Claims
- 1. A process for producing a high temperature oxidation resistant cermet composition which comprises sintering a mixture of (a) metal or metal alloy particles and (b) a ceramic material comprising silicon nitride and an oxide selected from the group consisting of aluminum oxide, yttrium oxide and chromium oxide, to form a cermet composition of said metal or metal alloy particles coated with and dispersed in a solid solution of said ceramic material.
- 2. A process as defined in claim 1, said mixture including aluminum nitride.
- 3. A process as defined in claim 1, said metal or metal alloy particles being metal particles selected from the group consisting of molybdenum, tungsten, tantalum and niobium particles, said sintering being carried out by hot pressing said mixture at temperature ranging from about 1,700.degree. to about 2,000.degree. C.
- 4. A process as defined in claim 2, said metal or metal alloy particles being metal particles selected from the group consisting of molybdenum, tungsten, tantalum and niobium particles, said sintering being carried out by hot pressing said mixture at temperature ranging from about 1,700.degree. to about 2,000.degree. C.
- 5. A process as defined in claim 3, said mixture containing about 5 to about 40% by volume of said metal particles.
- 6. A process as defined in claim 4, said mixture containing about 5 to about 40% by volume of said metal particles.
- 7. A process as defined in claim 3, said metal particles ranging in size from about 0.001 inches to about 0.125 inches in diameter, said ceramic material consisting of particles of a size less than 1/10 the diameter of said metal particles.
- 8. A process as defined in claim 3, said ceramic material containing about 30 to about 60 mol % silicon nitride, about 40 to about 70 mol % of said oxide.
- 9. A process as defined in claim 6, said ceramic material consisting of about 10 to about 90 mol % of the combination of aluminum nitride and said oxide, the mol proportions of aluminum nitride and said oxide in said combination being approximately equal, and about 10 to about 90 mol % silicon nitride.
- 10. A process as defined in claim 3, said oxide being aluminum oxide.
- 11. A process as defined in claim 6, said oxide being aluminum oxide.
- 12. A process as defined in claim 6, wherein said oxide is a mixture of about 1 to about 10% yttrium oxide and about 90 to about 99% aluminum oxide, by weight.
- 13. A process as defined in claim 6, said metal or metal alloy particles being coated with a binder selected from the group consisting of paraffin wax, carnauba wax and beeswax.
- 14. A process as defined in claim 6, said ceramic material consisting of about 10 to about 90 mol % silicon nitride, about 4 to about 47 mol % of said oxide, and about 5 to about 50 mol % aluminum nitride.
- 15. A process as defined in claim 6, said ceramic material consisting of about 3 to about 22 mol % silicon nitride, about 21 to about 38 mol % of said oxide, and about 55 to about 70 mol % aluminum nitride.
Parent Case Info
This is a division of application Ser. No. 633,876, filed Nov. 20, 1975 now U.S. Pat. No. 4,072,532.
ORIGIN OF INVENTION
The invention described herein 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 USC 2457).
US Referenced Citations (3)
Number |
Name |
Date |
Kind |
3526485 |
Dawihl et al. |
Sep 1970 |
|
3900626 |
Brennan |
Aug 1975 |
|
3914500 |
Prennan et al. |
Oct 1975 |
|
Divisions (1)
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Number |
Date |
Country |
Parent |
633876 |
Nov 1975 |
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