发明名称 mechanism for blade turnING of axial turbo-machine
摘要 A mechanism for turn includes blades mounted in the body of compressor and connected to synchronization ring by means of levers, synchronization ring is centered with respect to the body of compressor by means of rollers mounted in elastic support fixed on the body of the compressor. Under the elastic support of synchronization ring an adjusting screw is placed, this restricts deformation of the support within the limits providing compensation of thermal expansion. Such implementation makes it possible to increase resource of operation of mechanism.
申请公布号 UA89291(C2) 申请公布日期 2010.01.11
申请号 UA20080006587 申请日期 2008.05.15
申请人 "RESEARCH-AND-PRODUCTION COMPLEX FOR GAS-TURBINE BUILDING "ZORIA"-"MASHPROEKT" STATE ENTERPRISE 发明人 ZHYRNYTSKYI OLEKSANDR OLEHOVYCH;KONEV VALERII IVANOVYCH;SMYRNOV STANISLAV IVANOVYCH;YEVDOSHYN ANDRII ANATOLIIOVYCH
分类号 F04D29/40;F04D29/66 主分类号 F04D29/40
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