发明名称 METHOD OF SEALING TURBINE GAS STAGE AND METHOD OF SEAL FABRICATION
摘要 FIELD: machine building.SUBSTANCE: seals are produced as combination inserts composed of metal substrate, protective diffusion layer applied on the latter in contact with ring groove surface and sealing ceramic material applied on substrate surface opposite the blades. Said seals are fitted in stator ring grooves. Metal substrate is made with protective diffusion layer applied on its surface in contact with stator ring groove by application of protective paste consisting of binder component in amount of 63 wt %, filler making the rest. Metal substrate thus made is subjected to heat treatment to apply cermet sealing material on substrate surface facing the rotor blades by plasma evaporation.EFFECT: reduced deformation, ease of replacement and high wear resistance.2 cl, 3 dwg
申请公布号 RU2508451(C1) 申请公布日期 2014.02.27
申请号 RU20120131043 申请日期 2012.07.20
申请人 OBSHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU "TURBOEHNERGOKOMPLEKS" 发明人 SERKOV ANDREJ VLADIMIROVICH;LONSHAKOVA OKSANA NIKOLAEVNA;TIKHOMIROV ALEKSANDR EMEL'JANOVICH;BABICH IVAN IGNAT'EVICH;SAMOKHIN IVAN ANATOL'EVICH;SELEZNEV VLADIMIR VASIL'EVICH;RAVILOV RINAT GALIMCHANOVICH
分类号 F01D11/08 主分类号 F01D11/08
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