FIELD: aircraft industry.
SUBSTANCE: the invention is dealt with an aircraft industry and may be used for antioxygenation of non-metallic materials on the basis of silicon-carbide mold and a filler made out of carbon fibers. The technical problem of the invention is to increase oxidation resistance of carbon - ceramic composite materials at the temperature of 2000°С. The offered high-temperature coating contains components at the following ratio (in mass %): silicium 4-7, boron 2-4, hafnium oxide 60-65, hafnium boride 6-10, tantalum pentoxide 10-15, hafnium silicide 7-10. The invention allows to produce a high-temperature coating, that is environmentally appropriate and fire-explosive safe.
EFFECT: produced a high-temperature coating, that is environmentally appropriate and fire-explosive safe.
2 tbl
Title | Year | Author | Number |
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HIGH-TEMPERATURE COATING | 2003 |
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HIGH-TEMPERATURE COATING | 2000 |
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HEAT-RESISTING MATERIAL | 2000 |
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RU2178958C2 |
CERAMIC OXIDATING-RESISTANT COMPOSITE MATERIAL AND PRODUCT MADE FROM IT | 2014 |
|
RU2560046C1 |
MATERIAL FOR HEAT-RESISTANT PROTECTIVE COATING | 2017 |
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RU2685905C1 |
METHOD FOR PRODUCING COMPOSITE METAL-DISPERSED COATING, DISPERSED SYSTEM FOR PRECIPITATION OF COMPOSITE METAL-DISPERSED COATING AND METHOD FOR ITS PRODUCTION | 2020 |
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RU2746863C1 |
Authors
Dates
2004-07-20—Published
2002-10-09—Filed