发明名称 TURBO MACHINE ROTOR
摘要 FIELD: machine building.SUBSTANCE: turbo machine rotor comprises turbine disc fitted on the shaft by its rear flange. Turbine disc is locked by nut with radial flange arranged at disc hub front side. Labyrinth and cellular flange are bolted to radial flange by radial rib. Said labyrinth is locked by axial ledge in circumferential direction relative to sleeve fitted in radial bore. Webs inclined to rotor axis are arranged between radial flange and nut threaded end to make ledges enlarged in circumferential direction. Ledges of the web form the equally spaced rectangular and radial slots between themselves.EFFECT: better reparability, lower weight.2 cl, 3 dwg
申请公布号 RU2516983(C1) 申请公布日期 2014.05.27
申请号 RU20130109314 申请日期 2013.03.01
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 SYCHEV VLADIMIR KONSTANTINOVICH;JAZEV VLADIMIR MIKHAJLOVICH;KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F01D5/02;F02C7/28 主分类号 F01D5/02
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