FIELD: metallurgy.
SUBSTANCE: invention can be implemented at high temperature installations, for example in turbine blades, thermo-protecting components, gas or steam turbine case elements and also in blades of gas turbine compressor. Material for a structure component or for a layer consists of material of a matrix and particle (1) with nucleus (7) containing the first element or the first compound, and of at least one shell (4) around nucleus (7) containing the second element or the second compound. Material of the matrix corresponds to an alloy of MCrAlX type, the first element or the first composition of which consists of metal, metal oxide, non-metal oxide, glass or Si-O-C-compound or their mixture and of at least one shell (4', 4", 4'") made of ceramic, in particular of metal oxide.
EFFECT: more long-term protection against oxidation and corrosion.
36 cl, 1 tbl, 9 dwg
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Authors
Dates
2010-07-27—Published
2006-01-30—Filed