发明名称 GAS TURBINE CERMET BLADE
摘要 FIELD: machine building. ^ SUBSTANCE: axial-flow turbo machine blade consists of metal structural rod, shaped ceramic shell, deflector and two-layer heat isolator embracing deflector. Structural rod comprises stem made up of lock elements and bush flange, and radial rod with support flange on its edge. Support flange accommodates retainer flange made from refractory metal alloy jointed with support flange inner surface. Heat isolation outer layer fits ceramic shell inner edge, while inner layer adjoins radial rod. Radial lengths of ceramic shell, deflector, and two-layer heat isolation are identical and equal to radial distance from bush flange to support flange. Ceramic shell radial shape represents separate segments with boundary surfaces interconjugated and perpendicular to radial axis of structural rod. Inner surface of first segment, if seen from the bush flange, fits bush flange. Outer radial surface of said rod fits inner surface of support flange. ^ EFFECT: higher reliability. ^ 4 cl, 1 dwg
申请公布号 RU2433276(C2) 申请公布日期 2011.11.10
申请号 RU20090143051 申请日期 2009.11.20
申请人 OBSHCHESTVO S OGRANICHENNOJ OTVETSTVENNOST'JU "NAUCHNYJ TSENTR "KERAMICHESKIE DVIGATELI" IM. A.M. BOJKO" (OOO "TSENTR BOJKO") 发明人 SUDAREV ANATOLIJ VLADIMIROVICH;SUR'JANINOV ANDREJ ANDREEVICH;MOLCHANOV ALEKSANDR SERGEEVICH;KOLACHEVA JULIJA VLADIMIROVNA
分类号 F01D5/14 主分类号 F01D5/14
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