发明名称 COMPRESSOR RECTIFIER ARCHITECTURE
摘要 The present invention relates to a turbomachine rectifier comprising a plurality of stator vanes (5) connecting an inner collar (4) to an outer collar (3), each of said vanes (5) comprising a blade (11) and a blade-head platform (10), comprising an intermediate piece (6) arranged between the inner collar (4) and the outer collar (3) and fastened to the outer collar (3), said intermediate piece (6) comprising openings (14) for the passage of the vane blades (11) and said vane platforms (10) resting, on one side, on the outer collar (3) and, on the other side, on the intermediate piece (6).
申请公布号 CA2744571(C) 申请公布日期 2017.01.10
申请号 CA20112744571 申请日期 2011.06.27
申请人 TECHSPACE AERO S.A. 发明人 GRELIN, HERVE
分类号 F01D9/04 主分类号 F01D9/04
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