发明名称 Vane diffuser of an axial turbomachine compressor and method for manufacturing same
摘要 <p>The stator has an external shell that includes an annular array of openings and an internal annular groove designed to hold an annular layer (36) of abradable material. A row of stator blades (26) with platforms are located in the openings and secured by one or more weld beads between the platforms and the openings. The row of openings and the internal groove is partially overlapped so that a portion of the weld bead is positioned axially in the internal groove. Independent claims are included for the following: (1) a method of manufacturing a stator; and (2) a turbo-machine.</p>
申请公布号 EP2735706(A1) 申请公布日期 2014.05.28
申请号 EP20120193700 申请日期 2012.11.21
申请人 TECHSPACE AERO S.A. 发明人 CHARLES, XAVIER
分类号 F01D9/04 主分类号 F01D9/04
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