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US5480449A Expired / Lapsed US ⏱️ 0.0 years remaining

Composite prosthesis and method of manufacture

Assignee: Johnson and Johnson Professional Inc
•
Filing: 1993-01-28
•
Granted: 1996-01-02
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Expires: 2013-01-28
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Abstract

Abstract A process for making a composite stem for a prosthesis by providing a tapered metal core with a predetermined cross section and a composite shell having a tapered cavity having a cross sectional configuration to receive the metal core. Adhesive is applied to the metal core and the core is placed in the cavity and pressure is applied along the axis of the metal core toward the smaller end of the core to force the core against the composite shell and heat is applied with the pressure to bond the composite shell to the metal core.

Inventors

  • 👤 John V. Hamilton
  • 👤 Salvatore Caldarise
  • 👤 Debra J. Treacy

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 21:24
CPC Classifications
B; B29; B29C; B29C70/00; B29C70/68; B29C70/86; A; A61; A61F; A61F2/00; A61F2/02; A61F2/30; A61F2/30767; A61F2/30907; A61F2/3094; A61F2/30965; A61L; A61L27/00; A61L27/40; A61L27/44; A61L27/443; B29C35/00; B29C35/02; B29C35/0272; A61F2/32; A61F2/36; A61F2/3662; A61F2002/30001; A61F2002/30003; A61F2002/30004; A61F2002/30009; A61F2002/30014; A61F2002/3006; A61F2002/30065; A61F2002/30316; A61F2002/30329; A61F2002/30331; A61F2002/30354; A61F2002/30357; A61F2/3609; A61F2002/3625; A61F2002/3631; A61F2002/365; A61F2002/3652; A61F2210/00; A61F2210/0071; A61F2220/00; A61F2220/0025; A61F2220/0033; A61F2250/00; A61F2250/0014; A61F2250/0018; A61F2250/0028; A61F2310/00; A61F2310/00005; A61F2310/00011; A61F2310/00023; A61F2310/00029; B29C2035/0211; B29L; B29L2031/00; B29L2031/753; B29L2031/7532; Y; Y10; Y10S; Y10S623/00; Y10S623/909; Y10S623/911; Y10T; Y10T29/00; Y10T29/49; Y10T29/49826; Y10T29/49895; Y10T29/49897

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 209 words
A process of making a prosthesis stem having a metal core and composite fiber shell surrounding said core, comprising providing a tapered metal core having a predetermined cross sectional configuration and a composite shell having a tapered cavity having the same cross sectional configuration as said tapered metal core, said tapered cavity having a length extending from a first end to a second end of said shell, the cross sectional area of said second end being smaller than the cross sectional area of said first end, applying an adhesive to said tapered metal core, placing the tapered metal core into the cavity in the composite shell, said core having a length greater than the length of the cavity in said composite shell so that a portion of the core extends beyond the first and the second end of the composite shell, placing the composite shell in an insulated fixture having a length less than the length of said core, heating the metal core and the interior of the shell, applying pressure to the core in a direction from the first end to the second end along the length of the core to force the core against the adhesive within the composite shell thereby bonding the core to said shell.
Claim 2
Dependent Claim 209 words
A process of making a prosthesis stem having a metal core and composite fiber shell surrounding said core, comprising providing a tapered metal core having a predetermined cross sectional configuration and a composite shell having a tapered cavity having the same cross sectional configuration as said tapered metal core, said tapered cavity having a length extending from a first end to a second end of said shell, the cross sectional area of said second end being smaller than the cross sectional area of said first end, applying an adhesive to said tapered metal core, placing the tapered metal core into the cavity in the composite shell, said core having a length greater than the length of the cavity in said composite shell so that a portion of the core extends beyond the first and the second end of the composite shell, placing the composite shell in an insulated fixture having a length less than the length of said core, heating the metal core and the interior of the shell, applying pressure to the core in a direction from the first end to the second end along the length of the core to force the core against the adhesive within the composite shell thereby bonding the core to said shell.
Claim 3
Dependent Claim 19 words
The process of claim 1 in which the metal core is heated by directing electric current through the core.
Claim 4
Dependent Claim 31 words
The process of claim 1 in which a seal is affixed to the end of the core adjacent the second end of the cavity before pressure is applied to the core.
Claim 5
Dependent Claim 20 words
The process of claim 1 in which the composite shell comprises a high strength fiber bonded with a thermoplastic resin.
Claim 6
Dependent Claim 25 words
The process of claim 1 in which the metal core is a Ti-6A1-4b alloy and the composite shell comprises carbon fibers and a polyetheretherketone resin.

References Cited (Backward Citations)

US4892552A Cited
US4662887A Cited
US4750905A Cited
US4902297A Cited
US5018285A Cited
US4978358A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1999-01-01 1999-07-03 2000-01-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2003-01-01 2003-07-03 2004-01-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2007-01-01 2007-07-03 2008-01-02 $7700.00 Window Closed / Lapsed

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