发明名称 TWO-STAGE TURBINE ROTOR
摘要 FIELD: engines and pumps. ^ SUBSTANCE: two-stage turbine rotor comprises first-stage turbine, second-stage turbine and intermediate disk arranged in interdisk chamber. Inner surface of the hub of every disk is cylindrical at its center and changes into conical surfaces toward disk hub edges. Note here that disk hub width-to-cylindrical surface width varies from 1.5 to 6 while generatrix angle of disk hub conical surface taper makes 5-15. ^ EFFECT: higher reliability due to uniform distribution of strains over hub inner surface. ^ 1 dwg
申请公布号 RU2453708(C1) 申请公布日期 2012.06.20
申请号 RU20100152635 申请日期 2010.12.22
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 SYCHEV VLADIMIR KONSTANTINOVICH;POLATIDI LJUDMILA BORISOVNA;KARPMAN IRINA VIKTOROVNA;KUZNETSOV VALERIJ ALEKSEEVICH
分类号 F01D5/02 主分类号 F01D5/02
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