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Process of producing titanium composite having a coil-shaped skeletal structure on the surface thereof

Assignee: De Nora Permelec Ltd
•
Filing: 1986-11-28
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Granted: 1989-12-26
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Expires: 2006-11-28
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Abstract

Abstract A titanium composite having a coil-shaped skeletal structure on the surface, comprising a titanium or titanium alloy substrate and one or more layers of a coil-shaped skeletal titanium or titanium alloy structure that is firmly attached to the surface of said substrate and a process for producing a titanium composite having a coil-shaped skeletal structure on a surface of a titanium or titanium alloy substrate, which comprises: providing a coating composition which is a mixture of a titanium or titanium alloy powder with a binder; applying said composition in such a manner that titanium or titanium alloy coils which are to form the coil-shaped skeletal structure are firmly attached to both themselves and to the titanium or titanium alloy substrate; the heating the assembly either in vacuo or in an inert atmosphere so that the titanium or titanium alloy powder in the applied coating composition is sintered to have the coil-shaped skeletal titanium or titanium alloy structure attached firmly onto the titanium or titanium alloy substrate.

Inventors

  • 👤 Takayuki Shimamune
  • 👤 Masashi Hosonuma

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 22:40
CPC Classifications
B; B22; B22F; B22F7/00; B22F7/002; A; A61; A61F; A61F2/00; A61F2/02; A61F2/28; A61F2/30; A61F2/30767; A61F2/30907; A61L; A61L27/00; A61L27/02; A61L27/04; A61L27/06; C; C22; C22C; C22C14/00; C25; C25D; C25D17/00; C25D17/10; C25D17/12; A61F2002/30001; A61F2002/30108; A61F2002/30199; A61F2002/30289; A61F2002/30316; A61F2002/30329; A61F2002/30451; A61F2002/30929; A61F2/3094; A61F2002/30968; A61F2220/00; A61F2220/0025; A61F2220/0058; A61F2230/00; A61F2230/0063; A61F2230/0091; A61F2310/00; A61F2310/00005; A61F2310/00011; A61F2310/00023; A61F2310/00035; A61F2310/00047; A61F2310/00053; A61F2310/00095; A61F2310/00131; A61F2310/00149; A61F2310/00389; A61F2310/00395; A61F2310/00407

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 141 words
A process for producing a titanium composite having a coil-shaped skeletal structure on a surface of a titanium or titanium alloy substrate, which comprises: providing a coating composition which is a mixture of a titanium or titanium alloy powder with a binder; providing titanium or titanium alloy coils on the surface of a titanium or titanium alloy substrate; applying said coating composition in such a manner that said titanium or titanium alloy coils which are to form the coil-shaped skeletal structure are securely attached to both themselves and to the titanium or titanium alloy substrate; then heating the assembly either in vacuo or in an inert atmosphere so that the titanium or titanium alloy powder in the applied coating composition is sintered to have the coil-shaped skeletal titanium or titanium alloy structure attached firmly onto the titanium or titanium alloy substrate.
Claim 2
Dependent Claim 141 words
A process for producing a titanium composite having a coil-shaped skeletal structure on a surface of a titanium or titanium alloy substrate, which comprises: providing a coating composition which is a mixture of a titanium or titanium alloy powder with a binder; providing titanium or titanium alloy coils on the surface of a titanium or titanium alloy substrate; applying said coating composition in such a manner that said titanium or titanium alloy coils which are to form the coil-shaped skeletal structure are securely attached to both themselves and to the titanium or titanium alloy substrate; then heating the assembly either in vacuo or in an inert atmosphere so that the titanium or titanium alloy powder in the applied coating composition is sintered to have the coil-shaped skeletal titanium or titanium alloy structure attached firmly onto the titanium or titanium alloy substrate.
Claim 3
Dependent Claim 23 words
A process as in claim 1, wherein the heating of the assembly is achieved at a temperature of between 900° and 1,400° C.
Claim 4
Dependent Claim 18 words
A process as in claim 1, wherein the titanium or titanium alloy substrate is grooved in the surface.

References Cited (Backward Citations)

GB1059267A Cited
US3609842A Cited
SU581936A1 Cited
US4038703A Cited
US4122015A Cited
US4644942A Cited
US4495664A Cited
GB2142544A Cited
DE3508234A1 Cited
JPH05224938A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-12-25 1993-06-26 1993-12-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-12-25 1997-06-26 1997-12-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-12-25 2001-06-26 2001-12-26 $7700.00 Window Closed / Lapsed

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