Claims
- 1. A refractory composite consisting essentially of aluminosilicate fibers and silica fibers in a weight ratio within the range of about 19:1 to 1:19, and about 0.5 to 30% boron oxide, based on the total weight of the fibers.
- 2. The refractory composite of claim 1 wherein the fibers range in diameter from about 1 to about 15 microns.
- 3. The refractory composite of claim 1 wherein the boron oxide and aluminosilicate fibers are present in the form of aluminoborosilicate fibers.
- 4. The refractory composite of claim 3 also comprising boron oxide, in addition to that present in the fibers.
- 5. The refractory composite of claim 3 wherein the aluminoborosilicate fibers range in diameter from about 3 to 12 microns and the silica fibers range in diameter from about 1 to about 6 microns.
- 6. The refractory composite of claim 1 also comprising a refractory opacifying material.
- 7. The refractory composite of claim 1 wherein the aluminosilicate fiber to silica fiber ratio ranges from 1:9 to 2:3 and the boron oxide content is about 1 to 6% of the fiber weight.
- 8. A refractory composite prepared from aluminoborosilicate fibers containing about 14% boron oxide and pure silica fibers in a weight ratio of about 4:1 and about 3.5% silicon carbide, based on weight of the fibers.
ORIGIN
The invention described herewith was made in the performance of work under a NASA contract and is subject to the provisions of Section 305 of the National Aeronautics and Space Act of 1958, Public Law 85-568 (72 Stat. 435; 42 U.S.C. 2457).
US Referenced Citations (5)