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SAFETY METHOD AGAINST HIGH-TEMPERATURE OXIDATION OF INTERNAL CAVITY SURFACE OF COOLED TURBINE BLADES MADE OF CARBON-FREE HEAT-RESISTANCE ALLOY ON BASIS OF NICKEL
SAFETY METHOD AGAINST HIGH-TEMPERATURE OXIDATION OF INTERNAL CAVITY SURFACE OF COOLED TURBINE BLADES MADE OF CARBON-FREE HEAT-RESISTANCE ALLOY ON BASIS OF NICKEL
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机译:基于镍的无碳耐热合金制成的透平涡轮叶片内腔表面高温氧化的安全方法
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FIELD: metallurgy.;SUBSTANCE: it is implemented coating of internal cavity of blade by carbon with saturation rate from 1.5 till 8 g/m2 by means of filling of internal cavity of blade by powder mixture or gaseous medium, heating or isolation of blade with filled internal cavity. Then it is implemented application of diffusion aluminide coating with saturation rate from 15 till 60 g/m2.;EFFECT: high-temperature coat for protection against high-temperature oxidation of internal cavity surface of turbine blade.;3 cl, 1 tbl, 2 ex
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机译:领域:冶金;目的:通过粉末混合物或气态填充叶片内部腔体,以1.5至8 g / m 2 Sup>的饱和速率用碳对叶片内部腔体进行涂覆介质,加热或隔离带有内部空腔的叶片。在此基础上,实现了饱和铝扩散膜的应用,其饱和速率为15〜60 g / m 2 Sup>。效果:为防止涡轮机叶片内腔表面的高温氧化,采用高温涂层。 ; 3 cl,1 tbl,2前
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