FIELD: chemistry.
SUBSTANCE: invention relates to ceramic composite materials and can be used in making heat-loaded assemblies and components of prospective gas-turbine units and engines of gas and oil pumping, transportation and energy systems operating at high thermal cyclic loads at temperatures of up to 1650°C in air and in fuel combustion products. The disclosed ceramic composite material contains carbon fibre and a matrix obtained from a composition having the following chemical composition, wt %: Si 20-35, C 25-40, SiO2 5.5-6.0, HfO2 5-8, SiC - the rest.
EFFECT: high reliability and longer service life of articles under high thermal cyclic loads at operating temperature of up to 1650°C.
3 tbl
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Authors
Dates
2012-04-10—Published
2010-10-05—Filed