发明名称 |
METHOD OF MAKING HIGHER THERMAL STRENGTH HEAT-RESISTANT CERMET COAT |
摘要 |
FIELD: metallurgy.SUBSTANCE: method of making proposed coat for aircraft and rocket gas turbines and combustion chambers comprises application of alternating ceramic and metal plies on working surface by ion-plasma spraying. First metal ply is applied on said surface. All metal lies are made of identical-depth nickel, depth making at least 4 mcm. Ceramic different depth plies are made of zirconium oxide stabilised by yttrium oxide. First ceramic layer, if seen from working surface, features depth of at least 1-2 mcm. Every next ceramic ply features the depth increased by 2-3 mcm Outer surface ceramic layer features depth of 20-30 mcm.EFFECT: higher thermal strength and heat resistance.1 dwg, 1 ex |
申请公布号 |
RU2510429(C1) |
申请公布日期 |
2014.03.27 |
申请号 |
RU20120149401 |
申请日期 |
2012.11.20 |
申请人 |
FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "MOSKOVSKIJ AVIATSIONNYJ INSTITUT (NATSIONAL'NYJ ISSLEDOVATEL'SKIJ UNIVERSITET)" |
发明人 |
TARASOV SERGEJ SERGEEVICH;RABINSKIJ LEV NAUMOVICH;SOLJAEV JURIJ OLEGOVICH |
分类号 |
C23C14/34;C23C14/08 |
主分类号 |
C23C14/34 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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