发明名称 Blade grid and turbomachine
摘要 <p>The cascade (1) has a set of blade channels (4) delimited along peripheral direction by a pressure side (6) of a first blade (2a) and an oppositely situated suction side (8) of a second blade (2b). Each channel is delimited along radial direction by two oppositely situated side walls (14). One of the side walls comprises a circumferentially asymmetrical side wall contouring (18) e.g. impression, in an area of one of the blades. The other blade in pressure side or suction side area faces the contouring with shape variation (16) i.e. thickened area, extending downstream at each side wall.</p>
申请公布号 EP2746533(A1) 申请公布日期 2014.06.25
申请号 EP20120197930 申请日期 2012.12.19
申请人 MTU AERO ENGINES AG 发明人 BRETTSCHNEIDER, MARKUS;MALZACHER, FRANZ
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
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