发明名称 Shroud or section of shroud in two parts for a vane diffuser of an axial compressor
摘要 <p>The shroud (8) has curved elements provided with notches that correspond to portions of a contour of an end of vanes (4). The curved elements are arranged axially against each other, so as to confine the ends of the vanes in corresponding pairs of notches. An assembly edge in a plane is perpendicular to a main axis of a compressor and adapted to be in a mutual contact during assembly of the curved elements in a direction corresponding to a flow direction via the compressor. A groove is placed along a curved direction of the assembly edge. The shroud is made of a composite material.</p>
申请公布号 EP2336572(A1) 申请公布日期 2011.06.22
申请号 EP20090179128 申请日期 2009.12.14
申请人 TECHSPACE AERO S.A. 发明人 LHOEST, ANDRE;REMY, CHRISTOPHE
分类号 F04D29/16;F01D5/26;F01D11/12 主分类号 F04D29/16
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