发明名称 GAS TURBINE ENGINE HOLLOW BLADE
摘要 FIELD: engines and pumps. ^ SUBSTANCE: proposed blade comprises root including leading and trailing edges jointed by two shells, i.e. back and pressure side. Inner surface of, at least, one shell is provided with ribs jointed with second shell. Said ribs are arranged along direction of centrifugal force action on, blade root and has cross-sections varying over root height. Areas of said cross-sections are defined from conditions of equality of strains on all said cross-sections brought about by said centrifugal forces. ^ EFFECT: higher strength, decreased weight. ^ 2 cl, 4 dwg
申请公布号 RU2450126(C2) 申请公布日期 2012.05.10
申请号 RU20100121009 申请日期 2010.05.24
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "SATURN" 发明人 SABAEV GENRIKH VASIL'EVICH;SHREDER KARL VALENTINOVICH;EROCHKIN MIKHAIL PETROVICH;MURAV'EVA EKATERINA OLEGOVNA
分类号 F01D5/18;F04D29/38 主分类号 F01D5/18
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