发明名称 ROTOR OF GAS-TURBINE ENGINE
摘要 FIELD: mechanical engineering; turbine building; turbines of gas turbine engines. SUBSTANCE: rotor of gas turbine engine has shaft with labyrinth seal and Ist and 2nd stage disks with deflector secured on 2nd stage disk. Split rotating rings are installed in ring slot of labyrinth seal between deflector and labyrinth seal. EFFECT: enhanced reliability of rotor of gas turbine engine by sealing radial clearance between deflector and labyrinth seal. 4 dwg
申请公布号 RU2146765(C1) 申请公布日期 2000.03.20
申请号 RU19980114362 申请日期 1998.07.28
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZNETSOV V.A.;IVANOV V.V.
分类号 F01D5/06;F01D11/00;(IPC1-7):F01D5/06 主分类号 F01D5/06
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