发明名称 METHOD OF FORMING A SET OF TURBO MACHINE IMPELLER BLADES
摘要 FIELD: engines and pumps.SUBSTANCE: invention relates to drive engineering and can be used in assembling the turbomachine impeller blades. For each blade of a plurality of frequency of intrinsic oscillations at the most dangerous shape and weight are measured to define complex criterion, which considers weight characteristics and intrinsic oscillation frequency of blades at the most dangerous form, set consists of blades which complex criterion values deviation from its average value does not exceed specified value, arrangement scheme is selected, at which the spread of values of complex criterion of neighbour blades approximates to its average value and the blades are installed at disk slots by values of complex criterion. Blade weight or static moment or total blade static moment is selected as weight characteristics.EFFECT: higher resistance of turbo machine impeller against self-excited vibrations at the level of impeller unbalance in accordance with requirements of the design documentation.5 cl, 3 dwg, 4 tbl
申请公布号 RU2590983(C2) 申请公布日期 2016.07.10
申请号 RU20140143962 申请日期 2014.10.30
申请人 OTKRYTOE AKTSIONERNOE OBSHSHESTVO "NAUCHNO-PROIZVODSTVENNOE OBEDINENIE "SATURN" 发明人 POSADOV VLADIMIR VALENTINOVICH;POSADOV VLADIMIR VLADIMIROVICH;BAGROV SERGEJ VLADIMIROVICH
分类号 F01D5/10 主分类号 F01D5/10
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