发明名称 ROTOR OF TWO-STAGE TURBINE
摘要 mechanical engineering; turbines. SUBSTANCE: rotor of two stage turbine has shaft, working disks of first and second stages with cooled blades, and heat screen installed between working disks. Heat screen is made in form of two intermediate disks, each provided with rim, hub and plate with axial channels and holes. Large number of radial rectangular spline projections is made on hubs of intermediate disks. Projections are fitted in spline rectangular slots of centering flanges made under hubs. Clearance is left between projections and slots. EFFECT: improved reliability owing to provision of centering of intermediate disks relative to main disks at all operating conditions of engine. 2 cl, 5 dwg
申请公布号 RU2151883(C1) 申请公布日期 2000.06.27
申请号 RU19980118939 申请日期 1998.10.19
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" 发明人 KUZNETSOV V.A.;IVANOV V.V.
分类号 F01D5/08;(IPC1-7):F01D5/08 主分类号 F01D5/08
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