发明名称 GAS TURBINE COOLED BLADE
摘要 FIELD: electric power engineering. SUBSTANCE: aim is to increase blade reliability due to improvement of input edge cooling. Cooled blade of gas turbine has hollow vane with longitudinal fin from lock base, butt inner boss with plug. New thing is, that plug is set so, that it rests at fin butt and its diameter is equal at least to minimum width of vane inner canal section located between boss bottom and fin butt. EFFECT: increased blade reliability due to improvement of input edge cooling. 3 dwg
申请公布号 RU95100646(A) 申请公布日期 1996.11.27
申请号 RU19950100646 申请日期 1995.01.11
申请人 AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 CHERNJAEV I.A.;FADEEV S.I.
分类号 F01D5/10;F01D5/18 主分类号 F01D5/10
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