发明名称 SECTEUR ANGULAIRE DE REDRESSEUR POUR COMPRESSEUR DE TURBOMACHINE
摘要 <p>The sector has a blade (24) extended between inner and outer shells (20, 22) and including radial ends connected to the shells. The blade has leading and trailing edges (24a, 24b) connected on respective edges (26) of the outer shell. An angular locking flange (30) is arranged coaxially around the outer shell. The flange has an assembling unit i.e. projecting tab (34), that assembles the sector on an annular outer case (37) of a turbomachine. The flange has a shoulder (38) that is radially supported against the outer shell.</p>
申请公布号 FR2942638(B1) 申请公布日期 2015.08.21
申请号 FR20090051261 申请日期 2009.02.27
申请人 SNECMA 发明人 CLOAREC YVON
分类号 F01D9/04;F01D25/24;F04D29/54 主分类号 F01D9/04
代理机构 代理人
主权项
地址