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Method of manufacturing a reinforced composite structure of ceramic material

Assignee: Ceraver SA
•
Filing: 1984-11-28
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Granted: 1986-04-29
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Expires: 2004-11-28
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Abstract

Abstract An improved method of manufacturing a composite structure of ceramic material reinforced by refractory fibers is disclosed, whereby the fibers are first embedded in a slip of the ceramic material containing a synthetic resin with good ceramic and fiber wetting properties and a solvent of said resin, the liquid phase is thereafter eliminated from the slip by drying, the synthetic resin is driven from the formed structure by heating, and the fiber-reinforced ceramic material is sintered. The improvement consists in avoiding the use of costly aluminum-nitride powder by initially incorporating an aluminum powder in the slip along with the resin solvent and nitriding the powder in the structure, after drying and firing, but before sintering.

Inventors

  • 👤 Louis Minjolle
  • 👤 Claudette Drouet
  • 👤 Bernard Lengronne
  • 👤 Alain Hordonneau
  • 👤 Bernard Capdepuy

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 21:28
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/71; C04B35/78; C04B35/80; C04B35/515; C04B35/58; C04B35/581

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 128 words
A method for manufacturing an aluminum nitride matrix composite structure not requiring the input of said nitride, said structure being of a ceramic material reinforced with refractory fibers, comprising preparing a slurry containing aluminum powder, a synthetic resin and an organic for said resin; introducing refractory fibers selected from the group consisting of alumina, silicon carbide, short mullite, pure silica, silicon nitride and boron nitride fibers and whiskers into said slurry; removing the liquid phase from said slurry by drying to form a structure; firing the formed structure to remove the synthetic resin; then subjecting the structure to nitriding of the aluminum powder to form aluminum nitride and sintering the nitrided structure without particular gas pressure and under temperature conditions such that the refractory fibers are not damaged.
Claim 2
Independent Claim 128 words
A method for manufacturing an aluminum nitride matrix composite structure not requiring the input of said nitride, said structure being of a ceramic material reinforced with refractory fibers, comprising preparing a slurry containing aluminum powder, a synthetic resin and an organic for said resin; introducing refractory fibers selected from the group consisting of alumina, silicon carbide, short mullite, pure silica, silicon nitride and boron nitride fibers and whiskers into said slurry; removing the liquid phase from said slurry by drying to form a structure; firing the formed structure to remove the synthetic resin; then subjecting the structure to nitriding of the aluminum powder to form aluminum nitride and sintering the nitrided structure without particular gas pressure and under temperature conditions such that the refractory fibers are not damaged.
Claim 3
Dependent Claim 38 words
Method according to claim 1, wherein firing is carried out in a vacuum with temperature being raised from ambient to 400° C. in at least 40 hours, whilst keeping weight losses to a maximum of 0.5% per hour.
Claim 4
Dependent Claim 22 words
Method according to claim 2 or 1, wherein said nitriding is carried out at a temperature of approximately 700° to 800° C.
Claim 5
Dependent Claim 56 words
Method according to claim 3, wherein said nitriding is carried out by injecting nitrogen gas and raising the temperature from ambient temperature to 400° C. at a rate of 100° C./hour, then from 400° C. to 700° C. at a rate of 5° C./hour, then keeping the temperature at 700° C. for at least three hours.

References Cited (Backward Citations)

US2839413A Cited
US2929126A Cited
GB1001867A Cited
US3238018A Cited
GB1335842A Cited
US3899554A Cited
US4265794A Cited
US4233077A Cited
EP0032097A1 Cited
EP0128409A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-04-28 1989-10-28 1990-04-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-04-28 1993-10-28 1994-04-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-04-28 1997-10-28 1998-04-29 $7700.00 Window Closed / Lapsed

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