发明名称 Blade assembly for turbomachine
摘要 The surface of the blade (1) or a wall (2) in the region of corner flow is provided with at least one auxiliary blade extending from the surface of the blade and/or wall into the flow, set against the flow at this point. In the wake of the auxiliary blade, an eddy is formed whose rotation direction is directed to induce a velocity on the associated blade surface from the blade center to the transition region between wall and blade.
申请公布号 EP0976928(A2) 申请公布日期 2000.02.02
申请号 EP19990114975 申请日期 1999.07.30
申请人 DLR DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. 发明人 BECHERT, DIETRICH, DR.-ING.
分类号 F01D5/14;F04D29/18;F04D29/30;F04D29/32;F04D29/54;F04D29/68 主分类号 F01D5/14
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