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US08012271B2 Material for components of a gas turbine 有权
燃气轮机组件的材料

Material for components of a gas turbine
Abstract:
The presently described technology relates to a material for components of a gas turbine, in particular for components of a gas turbine aircraft engine, having a matrix of an iron-based alloy material, wherein the matrix of the iron-based alloy material being hardened by means of an intermetallic material of the Laves phase.
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