发明名称 Device for fixing annular unit on shaft of turbomachine e.g. turbojet of airplane, has nut whose one end comprises external or internal cylindrical surface of shaft, where end of nut is opposite to part of radial support annular unit
摘要 <p>The device has a nut (132) screwed on a shaft (110) for clamping a workpiece on the shaft. An end of the nut comprises an external or internal cylindrical surface (156) of the shaft, where the end of the nut is opposite to a part of a radial support annular unit (154) i.e. leg. A ring (138) is axially engaged in an inside of the nut for preventing rotation of the nut with respect to the shaft. The ring comprises radial projections (140) that are engaged between hooks (152) of the nut and teeth (136) of the shaft.</p>
申请公布号 FR2975449(A1) 申请公布日期 2012.11.23
申请号 FR20110054304 申请日期 2011.05.17
申请人 SNECMA 发明人 PERDRIGEON CHRISTOPHE;JOLY PHILIPPE, GERARD, EDMOND
分类号 F04D29/32;F04D29/054 主分类号 F04D29/32
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