FIELD: powder metallurgy and sealing materials.
SUBSTANCE: invention provides high-temperature composite material, which can be used for applying sealing coatings on the parts of gas-turbine engines. Material contains 10-15% zirconium dioxide stabilized with 7% yttrium oxide, fraction 100-250 μm; 15-25% boron nitride fraction 450-630 μm; 9-12% nichrome fiber 3-5 mm in length; and stabilized zirconium dioxide of activated dusty fraction - the rest.
EFFECT: increased stability under thermocyclation conditions and reduced wear of counter-body.
1 tbl
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Authors
Dates
2007-07-27—Published
2005-08-24—Filed