초록 ▼

The present invention is a composite material, a process and a product formed by the process. The composite is formed by a process that includes forming a fibrous structure comprising fibers into a preform, coating the fibers of the fibrous structure preform with elemental carbon to impregnate that

The present invention is a composite material, a process and a product formed by the process. The composite is formed by a process that includes forming a fibrous structure comprising fibers into a preform, coating the fibers of the fibrous structure preform with elemental carbon to impregnate that preform, infiltrating the preform with boron carbide to form an impregnated green body. The impregnated green body is infiltrated with liquid naphthalene or other carbon precursor, which is thereafter pyrolyzed to form a carbon char. Then, the char infiltrated green body is infiltrated with molten silicon to form a continuous matrix throughout the composite. The silicon in the continuous matrix is reacted with the carbon char to form silicon carbide.

대표청구항 ▼

The invention claimed is: 1. A composite material fabricated by a process comprising: a) forming a fibrous structure comprising carbon, polyacrylonitrile, or rayon fibers into a preform; b) impregnating the preform with elemental carbon to initially predominantly coat the fibers of the fibrous stru

The invention claimed is: 1. A composite material fabricated by a process comprising: a) forming a fibrous structure comprising carbon, polyacrylonitrile, or rayon fibers into a preform; b) impregnating the preform with elemental carbon to initially predominantly coat the fibers of the fibrous structure; c) infiltrating the preform with a ceramic slurry to predominantly impregnate the fibers of the preform to form an impregnated green body; d) infiltrating the impregnated green body with a liquid carbon precursor and pyrolyzing the liquid carbon precursor to form a carbon char; e) infiltrating the impregnated green body with molten silicon to form a continuous matrix throughout the composite; and f) reacting silicon in the continuous matrix with the carbon char to form silicon carbide, wherein said silicon carbide has a grain size of less than about 20 microns and said composite material has less than 5 volume % residual silicon. 2. The composite of claim 1, wherein the ceramic slurry is a boron carbide slurry. 3. The composite of claim 1, wherein said fibers of said preform are made from polyacrylonitrile. 4. The composite of claim 1, wherein said liquid carbon precursor is liquid naphthalene. 5. The composite of claim 1, wherein said molten silicon is a non alloyed silicon. 6. The composite of claim 1, wherein said molten silicon is an alloyed silicon. 7. The composite of claim 1, wherein said fibrous structure is initially coated with chemically vapor deposited elemental carbon. 8. The composite of claim 1, wherein said elemental carbon is deposited on the fibers using pitch or resin. 9. The composite of claim 1, wherein said infiltration with molten silicon occurs in the temperature range of about 1425 to about 1485�� C. 10. The composite of claim 2, wherein said boron carbide slurry comprises boron carbide having a particle size of less than about 1 micron. 11. A composite ceramic material comprising: a.) a fibrous structure comprising fibers of carbon, polyacrylonitrile, or rayon, and a silicon matrix; wherein said fibers are impregnated with elemental carbon to initially predominantly coat the fibers of the fibrous structure, and wherein said fibrous structure is subsequently predominantly impregnated with boron carbide; and b.) a silicon carbide phase comprising silicon carbide and residual silicon, wherein said silicon carbide phase is continuous and predominantly encompasses said fibrous structure, wherein silicon carbide in said silicon carbide phase has a grain size of less than about 10 microns, and wherein said composite ceramic material has less than 5 volume % residual silicon. 12. A composite ceramic material according to claim 11, wherein the amount of residual silicon in the matrix is less than that required to form a liquid phase on the wear face of a disk made from the composite material during a severe energy event. 13. A composite ceramic material according to claim 11, wherein said boron carbide comprises about 5 to about 15 volume % of said material. 14. A composite ceramic material according to claim 11, wherein said fibrous structure impregnated with elemental carbon comprises from about 20 to about 45 volume % of said material. 15. A composite ceramic material according to claim 11, wherein said silicon carbide phase comprises from about 20 to about 40 volume % of said material. 16. A composite ceramic material according to claim 11, wherein said boron carbide has an average particle size of less than about 1 micron. 17. A composite ceramic material according to claim 11, wherein said fibrous structure comprises from about 15 to about 40 volume % of said material. 18. A composite ceramic material comprising: a.) a fibrous structure and a silicon matrix which are initially predominantly impregnated with elemental carbon, and subsequently predominantly impregnated with boron carbide; and b.) a silicon carbide phase comprising silicon carbide and residual silicon wherein said silicon carbide phase is continuous and predominantly encompasses said fibrous structure, wherein silicon carbide in said silicon carbide phase has a grain size of less than about 10 microns, whenever said fibrous structure comprises fibers of carbon, polyacrylonitrile, or rayon or combinations thereof, wherein said fibers are coated with elemental carbon, and said composite ceramic material has less than 5 volume % residual silicon.