发明名称 METHOD AND DEVICE FOR INFLUENCING SECONDARY FLOWS IN A TURBOMACHINE
摘要 The invention relates to a method for influencing secondary flows in a passage (20) between two adjacent rotating blades and guide vanes (14) of a turbomachine. Said blades project respectively from a lateral wall (12) of a hub or a housing of the turbomachine, and a fluid flows through the passage (20) in a main flow direction (23). According to the method, the following step is carried out in order to reduce internal losses: a stable auxiliary fluid whirl (36) is generated, said whirl rotating in the passage, perpendicular to the main flow direction (23) and in the opposite direction to a secondary whirl (28), using a whirl channel (30) formed in the lateral wall (12) of the hub or housing. Said channel is not rotationally symmetrical in relation to the hub axis.
申请公布号 WO2010000788(A3) 申请公布日期 2011.01.20
申请号 WO2009EP58290 申请日期 2009.07.01
申请人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V.;DORFNER, CHRISTIAN;NICKE, EBERHARD 发明人 DORFNER, CHRISTIAN;NICKE, EBERHARD
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
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