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Niobium silicide-based composite material, turbine blade for gas turbine using the same, turbine stationary blade and high-temperature component for gas turbine, and gas turbine, jet engine and high-temperature heat engine using the high-temperature component
Niobium silicide-based composite material, turbine blade for gas turbine using the same, turbine stationary blade and high-temperature component for gas turbine, and gas turbine, jet engine and high-temperature heat engine using the high-temperature component
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摘要
A lamellar structure 2 including a particulate niobium crystal 1, a compound phase 3 containing niobium silicide, and a striped or dotted niobium phase dispersed in the compound phase 3, and composed of the compound phase 3 and the niobium phase. A niobium silicide based composite material containing is disclosed. Thereby, an alloy composite material having excellent heat resistance, strength, toughness, and ductility can be obtained.
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