US4722825A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of fabricating a metal/ceramic composite structure
Assignee: United States Department of the Navy
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Filing: 1987-07-01
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Granted: 1988-02-02
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Expires: 2007-07-01
Abstract
Abstract A method of producing a metal/ceramic composite structure in which an uncolidated metal or metal alloy powder is loaded into a sealable glass mold comprising a hollow ceramic sleeve and a sealable outer glass envelope surrounding the ceramic sleeve and forming with the outer wall of the ceramic sleeve a sealable chamber for the metal or metal alloy powder, wherein the glass is a type which becomes plastic when heated. The air in the mold is removed under vacuum and the mold is sealed and placed into a free flowing refractory powder in a crucible and consolidated by sintering under atmospheric pressure (CAP® process). Removal of the glass envelope leaves a composite article having a consolidated metal or metal alloy layer surrounding and placing a hollow ceramic liner (sleeve) under both radial and axial compression. A ceramic-line metal gun barrel insert can be produced by using a ceramic sleeve with rifling on its inner surface.
Inventors
- 👤 David Goldstein
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 11:31
CPC Classifications
C; C04; C04B; C04B37/00; C04B37/02; C04B37/021; B; B22; B22F; B22F3/00; B22F3/12; B22F3/1208; B22F3/1216; B22F3/1225; B22F3/14; B22F3/15; C04B35/00; C04B35/622; C04B35/64; C04B35/645; C04B35/6455; F; F41; F41A; F41A21/00; F41A21/02; C04B2235/00; C04B2235/65; C04B2235/658; C04B2235/6581; C04B2237/00; C04B2237/30; C04B2237/32; C04B2237/34; C04B2237/343; C04B2237/36; C04B2237/365; C04B2237/368; C04B2237/40; C04B2237/403; C04B2237/405; C04B2237/406; C04B2237/50; C04B2237/66; C04B2237/76; C04B2237/765; C04B2237/84
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
247 words
A method of producing a metal/ceramic composite structure comprising: (a) loading unconsolidated metal or metal alloy powder into a sealable glass mold comprising a hollow ceramic sleeve and a sealable outer glass envelope surrounding the ceramic sleeve and forming with the outer wall of the ceramic sleeve a sealable chamber for the metal or metal alloy powder, wherein the glass is of a type that becomes plastic when heated; (b) evacuating the atmosphere from the metal or metal alloy powder filled chamber in the mold; (c) sealing the chamber; (d) placing the mold in an open top refractory container and packing with free flowing refractory powder selected to freely flow at all the temperatures in the process; (e) heating the mold and the metal or metal alloy contents of the mold at a temperature at which sintering of the metal or metal alloy powder takes place and holding at this temperature for a time sufficient to cause substantially complete densification of the powered metal or metal alloy, during which step the mold is supported by the free flowing refractory powder as the glass sleeve and the glass envelope become plastic and the mold shrinks in volume as its metal or metal contents densify and are compressed against the hollow ceramic sleeve; (f) cooling and removing the glass portion of the mold to leave a composite article comprising the consolidated metal or metal alloy layer surrounding and placing the hollow ceramic sleeve under both axial and radial compression.
Claim 2
Independent Claim
247 words
A method of producing a metal/ceramic composite structure comprising: (a) loading unconsolidated metal or metal alloy powder into a sealable glass mold comprising a hollow ceramic sleeve and a sealable outer glass envelope surrounding the ceramic sleeve and forming with the outer wall of the ceramic sleeve a sealable chamber for the metal or metal alloy powder, wherein the glass is of a type that becomes plastic when heated; (b) evacuating the atmosphere from the metal or metal alloy powder filled chamber in the mold; (c) sealing the chamber; (d) placing the mold in an open top refractory container and packing with free flowing refractory powder selected to freely flow at all the temperatures in the process; (e) heating the mold and the metal or metal alloy contents of the mold at a temperature at which sintering of the metal or metal alloy powder takes place and holding at this temperature for a time sufficient to cause substantially complete densification of the powered metal or metal alloy, during which step the mold is supported by the free flowing refractory powder as the glass sleeve and the glass envelope become plastic and the mold shrinks in volume as its metal or metal contents densify and are compressed against the hollow ceramic sleeve; (f) cooling and removing the glass portion of the mold to leave a composite article comprising the consolidated metal or metal alloy layer surrounding and placing the hollow ceramic sleeve under both axial and radial compression.
Claim 3
Dependent Claim
61 words
The method of claim 1 which further comprises after step (e) but before step (f), transferring the open top refractory container, refractory powder, and mold directly into an insulated, refractory lined covered container and then placing the covered container into a pressure chamber and applying an isostatic pressure of 2,000 psi or more to the mold while it slowly cools down.
Claim 4
Dependent Claim
13 words
The method of claim 1 wherein the glass used is a borosilicate glass.
Claim 5
Dependent Claim
50 words
The method of claim 1 wherein an unconsolidated metal alloy powder comprising from 38 to 47 weight percent of titanium, from zero to 6 weight percent of an additive metal selected from the group consisting of cobalt, iron, and mixtures thereof, with the remainder of the alloy being essentially nickel.
Claim 6
Dependent Claim
17 words
The method of claim 4 wherein the alloy comprises from 42 to 46 weight percent of titanium.
Claim 7
Dependent Claim
17 words
The method of claim 4 wherein the weight percent of additive metal in the alloy is zero.
Claim 8
Dependent Claim
32 words
The method of claim 1 which is used to produce a composite article which is a gun barrel insert by using a hollow ceramic sleeve which has rifling on its inner surface.
Claim 9
Dependent Claim
29 words
The method of claim 1 wherein the ceramic sleeve is made of a ceramic material selected from the group consisting of alumina, silicon carbide, silicon nitride, and titanium carbide.
Claim 10
Dependent Claim
14 words
The method of claim 8 wherein the ceramic sleeve is made of titanium carbide.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-02-01 | 1991-08-03 | 1992-02-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-02-01 | 1995-08-03 | 1996-02-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-02-01 | 1999-08-03 | 2000-02-02 | $7700.00 | Window Closed / Lapsed |