发明名称 ETAGE DE TURBINE OU DE COMPRESSEUR, EN PARTICULIER DE TURBOMACHINE
摘要 <p>The stage has a vane disk surrounded with a sectorised ring supported by a casing and comprising a circumferential flange radially clamped on an annular rail of the casing by C-shaped cross-section locks (40) that are axially engaged on a casing rail and a flange of the ring. Each lock includes circumferentially directed parallel outer and inner walls (42, 44) that are connected together by a radial wall (46). The walls comprise a radial supporting or bearing unit on the flange and the casing rail, where the bearing unit only extends on a part of a width or angular extent of the lock.</p>
申请公布号 FR2923527(B1) 申请公布日期 2013.12.27
申请号 FR20070007946 申请日期 2007.11.13
申请人 SNECMA 发明人 AUDEON DAVID;DA SILVA DAVID
分类号 F01D11/08 主分类号 F01D11/08
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