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US4223075A Expired / Lapsed US ⏱️ 0.0 years remaining

Graphite fiber, metal matrix composite

Assignee: Aerospace Corp
•
Filing: 1977-01-21
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Granted: 1980-09-16
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Expires: 1997-01-21
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Abstract

Abstract Metals constituting the matrix of carbon (graphite) filament reinforced composites are alloyed with titanium and boron to prevent or reduce the migration of the titanium-boron coating applied to the filaments prior to their impregnation with the metal matrix materials.

Inventors

  • 👤 William C. Harrigan, Jr.
  • 👤 Robert H. Flowers
  • 👤 Silas P. Hudson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 03:18
CPC Classifications
C; C22; C22C; C22C47/00; C22C47/02; C22C47/04; C22C49/00; C22C49/14; Y; Y10; Y10T; Y10T428/00; Y10T428/12; Y10T428/12458; Y10T428/12486; Y10T428/12493; Y10T428/12535; Y10T428/12576; Y10T428/12625

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 101 words
A graphite filament reinforced metal matrix composite comprising: (a) at least one multi-strand graphite filament having an initial coating of titanium-boron on the surfaces thereof; and, (b) a solid metal matrix having the graphite filament embedded therein and adhered thereto, the metal of said matrix being selected from the group consisting of aluminum, copper, tin lead, silver, zinc, magnesium, and alloys thereof, said metal containing alloying elements of titanium and boron in amounts effective to minimize the net absorption of the initial titanium-boron coating by the metal matrix when said matrix is heated to a temperature approaching the liquidus, or higher.
Claim 2
Dependent Claim 101 words
A graphite filament reinforced metal matrix composite comprising: (a) at least one multi-strand graphite filament having an initial coating of titanium-boron on the surfaces thereof; and, (b) a solid metal matrix having the graphite filament embedded therein and adhered thereto, the metal of said matrix being selected from the group consisting of aluminum, copper, tin lead, silver, zinc, magnesium, and alloys thereof, said metal containing alloying elements of titanium and boron in amounts effective to minimize the net absorption of the initial titanium-boron coating by the metal matrix when said matrix is heated to a temperature approaching the liquidus, or higher.
Claim 3
Dependent Claim 36 words
A composite as defined in claim 1, wherein said metal comprises aluminum, or an alloy thereof, and the titanium and boron therein are in the approximate proportions of up to 0.25 and 0.025 weight percent, respectively.
Claim 4
Dependent Claim 36 words
A composite as defined in claim 1, wherein said metal comprises tin, or an alloy thereof, and the titanium and boron therein are in the approximate proportions of up to 0.25 and 0.025 weight percent, respectively.
Claim 5
Dependent Claim 32 words
A composite as defined in claim 1, wherein said metal comprises copper, and the titanium and boron therein, are in the approximate proportions of up to 1.0 and .05 weight percent, respectively.

References Cited (Backward Citations)

US3484270A Cited
US3622283A Cited
US3885959A Cited
US3837819A Cited
US3720257A Cited
US3828417A Cited
US3840350A Cited
US3888661A Cited
US3860443A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-09-16 1984-03-17 1984-09-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-09-16 1988-03-17 1988-09-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-09-16 1992-03-17 1992-09-16 $7700.00 Window Closed / Lapsed

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