US4737382A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Carbide coatings for fabrication of carbon-fiber-reinforced metal matrix composites
Assignee: Aerospace Corp
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Filing: 1986-09-29
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Granted: 1988-04-12
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Expires: 2006-09-29
Abstract
Abstract A carbon fiber reinforced metal matrix composite is produced by carbide coating the surface of the fibers by passing the fibers through an organometallic solution followed by pyrolysis of the organometallic compounds. The carbide coated fibers, so produced are readily wettable without degradation when immersed in a molten bath of metal matrix material containing an active alloying element.
Inventors
- 👤 Howard A. Katzman
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 14:45
CPC Classifications
D; D01; D01F; D01F11/00; D01F11/10; D01F11/12; D01F11/126; C; C22; C22C; C22C49/00; C22C49/14
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
98 words
A process for fabricating a carbon fiber reinforced metal matrix composite comprising: a. depositing a silicon carbide coating on the surfaces of the carbon fibers; b. immersing the silicon carbide coated fibers in a molten bath of a metal matrix material comprising an alloy consisting of a major portion of a metal non-reactive with the silicon carbide and a minor portion of a metal reactive with the silicon carbide coating; and, c. removing the fibers from the bath and solidifying the metal alloy adhered to fibers whereby to form metal matrix adhered chemically and mechanically to the fibers.
Claim 2
Dependent Claim
98 words
A process for fabricating a carbon fiber reinforced metal matrix composite comprising: a. depositing a silicon carbide coating on the surfaces of the carbon fibers; b. immersing the silicon carbide coated fibers in a molten bath of a metal matrix material comprising an alloy consisting of a major portion of a metal non-reactive with the silicon carbide and a minor portion of a metal reactive with the silicon carbide coating; and, c. removing the fibers from the bath and solidifying the metal alloy adhered to fibers whereby to form metal matrix adhered chemically and mechanically to the fibers.
Claim 3
Dependent Claim
24 words
The process as defined in claim 1 wherein the non-reactive metal in the alloy is selected from the group comprising copper, magnesium and aluminum.
Claim 4
Dependent Claim
16 words
The process as defined in claim 1 wherein the non-reactive metal in the alloy is copper.
Claim 5
Dependent Claim
28 words
The process as defined in claim 1 wherein the reactive metal in the alloy is selected from the group comprising titanium, iron, cobalt, nickel, zirconium, niobium and lanthanum.
Claim 6
Dependent Claim
16 words
The process as defined in claim 1 wherein the reactive metal in the alloy is titanium.
Claim 7
Dependent Claim
25 words
The process as defined in claim 1 wherein the non-reactive metal in the alloy is copper and the reactive metal in the allow is titanium.
Claim 8
Dependent Claim
59 words
The process as defined in claim 1 wherein the surfaces of the carbon fiber are coated with silicon carbide by: a. immersing the carbon fiber in an organosilicon polymeric precursor solution to thereby provide a coating of the solution on the surfaces of the fiber; and, b. pyrolyzing the coating of the solution into a coating of silicon carbide.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-04-12 | 1991-10-12 | 1992-04-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-04-12 | 1995-10-12 | 1996-04-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-04-12 | 1999-10-12 | 2000-04-12 | $7700.00 | Window Closed / Lapsed |