发明名称 AXIAL-FLOW TURBINE BLADE
摘要 FIELD: turbine engineering. SUBSTANCE: blade has root forming taper surface of flow path, feather with inner surface, and air-flow edge with slit. Root has chamber communicating with inner surface. Chamber wall forming flow path surface and abutting against concave part of feather is perforated on its taper section. Inner surface of end-part feather communicates with radial clearance. EFFECT: improved turbine efficiency. 2 cl, 4 dwg
申请公布号 RU2136895(C1) 申请公布日期 1999.09.10
申请号 RU19970108938 申请日期 1997.06.05
申请人 AKTSIONERNOE OBSHCHESTVO "TURBOMOTORNYJ ZAVOD" 发明人 PROSKURJAKOV G.V.
分类号 F01D5/18 主分类号 F01D5/18
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