FIELD: production of inorganic fibrous heat-insulating materials for hypersonic flying vehicles; aeronautical and space engineering and mechanical engineering.
SUBSTANCE: proposed material possesses high erosion resistance and high-temperature strength at working temperatures of 1000-1700C. Method of production of composite material includes impregnation of ceramic fiber blank with inorganic sol, molding and dehydration of blank by deformation followed by drying at temperature of 50-80C continued for 1-3 h. Dried blank is additionally subjected to impregnation with silicon organic polymer containing nano-powder SiC and secondary drying at temperature of 100-150C continued for 1-3 h. Content of nano-powder SiC in silicon organic polymer is equal to 1-5 mass-%. Heat treatment of blank is performed at temperature of 700-800C for 3-5 h.
EFFECT: enhanced erosion resistance.
4 cl, 2 tbl, 1 ex
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RU2397969C1 |
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SU1781995A1 |
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RU2792488C1 |
Authors
Dates
2007-08-20—Published
2005-09-08—Filed