ta-based alloys
• CPC Class Codes: A61L 27/04 Metals or alloys
• CPC Class Codes: A61L 27/30 Inorganic materials
• CPC Class Codes: A61L 27/56 Porous materials, e.g. foams or sponges
• CPC Class Codes: B22F 7/004 comprising at least one non-porous part
• CPC Class Codes: B22F 7/064 using an intermediate powder layer
• CPC Class Codes: B23P 23/00 Machines or arrangements of machines for performing specified combinations of different metal-working operations not covered by a single other subclass if the particular kinds of operation are not essential B23Q37/00 - B23Q41/00; working by laser beam combined with other working of metal B23K26/0093
• CPC Class Codes: C23C 26/00 Coating not provided for in groups C23C2/00 - C23C24/00
• CPC Class Codes: Y10T 29/49861 : Sizing mating parts during final positional association

Abstract

A method for attaching a porous metal layer to a dense metal substrate, wherein the method is particularly useful in forming orthopedic implants such as femoral knee components, femoral hip components, and/or acetabular cups. The method, in one embodiment thereof, comprises providing a solid metal substrate; providing a porous metal structure; contouring a surface of the porous metal structure; placing the porous structure against the substrate such that the contoured surface of the porous metal structure is disposed against the substrate, thereby forming an assembly; applying heat and pressure to the assembly in conjunction with thermal expansion of the substrate in order to metallurgically bond the porous structure and the substrate; and removing mass from the substrate after the porous structure is bonded to the substrate, thereby finish processing the assembly.

Claims

1. A method for attaching a porous metal structure to a metal substrate, the method comprising:

providing a solid metal substrate of a first mass;

providing the porous metal structure;

contouring a surface of the porous metal structure;

placing the porous structure against the substrate such that the contoured surface of the porous metal structure is disposed against the substrate, thereby forming an assembly;

applying heat and pressure to the assembly in conjunction with thermal expansion of the substrate in order to metallurgically bond the porous structure and the substrate; and

changing the shape of the substrate by removing mass from the substrate to form the substrate having a second mass after the porous structure is bonded to the substrate, thereby finish processing the assembly, the first mass being significantly greater than the second mass, whereby the substrate of the first mass exhibits greater thermal expansion when heated than would the substrate of the second mass;

wherein changing the shape of the substrate comprises forming an indentation in a surface of the substrate; and

wherein the surface of the substrate is located substantially within a plane such that the indentation in the surface of the substrate extends toward a side of the plane, the porous metal structure enveloping the substrate on the side of the plane containing the indentation.

2. The method of claim 1, wherein the metal substrate comprises a metal selected from the group consisting of cobalt, cobalt alloys, titanium and titanium alloys.

3. The method of claim 1, wherein the contouring step comprises machining the surface of the porous metal structure.

4. The method of claim 1, wherein the contouring step comprises electro-discharge machining the surface of the porous metal structure.

5. The method of claim 1, wherein the heating step comprises:

heating the assembly to about 800°

C. to 1600°

C. for about one hour to about four hours, under a clamping pressure of between about 200 p.s.i. and about 1200 p.s.i.

6. The method of claim 1, wherein the step of applying heat and pressure is in an inert environment comprising a gas selected from the group consisting of argon and helium.

7. The method of claim 1, wherein the step of applying heat and pressure is performed in an at least partial vacuum.

8. The method of claim 1, wherein changing the shape of the substrate comprises machining a surface of the substrate in a non-uniform manner.

9. A method for attaching a porous metal structure to a metal component of an orthopedic implant, the method comprising:

providing a metal component having a first three dimensional shape and a bone contacting surface;

providing the porous metal structure in a desired shape;

contouring a surface of the porous metal structure;

placing the porous structure against the bone contacting surface of the metal component such that the contoured surface of the porous structure is in contact with the metal component, thereby forming an assembly;

applying heat and pressure to the assembly in conjunction with thermal expansion of the metal component to metallurgically bond the porous structure and the metal component; and

removing mass from the metal component to form the metal component having a second three dimensional shape after the porous structure is bonded to the metal component, thereby finish processing the assembly, the first and second shapes differing in at least one dimension;

wherein removing mass from the metal component comprises forming an indentation in a surface of the metal component; and

wherein the surface of the metal component is located substantially within a plane such that the indentation in the surface of the metal component extends toward a side of the plane, the porous metal structure enveloping the metal component on the side of the plane containing the indentation.

10. The method of claim 9, wherein the first shape is a substantially solid hemisphere and the second shape is a hollow hemisphere.

11. The method of claim 9, wherein the metal component having the second shape is shaped to articulate anatomically with an adjacent orthopedic implant.

12. The method of claim 9, wherein the second shape of the metal component is a final shape of the metal component.

13. The method of claim 9, wherein the second shape of the metal component is a finished acetabular cup assembly.

14. The method of claim 9, wherein the removing mass step comprises forming an indentation in a surface of the metal component.

15. The method of claim 9, wherein the removing mass step comprises machining a surface of the metal component in a non-uniform manner.

16. A method for attaching a porous metal structure to a metal substrate, the method comprising:

providing a solid metal substrate of a first mass;

providing the porous metal structure;

placing the porous structure against the substrate, thereby forming an assembly;

applying heat and pressure to the assembly in conjunction with thermal expansion of the substrate in order to metallurgically bond the porous structure and the substrate; and

changing the shape of the substrate by removing mass from the substrate to form the substrate having a second mass after the porous structure is bonded to the substrate, thereby finish processing the assembly, the first mass being greater than the second mass, whereby the substrate of the first mass exhibits greater thermal expansion when heated than would the substrate of the second mass;

wherein changing the shape of the substrate comprises forming an indentation in a surface of the substrate; and

wherein the surface of the substrate is located substantially within a plane such that the indentation in the surface of the substrate extends toward a side of the plane, the porous metal structure enveloping the substrate on the side of the plane containing the indentation.