发明名称 Compressor stator stage
摘要 <p>A diffuser stage comprises concentric external and internal (4) flanges connected to each other by a series of fixed blades (60,61,62). At least one of the flanges has a series of slots (14,15) for the passage of the blades. The blades have at their ends (16,17) a cut-out (20,21,22, 30,31,32) for the passage of a locking element (40,50) which simultaneously unites all the blades in the diffuser stage.</p>
申请公布号 EP1213484(A1) 申请公布日期 2002.06.12
申请号 EP20000870292 申请日期 2000.12.06
申请人 TECHSPACE AERO S.A. 发明人 BOS, MATHIEU
分类号 F01D9/04;F04D29/54;(IPC1-7):F04D29/54 主分类号 F01D9/04
代理机构 代理人
主权项
地址