发明名称 Rotor or rotating element for turbocompressor
摘要 The turbocharger rotor (100) which constitutes the support for a rotor stage (3,3') comprises at least two individual crown wheels (20,21,22) comprising at their periphery half sections (110,110'111,111') which, during the juxtaposition of the crown wheels, make a complete groove (10) in which the feet (80,80') of the movable blades (70,70') are engaged.
申请公布号 EP1319842(A1) 申请公布日期 2003.06.18
申请号 EP20010870277 申请日期 2001.12.17
申请人 TECHSPACE AERO S.A. 发明人 BENEDETTO, DANTE;LAUVERGNAT, JACK-PIERRE
分类号 F01D5/30;F04D29/32;(IPC1-7):F04D29/32 主分类号 F01D5/30
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