发明名称 Rotor blade for an axial compressor
摘要 <p>The vane has a vane blade with a suction side wall, which is extended towards a vane blade tip by forming span width by an attached vane blade end. The blade comprises a profile (28) and a blade tip side profile (30) with a suction side contour (42) and a pressure side contour (40), and a partially curved skeleton line (32), and a linear chord (34) for vane blade height. The contours, the skeleton line and the chord are extended from a front edge point (24) to a rear edge point. The skeleton line of the blade tip side profile comprises two inflection points (36, 38).</p>
申请公布号 EP2299124(A1) 申请公布日期 2011.03.23
申请号 EP20090011392 申请日期 2009.09.04
申请人 SIEMENS AKTIENGESELLSCHAFT;DLR DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. 发明人 CORNELIUS, CHRISTIAN, DR.;KROEGER, GEORG;NICKE, EBERHARD
分类号 F04D29/32;F01D5/14 主分类号 F04D29/32
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