发明名称 RADIALLY-COMPACT ASSEMBLY BETWEEN A TURBINE SHAFT AND A STUB AXLE OF A TURBOMACHINE COMPRESSOR SHAFT
摘要 The invention relates to an assembly between a turbine shaft and a stub axle of a turbomachine compressor shaft, the assembly comprising a substantially cylindrical compressor shaft stub axle, a substantially cylindrical turbine shaft disposed coaxially inside the compressor shaft stub axle, means for transmitting torque between the turbine shaft and the compressor shaft stub axle, and clamping means for clamping a downstream end of the turbine shaft to the compressor shaft stub axle. The compressor shaft stub axle has a plurality of teeth extending radially from its inside surface, and the turbine shaft is provided at its downstream end with a plurality of axial slots, the teeth of the stub axle co-operating with the slots of the turbine shaft.
申请公布号 US2007212226(A1) 申请公布日期 2007.09.13
申请号 US20070625041 申请日期 2007.01.19
申请人 SNECMA 发明人 GUIHARD FREDERIC;CHARIER GILLES A.
分类号 F04D29/00 主分类号 F04D29/00
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