发明名称 PROCEDURE FOR MANUFACTURE OF HEAT RESISTANT COATING ON BLADES OF TURBINES OF GAS-TURBINE ENGINES AND POWER INSTALLATIONS
摘要 FIELD: machine building. ^ SUBSTANCE: procedure consists in ion-implantation treatment of blade surface, in vacuum plasma application of heat resistant layer on blade and in successive heat treatment of coating. Ion-implantation treatment of blade surface is carried out with ions of at least one of elements N, Pd, Ag, Nb, Pt, Yb, Y, La, Hf, Cr, Si. The heat resistant layer is applied of alloy of composition: Si - from 4.0 % to 12. 0 %; Y - from 1.0 to 2.0 %; Al - the rest in medium of nitrogen in vacuum not worse, than 10-3 mm murc. col. and at periodic implantation with ions of at least one of elements Nb, Pt, Yb, Y, La, Hf, Cr, Si, Pd, Ag with manufacture of heat resistant micro- and nano layers divided with implanted micro- and nano layers. ^ EFFECT: raised heat resistance of coating at simultaneous increased durability and cyclic hardness of coated parts. ^ 13 cl, 3 tbl, 1 ex
申请公布号 RU2435872(C2) 申请公布日期 2011.12.10
申请号 RU20100103301 申请日期 2010.02.01
申请人 OBSHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU "NAUCHNO-PROIZVODSTVENNOE PREDPRIJATIE VAKUUMMASH" 发明人 MINGAZHEV ASKAR DZHAMILEVICH;BYBIN ANDREJ ALEKSANDROVICH;NOVIKOV ANTON VLADIMIROVICH;SMYSLOVA MARINA KONSTANTINOVNA
分类号 C23C14/24;C23C14/48 主分类号 C23C14/24
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